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Serialized Form

Package fr.cnes.sirius.patrius.assembly

Class fr.cnes.sirius.patrius.assembly.Assembly extends Object implements Serializable

serialVersionUID: 2142102502513430662L

Serialized Fields

mainPart

MainPart mainPart

Main part of the assembly.

parts

Map<K,V> parts

The other parts.

Class fr.cnes.sirius.patrius.assembly.Vehicle extends Object implements Serializable

serialVersionUID: -6692571768602555532L

Serialized Fields

mainShape

CrossSectionProvider mainShape

Vehicle main shape.

solarPanels

List<E> solarPanels

Solar panels.

engines

List<E> engines

Engines.

tanks

List<E> tanks

Tanks.

dragCoeff

IParamDiffFunction dragCoeff

Drag aero property.

liftCoeff

IParamDiffFunction liftCoeff

Lift aero property.

kAbs

double kAbs

Radiative absorption coefficient (visible spectrum).

kSpec

double kSpec

Radiative specular coefficient (visible spectrum).

kDiff

double kDiff

Radiative diffusion coefficient (visible spectrum).

kAbsIr

double kAbsIr

Radiative absorption coefficient (IR).

kSpecIr

double kSpecIr

Radiative specular coefficient (IR).

kDiffIr

double kDiffIr

Radiative diffusion coefficient (IR).

dryMass

double dryMass

Vehicle dry mass (kg).

Package fr.cnes.sirius.patrius.assembly.models

Class fr.cnes.sirius.patrius.assembly.models.AeroModel extends Parameterizable implements Serializable

serialVersionUID: 4898707923970013932L

Serialized Fields

assembly

Assembly assembly

The considered vehicle on which the model is based on.

massModel

MassProvider massModel

Mass model

atmosphere

Atmosphere atmosphere

The atmosphere.

earthShape

OneAxisEllipsoid earthShape

The earth shape.

altitudeStep

double altitudeStep

Step for atmospheric density derivatives altitude finite differences computation wrt position (m).

vCosA

double vCosA

parameter for the derivatives computation

vCosA2

double vCosA2

parameter for the derivatives computation

v3CosA

double v3CosA

parameter for the derivatives computation

tRelNorm

double tRelNorm

parameter for the derivatives computation

tangentVector

Vector3D tangentVector

parameter for the derivatives computation

aeroSphereParts

List<E> aeroSphereParts

List of parts having an aero cross section property.

aeroFacetParts

List<E> aeroFacetParts

List of parts having an aero facet property.

Class fr.cnes.sirius.patrius.assembly.models.DirectRadiativeModel extends Parameterizable implements Serializable

serialVersionUID: -6974428498597665423L

Serialized Fields

k0

Parameter k0

K0 coefficient parameter

assembly

Assembly assembly

The considered vehicle on which the model is based on.

massModel

MassProvider massModel

Mass model

Class fr.cnes.sirius.patrius.assembly.models.DragLiftModel extends Parameterizable implements Serializable

serialVersionUID: -8747054892764517686L

Serialized Fields

assembly

Assembly assembly

The considered vehicle on which the model is based on.

massModel

MassProvider massModel

Mass model

aeroDragCoefFunction

IParamDiffFunction aeroDragCoefFunction

Drag force coefficient function (Cx)

aeroLiftCoefFunction

IParamDiffFunction aeroLiftCoefFunction

Lift force coefficient function (Cz)

Class fr.cnes.sirius.patrius.assembly.models.GlobalAeroModel extends Object implements Serializable

serialVersionUID: 8030508270216891103L

Serialized Fields

assembly

Assembly assembly

Assembly.

aeroProp

AeroProperty aeroProp

Aero property for the main part.

massModel

MassProvider massModel

Mass model.

dragCoefficientProvider

DragCoefficientProvider dragCoefficientProvider

Drag coefficient (x surface) provider.

atmosphere

ExtendedAtmosphere atmosphere

Atmosphere.

wallGasTemperature

CookWallGasTemperature wallGasTemperature

Wall gas temperature.

hPos

double hPos

Position step for partial derivatives computation.

Class fr.cnes.sirius.patrius.assembly.models.RediffusedRadiativeModel extends Parameterizable implements Serializable

serialVersionUID: 8286763516291639540L

Serialized Fields

assembly

Assembly assembly

The considered vehicle on which the model is based on.

albedo

boolean albedo

calculation indicator of the albedo force

ir

boolean ir

calculation indicator of the infrared force

massModel

MassProvider massModel

mass model of satellite

dAccK0AlParam

double[] dAccK0AlParam

derivative relative to the K0 albedo coefficient

dAccK0IRParam

double[] dAccK0IRParam

derivative relative to the K0 infrared coefficient

dAccSpeParam

Map<K,V> dAccSpeParam

derivative relative to the specular thermo-optic coefficient

dAccDiffParam

Map<K,V> dAccDiffParam

derivative relative to the diffused thermo-optic coefficient

dAccAbsParam

Map<K,V> dAccAbsParam

derivative relative to the absorption thermo-optic coefficient

k0Albedo

Parameter k0Albedo

Parameter for K0 albedo global coefficient.

k0Ir

Parameter k0Ir

Parameter for K0 infrared global coefficient.

Package fr.cnes.sirius.patrius.assembly.models.cook

Class fr.cnes.sirius.patrius.assembly.models.cook.CnCookModel extends Object implements Serializable

serialVersionUID: 4020488548530576523L

Serialized Fields

atmosphere

ExtendedAtmosphere atmosphere

Atmosphere.

facet

Facet facet

Facet.

facetFrame

Frame facetFrame

Facet frame.

epsilon

double epsilon

Specular reemission coefficient.

wallGasTemperatureModel

WallGasTemperatureProvider wallGasTemperatureModel

Wall gas temperature.

Class fr.cnes.sirius.patrius.assembly.models.cook.CtCookModel extends Object implements Serializable

serialVersionUID: 4020488548530576523L

Serialized Fields

atmosphere

ExtendedAtmosphere atmosphere

Atmosphere.

facet

Facet facet

Facet.

facetFrame

Frame facetFrame

Facet frame.

epsilon

double epsilon

Specular reemission coefficient.

Package fr.cnes.sirius.patrius.assembly.properties

Class fr.cnes.sirius.patrius.assembly.properties.AeroCrossSectionProperty extends Parameterizable implements Serializable

serialVersionUID: -6756221234693713611L

Serialized Fields

mainShape

CrossSectionProvider mainShape

Main satellite shape.

dragCoeff

IParamDiffFunction dragCoeff

Drag force coefficient.

Class fr.cnes.sirius.patrius.assembly.properties.AeroFacetProperty extends Parameterizable implements Serializable

serialVersionUID: -7402315627770135950L

Serialized Fields

facet

Facet facet

Facet.

normalCoeff

IParamDiffFunction normalCoeff

Normal force coefficient.

tangentialCoeff

IParamDiffFunction tangentialCoeff

Tangential force coefficient.

Class fr.cnes.sirius.patrius.assembly.properties.AeroGlobalProperty extends Parameterizable implements Serializable

serialVersionUID: -9193369357464080913L

Serialized Fields

dragCoeff

IParamDiffFunction dragCoeff

Drag force coefficient.

liftCoeff

IParamDiffFunction liftCoeff

Lift force coefficient.

mainShape

CrossSectionProvider mainShape

Main satellite shape.

Class fr.cnes.sirius.patrius.assembly.properties.AeroSphereProperty extends AeroCrossSectionProperty implements Serializable

serialVersionUID: -6756221234693713611L

Serialized Fields

sphereRadius

double sphereRadius

Sphere radius (m).

sphereArea

double sphereArea

Sphere radius area (m²).

Class fr.cnes.sirius.patrius.assembly.properties.MassEquation extends Object implements Serializable

serialVersionUID: 4585447992608363108L

Serialized Fields

name

String name

Equation name

flowRate

double flowRate

flow rate

Class fr.cnes.sirius.patrius.assembly.properties.MassProperty extends Parameterizable implements Serializable

serialVersionUID: 4120164826609170722L

Serialized Fields

mass

Parameter mass

Mass of the part.

Class fr.cnes.sirius.patrius.assembly.properties.TankProperty extends Parameterizable implements Serializable

serialVersionUID: 7714453843267281713L

Serialized Fields

name

String name

Name.

massProperty

MassProperty massProperty

Mass property.

Package fr.cnes.sirius.patrius.assembly.properties.features

Class fr.cnes.sirius.patrius.assembly.properties.features.Facet extends Object implements Serializable

Serialized Fields

normal

Vector3D normal

Unit Normal vector

area

double area

Area

Package fr.cnes.sirius.patrius.events

Class fr.cnes.sirius.patrius.events.CentralBodyMaskCircularFOVDetector extends AbstractDetector implements Serializable

serialVersionUID: 4676339505975043489L

Serialized Fields

eclipseDetector

EclipseDetector eclipseDetector

The eclipse detector taking into account ellipsoid body shape

circularFOVDetector

CircularFieldOfViewDetector circularFOVDetector

The circular field of view detector

actionCentralBodyMask

EventDetector.Action actionCentralBodyMask

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed.

Class fr.cnes.sirius.patrius.events.CombinedPhenomenaDetector extends AbstractDetector implements Serializable

serialVersionUID: 6674610443713490158L

Serialized Fields

detector1

EventDetector detector1

First event detector.

increasingIsStart1

boolean increasingIsStart1

True if increasing of the detector1 g function (from negative to positive value) represents the "beginning" of the phenomenon associated to the event.

detector2

EventDetector detector2

Second event detector.

increasingIsStart2

boolean increasingIsStart2

True if increasing of the detector2 g function (from negative to positive value) represents the "beginning" of the phenomenon associated to the event.

together

boolean together

True if the boolean operator is AND, false if it is OR.

actionCombinedPhenomena

EventDetector.Action actionCombinedPhenomena

Action performed

Class fr.cnes.sirius.patrius.events.EarthZoneDetector extends AbstractDetector implements Serializable

serialVersionUID: -1486877151128101288L

Serialized Fields

centralBodyShape

BodyShape centralBodyShape

the central body

fields

List<E> fields

The pyramidal field that represent the cone of space over the zone.

frame

Frame frame

Body attached frame

actionAtEntry

EventDetector.Action actionAtEntry

Action performed when the spacecraft point enters the zone.

actionAtExit

EventDetector.Action actionAtExit

Action performed when the spacecraft point leaves the zone.

removeAtEntry

boolean removeAtEntry

True if detector should be removed when the spacecraft point enters the zone.

removeAtExit

boolean removeAtExit

True if detector should be removed when the spacecraft point leaves the zone.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class fr.cnes.sirius.patrius.events.GenericCodingEventDetector extends Object implements Serializable

serialVersionUID: -8199109406635873283L

Serialized Fields

eventDetector

EventDetector eventDetector

Inner event detector.

increasingCode

String increasingCode

Code for the event that is triggered when g increases (from negative to positive value).

decreasingCode

String decreasingCode

Code for the event that is triggered when g decreases (from positive to negative value).

increasingIsStart

boolean increasingIsStart

True if increasing of the g function (from negative to positive value) represents the "beginning" of the phenomenon associated to the event.

phenomenaSupported

boolean phenomenaSupported

True when phenomena are supported.

phenomenonCode

String phenomenonCode

Phenomenon code.

delay

double delay

The delay of the event to log from the event detected during propagation.

occurrence

int occurrence

The occurrence number of the event to log.

nOccurrence

int nOccurrence

Parameter that tracks the number of occurrences of the event during propagation.

eventType

String eventType

Code for the event we want to log:
- STANDARD: no delay and no occurrence number;
- DELAY: a delay is associated to the logged event;
- N_OCCURRENCE: an occurrence number is associated to the logged event.

Package fr.cnes.sirius.patrius.events.sensor

Class fr.cnes.sirius.patrius.events.sensor.AbstractDetectorWithTropoCorrection extends AbstractDetector implements Serializable

serialVersionUID: -1504378004238040001L

Serialized Fields

correction

AngularCorrection correction

The correction model to apply to the station elevation.

station

GeometricStationAntenna station

Topocentric frame in which elevation should be evaluated.

Class fr.cnes.sirius.patrius.events.sensor.ExtremaSightAxisDetector extends AbstractDetector implements Serializable

serialVersionUID: -5397188919344806100L

Serialized Fields

targetPoint

PVCoordinatesProvider targetPoint

The target point : could be on central body or a vehicle

sightAxis

Vector3D sightAxis

The line defining the sight view expressed in attitude local frame

vehicle

Assembly vehicle

Used if the user define an assembly to define spacecraft

sensorName

String sensorName

Used if the user define an assembly containing a part with sensor property to modelize spacecraft

actionMIN

EventDetector.Action actionMIN

Action performed at local minimum detection.

actionMAX

EventDetector.Action actionMAX

Action performed at local maximum detection.

removeMIN

boolean removeMIN

True if detector should be removed at local minimum detection.

removeMAX

boolean removeMAX

True if detector should be removed at local maximum detection.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class fr.cnes.sirius.patrius.events.sensor.MaskingDetector extends AbstractDetector implements Serializable

serialVersionUID: 9023955237855203037L

Serialized Fields

sensor

SensorModel sensor

the sensor

inAssembly

Assembly inAssembly

the assembly to consider

maskingObjectName

String maskingObjectName

first masking object name

maskingPartName

String maskingPartName

first masking spacecraft's part name (if the first masking part is a spacecraft)

none

String none

"none" String

actionAtRaising

EventDetector.Action actionAtRaising

Action performed when propagation at raising.

actionAtSetting

EventDetector.Action actionAtSetting

Action performed when propagation at setting.

removeAtRaising

boolean removeAtRaising

True if detector should be removed at raising.

removeAtSetting

boolean removeAtSetting

True if detector should be removed at setting.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class fr.cnes.sirius.patrius.events.sensor.RFVisibilityDetector extends AbstractDetector implements Serializable

serialVersionUID: -8151701971140621219L

Serialized Fields

lbModel

RFLinkBudgetModel lbModel

The RF link budget model

lbThreshold

double lbThreshold

The RF link budget threshold for the nominal mode

assembly

Assembly assembly

The assembly representing the satellite.

actionAtEntry

EventDetector.Action actionAtEntry

Action performed when entering the region of RF visibility.

actionAtExit

EventDetector.Action actionAtExit

Action performed when exiting the region of RF visibility.

removeAtEntry

boolean removeAtEntry

True if detector should be removed when the spacecraft point enters the zone.

removeAtExit

boolean removeAtExit

True if detector should be removed when the spacecraft point leaves the zone.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class fr.cnes.sirius.patrius.events.sensor.SatToSatMutualVisibilityDetector extends AbstractDetector implements Serializable

serialVersionUID: 8838555816491196733L

Serialized Fields

inMainSpacecraftId

String inMainSpacecraftId

the main spacecraft id

inSecondarySpacecraftId

String inSecondarySpacecraftId

the secondary spacecraft id

inSensorMainSpacecraft

SensorModel inSensorMainSpacecraft

the main spacecraft sensor

inMainSpacecraft

Assembly inMainSpacecraft

the main assembly to consider

inSensorSecondarySpacecraft

SensorModel inSensorSecondarySpacecraft

the secondary spacecraft sensor

inSecondarySpacecraft

Assembly inSecondarySpacecraft

the secondary assembly to consider

secondPropagator

Propagator secondPropagator

the propagator for the secondary spacecraft (in single spacecraft propagation mode)

maskingCheck

boolean maskingCheck

true if maskings must be computed

actionAtEntry

EventDetector.Action actionAtEntry

Action performed when entering the visibility zone.

actionAtExit

EventDetector.Action actionAtExit

Action performed when exiting the visibility zone.

removeAtEntry

boolean removeAtEntry

True if detector should be removed when entering the visibility zone.

removeAtExit

boolean removeAtExit

True if detector should be removed when exiting the visibility zone.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

firstCall

boolean firstCall

True if g() method is called for thr first time.

type

fr.cnes.sirius.patrius.events.sensor.SatToSatMutualVisibilityDetector.PropagationType type

Type of the propagation (mono or multi).

Class fr.cnes.sirius.patrius.events.sensor.SecondarySpacecraft extends Object implements Serializable

serialVersionUID: 4244801907421842435L

Serialized Fields

inAssembly

Assembly inAssembly

the spacecraft's assembly

inPropagator

Propagator inPropagator

the spacecraft's propagator

inName

String inName

the spacecraft's name

Class fr.cnes.sirius.patrius.events.sensor.SensorInhibitionDetector extends AbstractDetector implements Serializable

serialVersionUID: 5320120546742645596L

Serialized Fields

sensor

SensorModel sensor

the sensor

inAssembly

Assembly inAssembly

the assembly to consider

inhibitionNumber

int inhibitionNumber

the first inhibition target to enter its field

actionAtEntry

EventDetector.Action actionAtEntry

Action performed when entering the inhibition zone.

actionAtExit

EventDetector.Action actionAtExit

Action performed when exiting the inhibition zone.

removeAtEntry

boolean removeAtEntry

True if detector should be removed when entering the inhibition zone.

removeAtExit

boolean removeAtExit

True if detector should be removed when exiting the inhibition zone.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class fr.cnes.sirius.patrius.events.sensor.SensorVisibilityDetector extends AbstractDetector implements Serializable

serialVersionUID: 5320120546742645596L

Serialized Fields

sensor

SensorModel sensor

the sensor

inAssembly

Assembly inAssembly

the assembly to consider

inhibitionNumber

int inhibitionNumber

the first inhibition target to enter its field

maskingObjectName

String maskingObjectName

first masking object name

maskingPartName

String maskingPartName

first masking spacecraft's part name (if the first masking part is a spacecraft)

none

String none

"none" String

actionAtEntry

EventDetector.Action actionAtEntry

Action performed when entering the visibility zone.

actionAtExit

EventDetector.Action actionAtExit

Action performed when exiting the visibility zone.

removeAtEntry

boolean removeAtEntry

True if detector should be removed when entering the visibility zone.

removeAtExit

boolean removeAtExit

True if detector should be removed when exiting the visibility zone.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class fr.cnes.sirius.patrius.events.sensor.StationToSatMutualVisibilityDetector extends AbstractDetectorWithTropoCorrection implements Serializable

serialVersionUID: -3026633624287530222L

Serialized Fields

inSensorSpacecraft

SensorModel inSensorSpacecraft

The spacecraft sensor

inSpacecraft

Assembly inSpacecraft

The assembly to consider

maskingCheck

boolean maskingCheck

True if maskings must be computed

actionAtEntry

EventDetector.Action actionAtEntry

Action performed when entering the visibility zone.

actionAtExit

EventDetector.Action actionAtExit

Action performed when exiting the visibility zone.

removeAtEntry

boolean removeAtEntry

True if detector should be removed when entering the visibility zone.

removeAtExit

boolean removeAtExit

True if detector should be removed when exiting the visibility zone.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class fr.cnes.sirius.patrius.events.sensor.TargetInFieldOfViewDetector extends AbstractDetector implements Serializable

serialVersionUID: 5320120546742645596L

Serialized Fields

sensor

SensorModel sensor

the sensor

inAssembly

Assembly inAssembly

the assembly to consider

actionAtEntry

EventDetector.Action actionAtEntry

Action performed when entering the visibility zone.

actionAtExit

EventDetector.Action actionAtExit

Action performed when exiting the visibility zone.

removeAtEntry

boolean removeAtEntry

True if detector should be removed when entering the visibility zone.

removeAtExit

boolean removeAtExit

True if detector should be removed when exiting the visibility zone.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class fr.cnes.sirius.patrius.events.sensor.VisibilityFromStationDetector extends AbstractDetectorWithTropoCorrection implements Serializable

serialVersionUID: 764052454048950887L

Serialized Fields

actionAtRaising

EventDetector.Action actionAtRaising

Action performed when propagation at raising.

actionAtSetting

EventDetector.Action actionAtSetting

Action performed when propagation at setting.

removeAtRaising

boolean removeAtRaising

True if detector should be removed at raising.

removeAtSetting

boolean removeAtSetting

True if detector should be removed at setting.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Package fr.cnes.sirius.patrius.forces

Class fr.cnes.sirius.patrius.forces.ConstantThrustManeuver extends JacobiansParameterizable implements Serializable

serialVersionUID: 5349622732741384211L

Serialized Fields

firingStartDetector

EventDetector firingStartDetector

Firing start detector.

firingStopDetector

EventDetector firingStopDetector

Firing stop detector.

direction

Vector3D direction

inDirection of the acceleration in the frame defined by the user.

frame

Frame frame

Frame of the acceleration inDirection. If null and no LOF has been provided, the acceleration is expressed in the satellite frame.

lofType

LOFType lofType

Local orbital frame type. If null and no frame has been provided, the acceleration is expressed in the satellite frame.

massModel

MassProvider massModel

Mass model.

tankProp

TankProperty tankProp

Tank property.

engineProp

PropulsiveProperty engineProp

Propulsive property.

firing

boolean firing

State of the engine (internal variable).

removeMassDv

boolean removeMassDv

Boolean for removal of mass dv (internal variable).

Class fr.cnes.sirius.patrius.forces.EmpiricalForce extends JacobiansParameterizable implements Serializable

serialVersionUID: 5685047685477772591L

Serialized Fields

n

int n

The harmonic factor.

s

Vector3D s

The vector S whose cross product with ω is used as a reference direction for the spacecraft orbital position computation. This vector shall be expressed in the SpacecraftState inertial frame.

coeffFrame

Frame coeffFrame

The local frame of definition of vectors A, B and C If null, the acceleration is expressed in the satellite frame

coeffFrameLOFType

LOFType coeffFrameLOFType

The local orbital frame type of definition of vectors A, B and C.

coeffAx

IParamDiffFunction coeffAx

Parameterizable coef A (representing the coefficient of cos(wnt) in the acceleration formula) along x.

coeffAy

IParamDiffFunction coeffAy

Parameterizable coef A (representing the coefficient of cos(wnt) in the acceleration formula) along y.

coeffAz

IParamDiffFunction coeffAz

Parameterizable coef A (representing the coefficient of cos(wnt) in the acceleration formula) along z.

coeffBx

IParamDiffFunction coeffBx

Parameterizable coef B (representing the coefficient of sin(wnt) in the acceleration formula) along x.

coeffBy

IParamDiffFunction coeffBy

Parameterizable coef B (representing the coefficient of sin(wnt) in the acceleration formula) along y.

coeffBz

IParamDiffFunction coeffBz

Parameterizable coef B (representing the coefficient of sin(wnt) in the acceleration formula) along z.

coeffCx

IParamDiffFunction coeffCx

Parameterizable coef C (representing the constant term in the acceleration formula) along x.

coeffCy

IParamDiffFunction coeffCy

Parameterizable coef C (representing the constant term in the acceleration formula) along y.

coeffCz

IParamDiffFunction coeffCz

Parameterizable coef C (representing the constant term in the acceleration formula) along z.

Class fr.cnes.sirius.patrius.forces.VariableThrustManeuver extends JacobiansParameterizable implements Serializable

serialVersionUID: 7627704061185299151L

Serialized Fields

firingStartDetector

EventDetector firingStartDetector

Firing start detector.

firingStopDetector

EventDetector firingStopDetector

Firing stop detector.

thrust

IDependentVariable<T> thrust

Engine thrust.

direction

IDependentVectorVariable<T> direction

Direction of the thrust in the frame defined by the user.

frame

Frame frame

Frame of the acceleration direction. If null and no LOF has been provided, the acceleration is expressed in the satellite frame.

lofType

LOFType lofType

Local orbital frame type. If null and no frame has been provided, the acceleration is expressed in the satellite frame.

isp

IDependentVariable<T> isp

ISP.

mass

MassProvider mass

Mass model

partFiring

String partFiring

Name of thruster in mass model

firing

boolean firing

State of the engine.

lastFlowRate

double lastFlowRate

Last flow rate

Package fr.cnes.sirius.patrius.forces.radiation

Class fr.cnes.sirius.patrius.forces.radiation.PatriusSolarRadiationPressure extends JacobiansParameterizable implements Serializable

serialVersionUID: -4510170320082379419L

Serialized Fields

sun

PVCoordinatesProvider sun

Sun model.

earthModel

GeometricBodyShape earthModel

Earth model.

spacecraft

RadiationSensitive spacecraft

Spacecraft.

fluxParam

Parameter fluxParam

Normalized reference flux parameter

cachedSatSunVector

Vector3D cachedSatSunVector

Cached Satellite-Sun vector.

cachedPosition

Vector3D cachedPosition

Cached satellite position.

cachedDate

AbsoluteDate cachedDate

Cached date.

computePartialDerivativesWrtPosition

boolean computePartialDerivativesWrtPosition

True if acceleration partial derivatives with respect to position have to be computed.

Package fr.cnes.sirius.patrius.guidance

Class fr.cnes.sirius.patrius.guidance.AngularVelocitiesHarmonicProfile extends GuidanceProfile implements Serializable

serialVersionUID: 5937397877355934211L

Serialized Fields

date

AbsoluteDate date

initial date

rotation

Rotation rotation

initial rotation

oFrame

Frame oFrame

frame of initial rotation and Fourier series

xfs

FourierSeries xfs

theta dot x

yfs

FourierSeries yfs

theta dot y

zfs

FourierSeries zfs

theta dot z

vectorFunction

Vector3DFunction vectorFunction

angular velocity wrapper

type

KinematicsToolkit.IntegrationType type

integration type

step

double step

integration step

Class fr.cnes.sirius.patrius.guidance.AngularVelocitiesPolynomialProfile extends GuidanceProfile implements Serializable

serialVersionUID: 481261569201925028L

Serialized Fields

referenceFrame

Frame referenceFrame

The reference frame of the polynomial functions.

rotation

Rotation rotation

Initial rotation.

dateZero

AbsoluteDate dateZero

The date at x = 0.

segments

List<E> segments

List of polynomial functions on segments.

vectorFunction

Vector3DFunction vectorFunction

Angular velocity wrapper

type

KinematicsToolkit.IntegrationType type

integration type

step

double step

integration step

Class fr.cnes.sirius.patrius.guidance.GuidanceProfile extends Object implements Serializable

serialVersionUID: 1774730921131738218L

Serialized Fields

interval

AbsoluteDateInterval interval

interval of validity

Class fr.cnes.sirius.patrius.guidance.QuaternionHarmonicProfile extends GuidanceProfile implements Serializable

serialVersionUID: 4343338300700455854L

Serialized Fields

date0

AbsoluteDate date0

Initial date.

referenceFrame

Frame referenceFrame

The reference frame of the Fourier series.

q0fs

FourierSeries q0fs

Fourier series representing the q0 component of the quaternion.

q1fs

FourierSeries q1fs

Fourier series representing the q1 component of the quaternion.

q2fs

FourierSeries q2fs

Fourier series representing the q2 component of the quaternion.

q3fs

FourierSeries q3fs

Fourier series representing the q3 component of the quaternion.

Class fr.cnes.sirius.patrius.guidance.QuaternionPolynomialProfile extends GuidanceProfile implements Serializable

serialVersionUID: -8642294471802958076L

Serialized Fields

referenceFrame

Frame referenceFrame

The reference frame of the polynomial functions.

segments

List<E> segments

List of polynomial functions on segments.

Package fr.cnes.sirius.patrius.projections

Class fr.cnes.sirius.patrius.projections.AbstractProjection extends Object implements Serializable

serialVersionUID: -5639443987042063885L

Serialized Fields

referenceShape

ProjectionEllipsoid referenceShape

Reference shape.

pivot

GeodeticPoint pivot

Pivot point used for projections define by its longitude and latitude.

Class fr.cnes.sirius.patrius.projections.GeneralizedFlamsteedSamson extends Mercator implements Serializable

serialVersionUID: -5510747491232792509L

Class fr.cnes.sirius.patrius.projections.IdentityProjection extends AbstractProjection implements Serializable

serialVersionUID: 430763443341865968L

Class fr.cnes.sirius.patrius.projections.Mercator extends AbstractProjection implements Serializable

serialVersionUID: 5232288358412768877L

Serialized Fields

azimuth

double azimuth

Azimuth (for rotated Mercator projection), can be 0. Convention used : azimuth is angle from the north direction to the current direction in CLOCKWISE sense.

cosAz

double cosAz

Cosinus of the azimuth.

sinAz

double sinAz

Sinus of the azimuth.

centered

boolean centered

if centered, Y coordinates equal 0 in pivot point. The rotation if around pivot.

series

boolean series

indicates if the inverse projection uses a direct method with series, or an iterative method.

pivotCosLat

double pivotCosLat

Cosinus of the latitude at the pivot point.

scaledRadius

double scaledRadius

Celestial body scaled radius.

Class fr.cnes.sirius.patrius.projections.ProjectionEllipsoid extends ExtendedOneAxisEllipsoid implements Serializable

serialVersionUID: 1L

Serialized Fields

series

double[] series

Ellipsoid series coefficients used to compute ellipsoid series

See Also:: https://pubs.er.usgs.gov/publication/pp1395

seriesComputed

boolean seriesComputed

Boolean to indicate if series have been computed.

Package fr.cnes.sirius.patrius.propagation

Class fr.cnes.sirius.patrius.propagation.PVCoordinatePropagator extends AbstractPropagator implements Serializable

serialVersionUID: -7801485357930534815L

Serialized Fields

pvProv

PVCoordinatesProvider pvProv

PVCoordinatesProvider used to propagate the position velocity

Package fr.cnes.sirius.patrius.propagation.precomputed.multi

Class fr.cnes.sirius.patrius.propagation.precomputed.multi.MultiIntegratedEphemeris extends AbstractPropagator implements Serializable

serialVersionUID: 2114446502509891643L

Serialized Fields

orbitType

OrbitType orbitType

Propagation orbit type.

angleType

PositionAngle angleType

Position angle type.

referenceFrame

Frame referenceFrame

Reference frame.

stateVectorInfo

MultiStateVectorInfo stateVectorInfo

State vector informations

mu

double mu

Central body gravitational constant.

startDates

List<E> startDates

List of start dates of the integration (can be min or max).

minDates

List<E> minDates

List of first date of the ranges.

maxDates

List<E> maxDates

List of last date of the ranges.

models

List<E> models

List of underlying raw mathematical models.

satId

String satId

Sat id.

Package fr.cnes.sirius.patrius.signalpropagation

Class fr.cnes.sirius.patrius.signalpropagation.AzoulayModel extends Object implements Serializable

serialVersionUID: 4794751982189820026L

Serialized Fields

inPressure

double inPressure

the ground atmospheric pressure

tK

double tK

the ground atmospheric temperature

inMoisture

double inMoisture

the ground atmospheric moisture

inAltitude

double inAltitude

the ground point geodetic altitude

inIsGeometricElevation

boolean inIsGeometricElevation

True if the correction due to the troposphere is computed from the geometric value of the elevation, to get the true elevation value; false if the correction is computed from the true value of the elevation (the measure), to get the geometric value.

Package fr.cnes.sirius.patrius.stela

Class fr.cnes.sirius.patrius.stela.PerigeeAltitudeDetector extends AbstractDetector implements Serializable

serialVersionUID: -1552109617025755015L

Serialized Fields

altitude

double altitude

Threshold altitude value (m).

earthRadius

double earthRadius

earth Radius with respect to which altitude should be evaluated.

isOsculating

boolean isOsculating

Is the perigee to be computed in osculating elements.

orbitConverter

OrbitNatureConverter orbitConverter

Orbit convertor to compute osculating perigee.

actionAtAscending

EventDetector.Action actionAtAscending

Action performed at altitude detection when ascending.

actionAtDescending

EventDetector.Action actionAtDescending

Action performed at altitude detection when descending.

removeAtAscending

boolean removeAtAscending

True if detector should be removed at altitude detection when ascending.

removeAtDescending

boolean removeAtDescending

True if detector should be removed at altitude detection when descending.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed at altitude detection (updated by eventOccured).

Package fr.cnes.sirius.patrius.stela.bodies

Class fr.cnes.sirius.patrius.stela.bodies.MeeusMoonStela extends AbstractCelestialBody implements Serializable

serialVersionUID: 1L

Serialized Fields

earthRadius

double earthRadius

The Earth Radius.

Class fr.cnes.sirius.patrius.stela.bodies.MeeusSunStela extends AbstractCelestialBody implements Serializable

serialVersionUID: 1L

Package fr.cnes.sirius.patrius.stela.forces.atmospheres

Class fr.cnes.sirius.patrius.stela.forces.atmospheres.MSIS00Adapter extends Object implements Serializable

serialVersionUID: -1995857838866326747L

Serialized Fields

atmosModel

NRLMSISE00 atmosModel

An instance of the MSIS00 model.

output

Output output

Output for the MSIS00 density computation.

flags

Flags flags

Flags for the MSIS00 density computation.

flattening

double flattening

Flattening of the Earth.

rEquatorial

double rEquatorial

Earth Radius.

inputParams

MSISE2000InputParameters inputParams

Solar activity data container.

calendar

Calendar calendar

Calendar (internal variable, set there for computation time saving).

sun

CelestialBody sun

The Sun.

cachedTemperature

double cachedTemperature

Cache mecanism - Output temperature.

cachedOutputData

AtmosphereData cachedOutputData

Cache mecanism - Output atmosphere data.

cachedDate

AbsoluteDate cachedDate

Cache mecanism - Input date.

cachedFrame

Frame cachedFrame

Cache mecanism - Input frame.

cachedPosition

Vector3D cachedPosition

Cache mecanism - Input position.

Package fr.cnes.sirius.patrius.stela.forces.drag

Class fr.cnes.sirius.patrius.stela.forces.drag.StelaAeroModel extends Parameterizable implements Serializable

serialVersionUID: 4898707923970013932L

Serialized Fields

mass

double mass

The spacecraft mass.

cd

StelaCd cd

The spacecraft drag coefficient.

surface

double surface

The spacecraft cross section (m²).

atmosphere

Atmosphere atmosphere

The atmosphere.

geodPosition

GeodPosition geodPosition

The class representing the geodetic position of the spacecraft.

densityDerivativesByFullFiniteDifference

boolean densityDerivativesByFullFiniteDifference

Atmospheric density derivatives computation by full finite differences or altitude finite differences flag.

atmosDp

double atmosDp

Parameters representing:
- dX in atmospheric density derivatives full finite differences computation (m).
- dH in atmospheric density derivatives altitude finite differences computation (m).

Package fr.cnes.sirius.patrius.stela.orbits

Class fr.cnes.sirius.patrius.stela.orbits.StelaEquinoctialOrbit extends Orbit implements Serializable

serialVersionUID: 4389291298378313927L

Serialized Fields

parameters

StelaEquinoctialParameters parameters

Orbital parameters.

Package fr.cnes.sirius.patrius.stela.propagation

Class fr.cnes.sirius.patrius.stela.propagation.ForcesStepHandler extends Object implements Serializable

serialVersionUID: 6884459947160793318L

Serialized Fields

converter

OrbitNatureConverter converter

Orbit nature converter.

nonInertialContribution

NonInertialContribution nonInertialContribution

Non-inertial contribution.

dnonInertial

double[] dnonInertial

Non-inertial contribution (value).

Class fr.cnes.sirius.patrius.stela.propagation.StelaAbstractPropagator extends Object implements Serializable

serialVersionUID: 2434402795728927604L

Serialized Fields

oldStepHandler

OrekitFixedStepHandler oldStepHandler

Entry Step handler.

eventsStates

Collection<E> eventsStates

Event steps.

integrator

FirstOrderIntegrator integrator

Integrator for the orbital extrapolation process.

attitudeProviderForces

AttitudeProvider attitudeProviderForces

Attitude provider for forces computation.

attitudeProviderEvents

AttitudeProvider attitudeProviderEvents

Attitude provider for events computation.

attitudeProviderByDefault

AttitudeProvider attitudeProviderByDefault

Attitude provider given by default for one attitude.

mode

int mode

Propagation mode.

fixedStepSize

double fixedStepSize

Fixed step size.

stepHandler

OrekitStepHandler stepHandler

Step handler.

stepHandlers

List<E> stepHandlers

Step handlers.

statesInitialized

boolean statesInitialized

Initialization indicator of events states.

additionalStateProviders

List<E> additionalStateProviders

Additional state providers.

interpolator

StelaBasicInterpolator interpolator

Steps interpolator.

lastPropagationStart

AbsoluteDate lastPropagationStart

Start date of last propagation.

lastPropagationEnd

AbsoluteDate lastPropagationEnd

End date of last propagation.

startDate

AbsoluteDate startDate

Start date.

pvProvider

PVCoordinatesProvider pvProvider

Provider for attitude computation.

initialState

SpacecraftState initialState

Initial state.

isLastStep

boolean isLastStep

Indicator for last step.

isLastDetection

boolean isLastDetection

Indicator for last detection of the current detector.

interInitialised

boolean interInitialised

Initialisation indicator for interpolation

storeTimeDerivatives

boolean storeTimeDerivatives

Flag to indicate if time derivatives dE'/dt must be stored.

registerTimeDerivatives

boolean registerTimeDerivatives

Flag to indicate if time derivatives dE'/dt must be stored during next step (internal use only).

timeDerivativesList

List<E> timeDerivativesList

Time derivatives list.

Class fr.cnes.sirius.patrius.stela.propagation.StelaBasicInterpolator extends Object implements Serializable

serialVersionUID: 26269718303505539L

Serialized Fields

previousDate

AbsoluteDate previousDate

Previous date.

currentDate

AbsoluteDate currentDate

Current date.

interpolatedState

SpacecraftState interpolatedState

Interpolated state.

initialState

SpacecraftState initialState

Initial state.

currentState

SpacecraftState currentState

Interpolated state.

forward

boolean forward

Forward propagation indicator.

additionalStateProviders

List<E> additionalStateProviders

Additional state providers.

Class fr.cnes.sirius.patrius.stela.propagation.StelaGTOPropagator extends StelaAbstractPropagator implements Serializable

serialVersionUID: 6976438319827286237L

Serialized Fields

wasException

boolean wasException

Was the exception mecanism triggered already

maxDate

AbsoluteDate maxDate

Max date after which simulation has to fail if exception mecanism was triggered

stepCounter

int stepCounter

Step counter for drag computation.

integrationFrame

Frame integrationFrame

Frame to be used during the extrapolation (CIRF).

gaussForces

List<E> gaussForces

Gauss force models used during the extrapolation of the orbit.

lagrangeForces

List<E> lagrangeForces

Lagrange force models used during the extrapolation of the orbit.

referenceDate

AbsoluteDate referenceDate

Reference date.

mu

double mu

Current μ.

mass

double mass

The mass of the spacecraft.

osculatingFlag

boolean osculatingFlag

Is the orbital state in osculating parameters.

addEquationsList

List<E> addEquationsList

Additional equations and associated data.

converter

OrbitNatureConverter converter

The mean / osculating orbit converter.

recomputeDrag

boolean recomputeDrag

Drag re-computation parameter

dDragdt

double[] dDragdt

Stored drag contribution.

maxShift

double maxShift

Maximum number of original steps after which propagation is stopped

minStepSize

double minStepSize

Minimum step size.

forcesStepHandler

ForcesStepHandler forcesStepHandler

Step handler for forces requiring update every step, not every substep.

Package fr.cnes.sirius.patrius.tools.ephemerisComparator

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.AbstractDataLoader extends Object implements Serializable

serialVersionUID: -8498144026343789919L

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.ComparisonData extends Data<Double> implements Serializable

serialVersionUID: 9118379652399697119L

Serialized Fields

thresholds

ArrayList<E> thresholds

represents an associated set of thresholds

meanDeviation

ArrayList<E> meanDeviation

represents an associated set of means, one per column

maxDeviation

ArrayList<E> maxDeviation

represents an associated set of maximums, one per column

sigmaDeviation

ArrayList<E> sigmaDeviation

represents an associated set of sigma, one per column

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.Data extends Object implements Serializable

serialVersionUID: -1686168254739120113L

Serialized Fields

columns

ArrayList<E> columns

represents a set of columns extracted from a data file.

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.DateDPFacade extends AbsoluteDate implements Serializable

serialVersionUID: 4873688185707481412L

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.MeaningfulData extends Data<DeviationProvider> implements Serializable

serialVersionUID: 1019774180194459606L

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.PSimuDataLoader extends AbstractDataLoader implements Serializable

serialVersionUID: 1652822976916289540L

Serialized Fields

ephemerisPattern

Pattern ephemerisPattern

Pattern for the ephemeris columns.

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.PVCoordinatesDPFacade extends PVCoordinates implements Serializable

serialVersionUID: 6453185373436578483L

Serialized Fields

type

DataType type

The type associated with this PV instance : conditions the type of computed deviation.

qsw

boolean qsw

QSW or TNW frame.

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.RawDataComparator extends DataComparator<Double> implements Serializable

serialVersionUID: 8189165708223983569L

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.ThresholdsData extends Data<Double> implements Serializable

serialVersionUID: 7662856391834918136L

Serialized Fields

acceptableNumbers

ArrayList<E> acceptableNumbers

represents an associated set of number of acceptable lines, one per column

refusedNumbers

ArrayList<E> refusedNumbers

represents an associated set of number of refused lines, one per column

firstRefusedLines

ArrayList<E> firstRefusedLines

represents an associated set of number of the first refused lines on each column.

Class fr.cnes.sirius.patrius.tools.ephemerisComparator.VectorDPFacade extends ArrayRealVector implements Serializable

serialVersionUID: -7474179759071392547L

Package fr.cnes.sirius.patrius.tools.exception

Class fr.cnes.sirius.patrius.tools.exception.EphemerisComparatorException extends Exception implements Serializable

serialVersionUID: 3499429249873865775L

Class fr.cnes.sirius.patrius.tools.exception.EphemerisComparatorRuntimeException extends RuntimeException implements Serializable

serialVersionUID: 3681052026194387286L

Package fr.cnes.sirius.patrius.utils

Class fr.cnes.sirius.patrius.utils.AngleInterval extends AbstractInterval implements Serializable

serialVersionUID: -5206233637720732029L

Serialized Fields

lowerAngle

double lowerAngle

lower end angle value

upperAngle

double upperAngle

upper end angle value

reference

double reference

reference angle value

length

double length

interval length value

Class fr.cnes.sirius.patrius.utils.GenericInterval extends AbstractInterval implements Serializable

serialVersionUID: -8322705461339724889L

Serialized Fields

upperData

Object upperData

upper end data value

lowerData

Object lowerData

lower end data value

Package fr.cnes.sirius.patrius.wrenches

Class fr.cnes.sirius.patrius.wrenches.SolarRadiationWrench extends Parameterizable implements Serializable

serialVersionUID: 2682628484008113102L

Serialized Fields

sun

PVCoordinatesProvider sun

Sun model.

earthModel

GeometricBodyShape earthModel

Earth model.

spacecraft

RadiationWrenchSensitive spacecraft

Spacecraft.

sunDistance

Parameter sunDistance

Parameter for reference sun distance

sunPressure

Parameter sunPressure

Parameter for reference sun pressure

cachedSatSunVector

Vector3D cachedSatSunVector

Cached Satellite-Sun vector.

cachedPosition

Vector3D cachedPosition

Cached satellite position.

cachedDate

AbsoluteDate cachedDate

Cached date.

Package fr.cnes.sirius.validate.mocks.ephemeris

Class fr.cnes.sirius.validate.mocks.ephemeris.UserCelestialBody extends AbstractCelestialBody implements Serializable

serialVersionUID: -1863617019515445599L

Serialized Fields

eph

IUserEphemeris eph

Ephemeris.

dateEphemeris

AbsoluteDate[] dateEphemeris

The list of dates.

framesConfiguration

FramesConfiguration framesConfiguration

Frame configuration.

Package fr.cnes.sirius.validate.parallel

Class fr.cnes.sirius.validate.parallel.ParallelException extends RuntimeException implements Serializable

serialVersionUID: 5510913937832728366L

Package org.apache.commons.math3.analysis.differentiation

Class org.apache.commons.math3.analysis.differentiation.DerivativeStructure extends Object implements Serializable

serialVersionUID: 20120730L

Serialization Methods

writeReplace

private Object writeReplace()

Replace the instance with a data transfer object for serialization.

Serialized Fields

data

double[] data

Combined array holding all values.

Class org.apache.commons.math3.analysis.differentiation.FiniteDifferencesDifferentiator extends Object implements Serializable

serialVersionUID: 20120917L

Serialized Fields

nbPoints

int nbPoints

Number of points to use.

stepSize

double stepSize

Step size.

halfSampleSpan

double halfSampleSpan

Half sample span.

tMin

double tMin

Lower bound for independent variable.

tMax

double tMax

Upper bound for independent variable.

Package org.apache.commons.math3.analysis.interpolation

Class org.apache.commons.math3.analysis.interpolation.DividedDifferenceInterpolator extends Object implements Serializable

serialVersionUID: 107049519551235069L

Class org.apache.commons.math3.analysis.interpolation.LoessInterpolator extends Object implements Serializable

serialVersionUID: 5204927143605193821L

Serialized Fields

bandwidth

double bandwidth

The bandwidth parameter: when computing the loess fit at a particular point, this fraction of source points closest to the current point is taken into account for computing a least-squares regression.

A sensible value is usually 0.25 to 0.5.

robustnessIters

int robustnessIters

The number of robustness iterations parameter: this many robustness iterations are done.

A sensible value is usually 0 (just the initial fit without any robustness iterations) to 4.

accuracy

double accuracy

If the median residual at a certain robustness iteration is less than this amount, no more iterations are done.

Class org.apache.commons.math3.analysis.interpolation.NevilleInterpolator extends Object implements Serializable

serialVersionUID: 3003707660147873733L

Package org.apache.commons.math3.analysis.polynomials

Class org.apache.commons.math3.analysis.polynomials.FourierSeries extends Object implements Serializable

serialVersionUID: -669438626664714658L

Serialized Fields

angularFrequency

double angularFrequency

angular frequency

constant

double constant

a0 coefficient

cosArray

double[] cosArray

a coefficients

sinArray

double[] sinArray

b coefficients

degree

int degree

degree of polynomial

Class org.apache.commons.math3.analysis.polynomials.FourierSeriesApproximation extends Object implements Serializable

serialVersionUID: 173810426201847455L

Serialized Fields

function

UnivariateFunction function

Original function

fourier

FourierSeries fourier

Fourier series approximation

Class org.apache.commons.math3.analysis.polynomials.PolynomialFunction extends Object implements Serializable

serialVersionUID: -7726511984200295583L

Serialized Fields

coefficients

double[] coefficients

The coefficients of the polynomial, ordered by degree -- i.e., coefficients[0] is the constant term and coefficients[n] is the coefficient of x^n where n is the degree of the polynomial.

Class org.apache.commons.math3.analysis.polynomials.TrigonometricPolynomialFunction extends Object implements Serializable

serialVersionUID: -7735389592574470960L

Serialized Fields

a0

double a0

a0 coefficient

a

double[] a

a coefficients

b

double[] b

b coefficients

degree

int degree

degree of polynomial

Class org.apache.commons.math3.analysis.polynomials.TrigonometricPolynomialPrimitive extends Object implements Serializable

serialVersionUID: -199931044622539474L

Serialized Fields

triPolynomial

TrigonometricPolynomialFunction triPolynomial

Trigonometric Polynomial part

linPolynomial

PolynomialFunction linPolynomial

Linear Polynomial part

Package org.apache.commons.math3.complex

Class org.apache.commons.math3.complex.Complex extends Object implements Serializable

serialVersionUID: -6195664516687396620L

Serialization Methods

readResolve

protected final Object readResolve()

Resolve the transient fields in a deserialized Complex Object. Subclasses will need to override Complex.createComplex(double, double) to deserialize properly.

Since:: 2.0

Serialized Fields

imaginary

double imaginary

The imaginary part.

real

double real

The real part.

Class org.apache.commons.math3.complex.ComplexField extends Object implements Serializable

serialVersionUID: -6130362688700788798L

Serialization Methods

readResolve

private Object readResolve()

Handle deserialization of the singleton.

Class org.apache.commons.math3.complex.Quaternion extends Object implements Serializable

serialVersionUID: 20092012L

Serialized Fields

q0

double q0

First component (scalar part).

q1

double q1

Second component (first vector part).

q2

double q2

Third component (second vector part).

q3

double q3

Fourth component (third vector part).

Class org.apache.commons.math3.complex.RootsOfUnity extends Object implements Serializable

serialVersionUID: 20120201L

Serialized Fields

omegaCount

int omegaCount

Number of roots of unity.

omegaReal

double[] omegaReal

Real part of the roots.

omegaImaginaryCounterClockwise

double[] omegaImaginaryCounterClockwise

Imaginary part of the n-th roots of unity, for positive values of n. In this array, the roots are stored in counter-clockwise order.

omegaImaginaryClockwise

double[] omegaImaginaryClockwise

Imaginary part of the n-th roots of unity, for negative values of n. In this array, the roots are stored in clockwise order.

isCounterClockWise

boolean isCounterClockWise

true if RootsOfUnity.computeRoots(int) was called with a positive value of its argument n. In this case, counter-clockwise ordering of the roots of unity should be used.

Package org.apache.commons.math3.distribution

Class org.apache.commons.math3.distribution.AbstractIntegerDistribution extends Object implements Serializable

serialVersionUID: -1146319659338487221L

Serialized Fields

randomData

RandomDataImpl randomData

Deprecated. As of 3.1, to be removed in 4.0. Please use the AbstractIntegerDistribution.random instance variable instead.

RandomData instance used to generate samples from the distribution.

random

RandomGenerator random

RNG instance used to generate samples from the distribution.

Since:: 3.1

Class org.apache.commons.math3.distribution.AbstractRealDistribution extends Object implements Serializable

serialVersionUID: -38038050983108802L

Serialized Fields

randomData

RandomDataImpl randomData

Deprecated. As of 3.1, to be removed in 4.0. Please use the AbstractRealDistribution.random instance variable instead.

RandomData instance used to generate samples from the distribution.

random

RandomGenerator random

RNG instance used to generate samples from the distribution.

Since:: 3.1

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Solver absolute accuracy for inverse cumulative computation

Class org.apache.commons.math3.distribution.BetaDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: -1221965979403477668L

Serialized Fields

alpha

double alpha

First shape parameter.

beta

double beta

Second shape parameter.

z

double z

Normalizing factor used in density computations. updated whenever alpha or beta are changed.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

Class org.apache.commons.math3.distribution.BinomialDistribution extends AbstractIntegerDistribution implements Serializable

serialVersionUID: 6751309484392813623L

Serialized Fields

numberOfTrials

int numberOfTrials

The number of trials.

probabilityOfSuccess

double probabilityOfSuccess

The probability of success.

Class org.apache.commons.math3.distribution.CauchyDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: 8589540077390120676L

Serialized Fields

median

double median

The median of this distribution.

scale

double scale

The scale of this distribution.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy

Class org.apache.commons.math3.distribution.ChiSquaredDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: -8352658048349159782L

Serialized Fields

gamma

GammaDistribution gamma

Internal Gamma distribution.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy

Class org.apache.commons.math3.distribution.ExponentialDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: 2401296428283614780L

Serialized Fields

mean

double mean

The mean of this distribution.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

Class org.apache.commons.math3.distribution.FDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: -8516354193418641566L

Serialized Fields

numeratorDegreesOfFreedom

double numeratorDegreesOfFreedom

The numerator degrees of freedom.

denominatorDegreesOfFreedom

double denominatorDegreesOfFreedom

The numerator degrees of freedom.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

numericalVariance

double numericalVariance

Cached numerical variance

numericalVarianceIsCalculated

boolean numericalVarianceIsCalculated

Whether or not the numerical variance has been calculated

Class org.apache.commons.math3.distribution.GammaDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: 20120524L

Serialized Fields

shape

double shape

The shape parameter.

scale

double scale

The scale parameter.

shiftedShape

double shiftedShape

The constant value of shape + g + 0.5, where g is the Lanczos constant Gamma.LANCZOS_G.

densityPrefactor1

double densityPrefactor1

The constant value of shape / scale * sqrt(e / (2 * pi * (shape + g + 0.5))) / L(shape), where L(shape) is the Lanczos approximation returned by Gamma.lanczos(double). This prefactor is used in GammaDistribution.density(double), when no overflow occurs with the natural calculation.

densityPrefactor2

double densityPrefactor2

The constant value of shape * sqrt(e / (2 * pi * (shape + g + 0.5))) / L(shape), where L(shape) is the Lanczos approximation returned by Gamma.lanczos(double). This prefactor is used in GammaDistribution.density(double), when overflow occurs with the natural calculation.

minY

double minY

Lower bound on y = x / scale for the selection of the computation method in GammaDistribution.density(double). For y <= minY, the natural calculation overflows.

maxLogY

double maxLogY

Upper bound on log(y) (y = x / scale) for the selection of the computation method in GammaDistribution.density(double). For log(y) >= maxLogY, the natural calculation overflows.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

Class org.apache.commons.math3.distribution.HypergeometricDistribution extends AbstractIntegerDistribution implements Serializable

serialVersionUID: -436928820673516179L

Serialized Fields

numberOfSuccesses

int numberOfSuccesses

The number of successes in the population.

populationSize

int populationSize

The population size.

sampleSize

int sampleSize

The sample size.

numericalVariance

double numericalVariance

Cached numerical variance

numericalVarianceIsCalculated

boolean numericalVarianceIsCalculated

Whether or not the numerical variance has been calculated

Class org.apache.commons.math3.distribution.KolmogorovSmirnovDistribution extends Object implements Serializable

serialVersionUID: -4670676796862967187L

Serialized Fields

n

int n

Number of observations.

Class org.apache.commons.math3.distribution.LogNormalDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: 20120112L

Serialized Fields

scale

double scale

The scale parameter of this distribution.

shape

double shape

The shape parameter of this distribution.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

Class org.apache.commons.math3.distribution.NormalDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: 8589540077390120676L

Serialized Fields

mean

double mean

Mean of this distribution.

standardDeviation

double standardDeviation

Standard deviation of this distribution.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

Class org.apache.commons.math3.distribution.PascalDistribution extends AbstractIntegerDistribution implements Serializable

serialVersionUID: 6751309484392813623L

Serialized Fields

numberOfSuccesses

int numberOfSuccesses

The number of successes.

probabilityOfSuccess

double probabilityOfSuccess

The probability of success.

Class org.apache.commons.math3.distribution.PoissonDistribution extends AbstractIntegerDistribution implements Serializable

serialVersionUID: -3349935121172596109L

Serialized Fields

normal

NormalDistribution normal

Distribution used to compute normal approximation.

exponential

ExponentialDistribution exponential

Distribution needed for the PoissonDistribution.sample() method.

mean

double mean

Mean of the distribution.

maxIterations

int maxIterations

Maximum number of iterations for cumulative probability. Cumulative probabilities are estimated using either Lanczos series approximation of Gamma.regularizedGammaP(double, double, double, int) or continued fraction approximation of Gamma.regularizedGammaQ(double, double, double, int).

epsilon

double epsilon

Convergence criterion for cumulative probability.

Class org.apache.commons.math3.distribution.TDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: -5852615386664158222L

Serialized Fields

degreesOfFreedom

double degreesOfFreedom

The degrees of freedom.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

Class org.apache.commons.math3.distribution.TriangularDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: 20120112L

Serialized Fields

a

double a

Lower limit of this distribution (inclusive).

b

double b

Upper limit of this distribution (inclusive).

c

double c

Mode of this distribution.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

Class org.apache.commons.math3.distribution.UniformIntegerDistribution extends AbstractIntegerDistribution implements Serializable

serialVersionUID: 20120109L

Serialized Fields

lower

int lower

Lower bound (inclusive) of this distribution.

upper

int upper

Upper bound (inclusive) of this distribution.

Class org.apache.commons.math3.distribution.UniformRealDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: 20120109L

Serialized Fields

lower

double lower

Lower bound of this distribution (inclusive).

upper

double upper

Upper bound of this distribution (exclusive).

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

Class org.apache.commons.math3.distribution.WeibullDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: 8589540077390120676L

Serialized Fields

shape

double shape

The shape parameter.

scale

double scale

The scale parameter.

solverAbsoluteAccuracy

double solverAbsoluteAccuracy

Inverse cumulative probability accuracy.

numericalMean

double numericalMean

Cached numerical mean

numericalMeanIsCalculated

boolean numericalMeanIsCalculated

Whether or not the numerical mean has been calculated

numericalVariance

double numericalVariance

Cached numerical variance

numericalVarianceIsCalculated

boolean numericalVarianceIsCalculated

Whether or not the numerical variance has been calculated

Class org.apache.commons.math3.distribution.ZipfDistribution extends AbstractIntegerDistribution implements Serializable

serialVersionUID: -140627372283420404L

Serialized Fields

numberOfElements

int numberOfElements

Number of elements.

exponent

double exponent

Exponent parameter of the distribution.

numericalMean

double numericalMean

Cached numerical mean

numericalMeanIsCalculated

boolean numericalMeanIsCalculated

Whether or not the numerical mean has been calculated

numericalVariance

double numericalVariance

Cached numerical variance

numericalVarianceIsCalculated

boolean numericalVarianceIsCalculated

Whether or not the numerical variance has been calculated

Package org.apache.commons.math3.exception

Class org.apache.commons.math3.exception.ConvergenceException extends MathIllegalStateException implements Serializable

serialVersionUID: 4330003017885151975L

Class org.apache.commons.math3.exception.DimensionMismatchException extends MathIllegalNumberException implements Serializable

serialVersionUID: -8415396756375798143L

Serialized Fields

dimension

int dimension

Correct dimension.

Class org.apache.commons.math3.exception.MathArithmeticException extends ArithmeticException implements Serializable

serialVersionUID: -6024911025449780478L

Serialized Fields

context

ExceptionContext context

Context.

Class org.apache.commons.math3.exception.MathIllegalArgumentException extends IllegalArgumentException implements Serializable

serialVersionUID: -6024911025449780478L

Serialized Fields

context

ExceptionContext context

Context.

Class org.apache.commons.math3.exception.MathIllegalNumberException extends MathIllegalArgumentException implements Serializable

serialVersionUID: -7447085893598031110L

Serialized Fields

argument

Number argument

Requested.

Class org.apache.commons.math3.exception.MathIllegalStateException extends IllegalStateException implements Serializable

serialVersionUID: -6024911025449780478L

Serialized Fields

context

ExceptionContext context

Context.

Class org.apache.commons.math3.exception.MathInternalError extends MathIllegalStateException implements Serializable

serialVersionUID: -6276776513966934846L

Class org.apache.commons.math3.exception.MathParseException extends MathIllegalStateException implements Serializable

serialVersionUID: -6024911025449780478L

Class org.apache.commons.math3.exception.MathRuntimeException extends RuntimeException implements Serializable

serialVersionUID: 20120926L

Serialized Fields

context

ExceptionContext context

Context.

Class org.apache.commons.math3.exception.MathUnsupportedOperationException extends UnsupportedOperationException implements Serializable

serialVersionUID: -6024911025449780478L

Serialized Fields

context

ExceptionContext context

Context.

Class org.apache.commons.math3.exception.MaxCountExceededException extends MathIllegalStateException implements Serializable

serialVersionUID: 4330003017885151975L

Serialized Fields

max

Number max

Maximum number of evaluations.

Class org.apache.commons.math3.exception.MultiDimensionMismatchException extends MathIllegalArgumentException implements Serializable

serialVersionUID: -8415396756375798143L

Serialized Fields

wrong

Integer[] wrong

Wrong dimensions.

expected

Integer[] expected

Correct dimensions.

Class org.apache.commons.math3.exception.NoBracketingException extends MathIllegalArgumentException implements Serializable

serialVersionUID: -3629324471511904459L

Serialized Fields

lo

double lo

Lower end of the interval.

hi

double hi

Higher end of the interval.

fLo

double fLo

Value at lower end of the interval.

fHi

double fHi

Value at higher end of the interval.

Class org.apache.commons.math3.exception.NoDataException extends MathIllegalArgumentException implements Serializable

serialVersionUID: -3629324471511904459L

Class org.apache.commons.math3.exception.NonMonotonicSequenceException extends MathIllegalNumberException implements Serializable

serialVersionUID: 3596849179428944575L

Serialized Fields

direction

MathArrays.OrderDirection direction

Direction (positive for increasing, negative for decreasing).

strict

boolean strict

Whether the sequence must be strictly increasing or decreasing.

index

int index

Index of the wrong value.

Number previous

Previous value.

Class org.apache.commons.math3.exception.NotANumberException extends MathIllegalNumberException implements Serializable

serialVersionUID: 20120906L

Class org.apache.commons.math3.exception.NotFiniteNumberException extends MathIllegalNumberException implements Serializable

serialVersionUID: -6100997100383932834L

Class org.apache.commons.math3.exception.NotPositiveException extends NumberIsTooSmallException implements Serializable

serialVersionUID: -2250556892093726375L

Class org.apache.commons.math3.exception.NotStrictlyPositiveException extends NumberIsTooSmallException implements Serializable

serialVersionUID: -7824848630829852237L

Class org.apache.commons.math3.exception.NullArgumentException extends MathIllegalArgumentException implements Serializable

serialVersionUID: -6024911025449780478L

Class org.apache.commons.math3.exception.NumberIsTooLargeException extends MathIllegalNumberException implements Serializable

serialVersionUID: 4330003017885151975L

Serialized Fields

max

Number max

Higher bound.

boundIsAllowed

boolean boundIsAllowed

Whether the maximum is included in the allowed range.

Class org.apache.commons.math3.exception.NumberIsTooSmallException extends MathIllegalNumberException implements Serializable

serialVersionUID: -6100997100383932834L

Serialized Fields

min

Number min

Higher bound.

boundIsAllowed

boolean boundIsAllowed

Whether the maximum is included in the allowed range.

Class org.apache.commons.math3.exception.OutOfRangeException extends MathIllegalNumberException implements Serializable

serialVersionUID: 111601815794403609L

Serialized Fields

lo

Number lo

Lower bound.

hi

Number hi

Higher bound.

Class org.apache.commons.math3.exception.TooManyEvaluationsException extends MaxCountExceededException implements Serializable

serialVersionUID: 4330003017885151975L

Class org.apache.commons.math3.exception.TooManyIterationsException extends MaxCountExceededException implements Serializable

serialVersionUID: 20121211L

Class org.apache.commons.math3.exception.ZeroException extends MathIllegalNumberException implements Serializable

serialVersionUID: -1960874856936000015L

Package org.apache.commons.math3.exception.util

Class org.apache.commons.math3.exception.util.DummyLocalizable extends Object implements Serializable

serialVersionUID: 8843275624471387299L

Serialized Fields

source

String source

Source string.

Class org.apache.commons.math3.exception.util.ExceptionContext extends Object implements Serializable

serialVersionUID: -6024911025449780478L

Serialization Methods

readObject

private void readObject(ObjectInputStream in)
                 throws IOException,
                        ClassNotFoundException

Deserialize this object from the given stream.

Throws:: IOException - This should never happen.; ClassNotFoundException - This should never happen.

writeObject

private void writeObject(ObjectOutputStream out)
                  throws IOException

Serialize this object to the given stream.

Throws:: IOException - This should never happen.

Serialized Fields

throwable

Throwable throwable

The throwable to which this context refers to.

msgPatterns

List<E> msgPatterns

Various informations that enrich the informative message.

msgArguments

List<E> msgArguments

Various informations that enrich the informative message. The arguments will replace the corresponding place-holders in ExceptionContext.msgPatterns.

context

Map<K,V> context

Arbitrary context information.

Package org.apache.commons.math3.fitting

Class org.apache.commons.math3.fitting.WeightedObservedPoint extends Object implements Serializable

serialVersionUID: 5306874947404636157L

Serialized Fields

weight

double weight

Weight of the measurement in the fitting process.

x

double x

Abscissa of the point.

y

double y

Observed value of the function at x.

Package org.apache.commons.math3.fraction

Class org.apache.commons.math3.fraction.AbstractFormat extends NumberFormat implements Serializable

serialVersionUID: -6981118387974191891L

Serialized Fields

denominatorFormat

NumberFormat denominatorFormat

The format used for the denominator.

numeratorFormat

NumberFormat numeratorFormat

The format used for the numerator.

Class org.apache.commons.math3.fraction.BigFraction extends Number implements Serializable

serialVersionUID: -5630213147331578515L

Serialized Fields

numerator

BigInteger numerator

The numerator.

denominator

BigInteger denominator

The denominator.

Class org.apache.commons.math3.fraction.BigFractionField extends Object implements Serializable

serialVersionUID: -1699294557189741703L

Serialization Methods

readResolve

private Object readResolve()

Handle deserialization of the singleton.

Class org.apache.commons.math3.fraction.BigFractionFormat extends AbstractFormat implements Serializable

serialVersionUID: -2932167925527338976L

Class org.apache.commons.math3.fraction.Fraction extends Number implements Serializable

serialVersionUID: 3698073679419233275L

Serialized Fields

denominator

int denominator

The denominator.

numerator

int numerator

The numerator.

Class org.apache.commons.math3.fraction.FractionConversionException extends ConvergenceException implements Serializable

serialVersionUID: -4661812640132576263L

Class org.apache.commons.math3.fraction.FractionField extends Object implements Serializable

serialVersionUID: -1257768487499119313L

Serialization Methods

readResolve

private Object readResolve()

Handle deserialization of the singleton.

Class org.apache.commons.math3.fraction.FractionFormat extends AbstractFormat implements Serializable

serialVersionUID: 3008655719530972611L

Class org.apache.commons.math3.fraction.ProperBigFractionFormat extends BigFractionFormat implements Serializable

serialVersionUID: -6337346779577272307L

Serialized Fields

wholeFormat

NumberFormat wholeFormat

The format used for the whole number.

Class org.apache.commons.math3.fraction.ProperFractionFormat extends FractionFormat implements Serializable

serialVersionUID: 760934726031766749L

Serialized Fields

wholeFormat

NumberFormat wholeFormat

The format used for the whole number.

Package org.apache.commons.math3.genetics

Class org.apache.commons.math3.genetics.InvalidRepresentationException extends MathIllegalArgumentException implements Serializable

serialVersionUID: 1L

Package org.apache.commons.math3.geometry

Package org.apache.commons.math3.geometry.euclidean.oned

Class org.apache.commons.math3.geometry.euclidean.oned.Euclidean1D extends Object implements Serializable

serialVersionUID: -1178039568877797126L

Serialization Methods

readResolve

private Object readResolve()

Handle deserialization of the singleton.

Class org.apache.commons.math3.geometry.euclidean.oned.Vector1D extends Object implements Serializable

serialVersionUID: 7556674948671647925L

Serialized Fields

x

double x

Abscissa.

Package org.apache.commons.math3.geometry.euclidean.threed

Class org.apache.commons.math3.geometry.euclidean.threed.AbstractEllipse extends Object implements Serializable

serialVersionUID: 2542698102987576947L

Serialized Fields

center

Vector3D center

position of the center

centerTab

double[] centerTab

position of the center in doubles

normal

Vector3D normal

normal to the plane containing the ellipse

normalTab

double[] normalTab

normal to the plane containing the ellipse in doubles

radiusA

double radiusA

radius on the U axis of the local frame

radiusB

double radiusB

radius on the V axis of the local frame

u

Vector3D u

U vector of the local frame

uTab

double[] uTab

U vector of the local frame in doubles

v

Vector3D v

V vector of the local frame

vTab

double[] vTab

V vector of the local frame in doubles

pointsToTest

Vector3D[] pointsToTest

first four points to test in iterative algorithms

Class org.apache.commons.math3.geometry.euclidean.threed.Disk extends AbstractEllipse implements Serializable

serialVersionUID: 9040808229741425729L

Class org.apache.commons.math3.geometry.euclidean.threed.Ellipse extends AbstractEllipse implements Serializable

serialVersionUID: 9047708229741235629L

Class org.apache.commons.math3.geometry.euclidean.threed.Ellipsoid extends Object implements Serializable

serialVersionUID: 8950995549840576381L

Serialized Fields

epsNewton

double epsNewton

Epsilon for Newton algorithm.

position

Vector3D position

Ellipsoid center position

ellipsoidX

Vector3D ellipsoidX

Ellipsoid X-axis in standard basis

ellipsoidY

Vector3D ellipsoidY

Ellipsoid Y-axis in standard basis

ellipsoidZ

Vector3D ellipsoidZ

Ellipsoid axis of revolution in standard basis

a

double a

Ellipsoid semi-axis a (in plan orthogonal to axis of revolution)

b

double b

Ellipsoid semi-axis b (in plan orthogonal to axis of revolution)

c

double c

Ellipsoid semi-axis c (along ellipsoids axis of revolution)

a2

double a2

Ellipsoid semi-axis a to the power of 2

b2

double b2

Ellipsoid semi-axis b to the power of 2

c2

double c2

Ellipsoid semi-axis c to the power of 2

standardBasisTransform

Matrix3D standardBasisTransform

Ellipsoid basis of local

localBasisTransform

Matrix3D localBasisTransform

Ellipsoid inverted basis of local

smallest

org.apache.commons.math3.geometry.euclidean.threed.Ellipsoid.SmallestAxis smallest

Smallest axis

an

double an

Normalized ellipsoid semi-axis a (in plan orthogonal to axis of revolution)

bn

double bn

Normalized ellipsoid semi-axis b (in plan orthogonal to axis of revolution)

cn

double cn

Normalized ellipsoid semi-axis c (along ellipsoids axis of revolution)

a2n

double a2n

Normalized ellipsoid semi-axis a to the power of 2

b2n

double b2n

Normalized ellipsoid semi-axis b to the power of 2

c2n

double c2n

Normalized ellipsoid semi-axis c to the power of 2

normFactor

double normFactor

Normalized ellipsoid norm factor (average of [a, b, c])

Class org.apache.commons.math3.geometry.euclidean.threed.EllipticCone extends Object implements Serializable

serialVersionUID: 8807976486767394008L

Serialized Fields

height

double height

length of the cone on its axis

infiniteCone

InfiniteEllipticCone infiniteCone

The associated infinite cone

upEllipse

Ellipse upEllipse

the ending ellipse

origin

Vector3D origin

Position of the origin of the axis

direction

Vector3D direction

Direction of the axis, defines the orientation : Z of the local frame

u

Vector3D u

U vector of the local frame

v

Vector3D v

V vector of the local frame

Class org.apache.commons.math3.geometry.euclidean.threed.EllipticCylinder extends Object implements Serializable

serialVersionUID: 9040808449742261729L

Serialized Fields

height

double height

length of the cone on its axis

radiusA

double radiusA

radius on U axis

radiusB

double radiusB

radius on V axis

infiniteCylinder

InfiniteEllipticCylinder infiniteCylinder

The associated infinite cone

upEllipse

Ellipse upEllipse

the up ending ellipse

bottomEllipse

Ellipse bottomEllipse

the bottom ending ellipse

origin

Vector3D origin

Position of the origin of the axis

direction

Vector3D direction

Direction of the axis, defines the orientation : Z of the local frame

u

Vector3D u

U vector of the local frame

v

Vector3D v

V vector of the local frame

Class org.apache.commons.math3.geometry.euclidean.threed.Euclidean3D extends Object implements Serializable

serialVersionUID: 6249091865814886817L

Serialization Methods

readResolve

private Object readResolve()

Handle deserialization of the singleton.

Class org.apache.commons.math3.geometry.euclidean.threed.FieldRotation extends Object implements Serializable

serialVersionUID: 20130224L

Serialized Fields

q0

RealFieldElement<T> q0

Scalar coordinate of the quaternion.

q1

RealFieldElement<T> q1

First coordinate of the vectorial part of the quaternion.

q2

RealFieldElement<T> q2

Second coordinate of the vectorial part of the quaternion.

q3

RealFieldElement<T> q3

Third coordinate of the vectorial part of the quaternion.

Class org.apache.commons.math3.geometry.euclidean.threed.FieldVector3D extends Object implements Serializable

serialVersionUID: 20130224L

Serialized Fields

x

RealFieldElement<T> x

Abscissa.

y

RealFieldElement<T> y

Ordinate.

z

RealFieldElement<T> z

Height.

Class org.apache.commons.math3.geometry.euclidean.threed.InfiniteEllipticCone extends Object implements Serializable

serialVersionUID: -7542518748306042613L

Serialized Fields

origin

Vector3D origin

Position of origin

localX

Vector3D localX

local X-axis

localY

Vector3D localY

local Y-axis

localZ

Vector3D localZ

local Z-axis

alpha

double alpha

angle along X axis

beta

double beta

angle along Y axis

ta

double ta

tangeant of alpha

tb

double tb

tangeant of beta

standardBasisTransform

Matrix3D standardBasisTransform

Transformation Matrix to standard basis

localBasisTransform

Matrix3D localBasisTransform

Transformation Matrix to local cone basis

Class org.apache.commons.math3.geometry.euclidean.threed.InfiniteEllipticCylinder extends Object implements Serializable

serialVersionUID: -4454479846241988517L

Serialized Fields

origin

Vector3D origin

point of cylinders' axis

localX

Vector3D localX

local X-axis

localY

Vector3D localY

local Y-axis

localZ

Vector3D localZ

local Z-axis (Cylinder axis)

a

double a

Semi axis along X axis

b

double b

Semi axis along Y axis

standardBasisTransform

Matrix3D standardBasisTransform

Transformation Matrix to standard basis

localBasisTransform

Matrix3D localBasisTransform

Transformation Matrix to local cone basis

Class org.apache.commons.math3.geometry.euclidean.threed.InfiniteRectangleCone extends Object implements Serializable

serialVersionUID: -2908830751652223671L

Serialized Fields

origin

Vector3D origin

Position of the origin of the cone

originDoubles

double[] originDoubles

Position of the origin of the cone in doubles

axis

Vector3D axis

Axis of the cone, defines its orientation : Z of the local frame

u

Vector3D u

U vector of the local frame

v

Vector3D v

V vector of the local frame

angleU

double angleU

angle on the U axis

angleV

double angleV

angle on the U axis

sideAxis

Vector3D[] sideAxis

Side axis

sideAxisDoubles

double[][] sideAxisDoubles

Side axis in doubles

sideNormal

Vector3D[] sideNormal

Side normal vectors

sideNormalDoubles

double[][] sideNormalDoubles

Side normal vectors in doubles

rotationMatrix

Matrix3D rotationMatrix

rotation matrix to the local frame

Class org.apache.commons.math3.geometry.euclidean.threed.InfiniteRightCircularCone extends Object implements Serializable

serialVersionUID: -6525651616917874512L

Serialized Fields

origin

Vector3D origin

Position of the origin of the cone

axis

Vector3D axis

Axis of the cone, defines its orientation : Z of the local frame

angle

double angle

Half angle of the cone

tan

double tan

tangent of the angle

sin

double sin

sine of the angle

u

Vector3D u

U vector of the local frame

v

Vector3D v

V vector of the local frame

rotationMatrix

Matrix3D rotationMatrix

rotation matrix to the local frame

Class org.apache.commons.math3.geometry.euclidean.threed.InfiniteRightCircularCylinder extends Object implements Serializable

serialVersionUID: -5163863575805965884L

Serialized Fields

origin

Vector3D origin

Position of the origin of the axis

direction

Vector3D direction

Direction of the axis, defines the orientation : Z of the local frame

originDoubles

double[] originDoubles

Position of the origin of the axis

directionDoubles

double[] directionDoubles

Direction of the axis, defines the orientation : Z of the local frame

radius

double radius

Radius of the cylinder

u

Vector3D u

U vector of the local frame

v

Vector3D v

V vector of the local frame

rotationMatrix

Matrix3D rotationMatrix

rotation matrix to the local frame

Class org.apache.commons.math3.geometry.euclidean.threed.LineSegment extends Object implements Serializable

serialVersionUID: 9192006834483139397L

Serialized Fields

origin

Vector3D origin

Position of the origin of the segment

end

Vector3D end

Position of the end of the segment

length

double length

Length of the segment

direction

Vector3D direction

Direction of the cone, defines its orientation : Z of the local frame

Class org.apache.commons.math3.geometry.euclidean.threed.Matrix3D extends Object implements Serializable

serialVersionUID: -451912259186366524L

Serialized Fields

data

double[][] data

Entries of the matrix.

Class org.apache.commons.math3.geometry.euclidean.threed.NotARotationMatrixException extends MathIllegalArgumentException implements Serializable

serialVersionUID: 5647178478658937642L

Class org.apache.commons.math3.geometry.euclidean.threed.Parallelepiped extends Object implements Serializable

serialVersionUID: 7729404150529575478L

Serialized Fields

center

Vector3D center

Position of the center of the parallelepiped

u

Vector3D u

U vector of the Frame

v

Vector3D v

V vector of the Frame

w

Vector3D w

W vector of the Frame

length

double length

Dimension in the u direction

width

double width

Dimension in the v direction

height

double height

Dimension in the w direction

corners

Vector3D[] corners

Corners of the rectangle

faces

Plate[] faces

The face 1

Class org.apache.commons.math3.geometry.euclidean.threed.Plate extends Object implements Serializable

serialVersionUID: -3489518699224406794L

Serialized Fields

center

Vector3D center

Position of the center of the plate

centerTab

double[] centerTab

Position of the center of the plate as doubles

u

Vector3D u

U vector of the Frame

uTab

double[] uTab

U vector of the Frame as doubles

v

Vector3D v

V vector of the Frame

vTab

double[] vTab

V vector of the Frame as doubles

w

Vector3D w

W vector of the Frame

wTab

double[] wTab

W vector of the Frame as doubles

length

double length

Dimension in the u direction

width

double width

Dimension in the v direction

corners

Vector3D[] corners

Corners of the rectangle

edges

LineSegment[] edges

Edges of the rectangle

Class org.apache.commons.math3.geometry.euclidean.threed.RectangleCone extends Object implements Serializable

serialVersionUID: -617787590801253864L

Serialized Fields

origin

Vector3D origin

Position of the origin of the cone

height

double height

Height of the cone on its axis

length

double length

Length of the cone's basis (U axis)

width

double width

Width of the cone's basis (U axis)

direction

Vector3D direction

Direction of the cone, defines its orientation : Z of the local frame

u

Vector3D u

U vector of the local frame

v

Vector3D v

V vector of the local frame

infiniteCone

InfiniteRectangleCone infiniteCone

The associated infinite cone

endingPlate

Plate endingPlate

The ending plate

edges

LineSegment[] edges

Edges of the pyramid

edgesDirections

Vector3D[] edgesDirections

Edges' directions

rotationMatrix

Matrix3D rotationMatrix

rotation matrix to the local frame

Class org.apache.commons.math3.geometry.euclidean.threed.RightCircularCone extends Object implements Serializable

serialVersionUID: -6204155105548567293L

Serialized Fields

height

double height

height of the cone on its axis

infiniteCone

InfiniteRightCircularCone infiniteCone

The associated infinite cone

upDisk

Disk upDisk

the ending disk

origin

Vector3D origin

Position of the origin of the axis

direction

Vector3D direction

Direction of the axis, defines the orientation : Z of the local frame

angle

double angle

Angle of the cone

tan

double tan

tangent of the angle

cos

double cos

cosine of the angle

sin

double sin

sine of the angle

u

Vector3D u

U vector of the local frame

v

Vector3D v

V vector of the local frame

rotationMatrix

Matrix3D rotationMatrix

rotation matrix to the local frame

Class org.apache.commons.math3.geometry.euclidean.threed.RightCircularCylinder extends Object implements Serializable

serialVersionUID: 4760299772648614616L

Serialized Fields

height

double height

height of the cylinder on its axis

infiniteCylinder

InfiniteRightCircularCylinder infiniteCylinder

The associated infinite cylinder

upDisk

Disk upDisk

the up side disk

bottomDisk

Disk bottomDisk

the bottom side disk

origin

Vector3D origin

Position of the origin of the axis

direction

Vector3D direction

Direction of the axis, defines the orientation : Z of the local frame

radius

double radius

Radius of the cylinder

Class org.apache.commons.math3.geometry.euclidean.threed.Rotation extends Object implements Serializable

serialVersionUID: -2153622329907944313L

Serialized Fields

q0

double q0

Scalar coordinate of the quaternion.

q1

double q1

First coordinate of the vectorial part of the quaternion.

q2

double q2

Second coordinate of the vectorial part of the quaternion.

q3

double q3

Third coordinate of the vectorial part of the quaternion.

Class org.apache.commons.math3.geometry.euclidean.threed.Sphere extends Object implements Serializable

serialVersionUID: -7540625758165659580L

Serialized Fields

center

Vector3D center

Position of the center of the sphere

radius

double radius

Radius of the sphere

centerTab

double[] centerTab

Position of the center of the sphere (doubles)

Class org.apache.commons.math3.geometry.euclidean.threed.Spheroid extends Ellipsoid implements Serializable

serialVersionUID: -874292129066116967L

Class org.apache.commons.math3.geometry.euclidean.threed.Vector3D extends Object implements Serializable

serialVersionUID: 1313493323784566947L

Serialized Fields

x

double x

Abscissa.

y

double y

Ordinate.

z

double z

Height.

Package org.apache.commons.math3.geometry.euclidean.twod

Class org.apache.commons.math3.geometry.euclidean.twod.Euclidean2D extends Object implements Serializable

serialVersionUID: 4793432849757649566L

Serialization Methods

readResolve

private Object readResolve()

Handle deserialization of the singleton.

Class org.apache.commons.math3.geometry.euclidean.twod.Vector2D extends Object implements Serializable

serialVersionUID: 266938651998679754L

Serialized Fields

x

double x

Abscissa.

y

double y

Ordinate.

Package org.apache.commons.math3.linear

Class org.apache.commons.math3.linear.Array2DRowFieldMatrix extends AbstractFieldMatrix<T extends FieldElement<T>> implements Serializable

serialVersionUID: 7260756672015356458L

Serialized Fields

data

FieldElement<T>[][] data

Entries of the matrix

Class org.apache.commons.math3.linear.Array2DRowRealMatrix extends AbstractRealMatrix implements Serializable

serialVersionUID: -1067294169172445528L

Serialized Fields

data

double[][] data

Entries of the matrix.

Class org.apache.commons.math3.linear.ArrayFieldVector extends Object implements Serializable

serialVersionUID: 7648186910365927050L

Serialized Fields

data

FieldElement<T>[] data

Entries of the vector.

field

Field<T> field

Field to which the elements belong.

Class org.apache.commons.math3.linear.ArrayRealVector extends RealVector implements Serializable

serialVersionUID: -1097961340710804027L

Serialized Fields

data

double[] data

Entries of the vector.

Class org.apache.commons.math3.linear.BlockFieldMatrix extends AbstractFieldMatrix<T extends FieldElement<T>> implements Serializable

serialVersionUID: -4602336630143123183L

Serialized Fields

blocks

FieldElement<T>[][] blocks

Blocks of matrix entries.

rows

int rows

Number of rows of the matrix.

columns

int columns

Number of columns of the matrix.

blockRows

int blockRows

Number of block rows of the matrix.

blockColumns

int blockColumns

Number of block columns of the matrix.

Class org.apache.commons.math3.linear.BlockRealMatrix extends AbstractRealMatrix implements Serializable

serialVersionUID: 4991895511313664478L

Serialized Fields

blocks

double[][] blocks

Blocks of matrix entries.

rows

int rows

Number of rows of the matrix.

columns

int columns

Number of columns of the matrix.

blockRows

int blockRows

Number of block rows of the matrix.

blockColumns

int blockColumns

Number of block columns of the matrix.

Class org.apache.commons.math3.linear.DefaultIterativeLinearSolverEvent extends IterativeLinearSolverEvent implements Serializable

serialVersionUID: 20120129L

Serialized Fields

b

RealVector b

The right-hand side vector.

r

RealVector r

The current estimate of the residual.

rnorm

double rnorm

The current estimate of the norm of the residual.

x

RealVector x

The current estimate of the solution.

Class org.apache.commons.math3.linear.DiagonalMatrix extends AbstractRealMatrix implements Serializable

serialVersionUID: 20121229L

Serialized Fields

data

double[] data

Entries of the diagonal.

Class org.apache.commons.math3.linear.IllConditionedOperatorException extends MathIllegalArgumentException implements Serializable

serialVersionUID: -7883263944530490135L

Class org.apache.commons.math3.linear.IterativeLinearSolverEvent extends IterationEvent implements Serializable

serialVersionUID: 20120129L

Class org.apache.commons.math3.linear.MatrixDimensionMismatchException extends MultiDimensionMismatchException implements Serializable

serialVersionUID: -8415396756375798143L

Class org.apache.commons.math3.linear.NonPositiveDefiniteMatrixException extends NumberIsTooSmallException implements Serializable

serialVersionUID: 1641613838113738061L

Serialized Fields

index

int index

Index (diagonal element).

threshold

double threshold

Threshold.

Class org.apache.commons.math3.linear.NonPositiveDefiniteOperatorException extends MathIllegalArgumentException implements Serializable

serialVersionUID: 917034489420549847L

Class org.apache.commons.math3.linear.NonSelfAdjointOperatorException extends MathIllegalArgumentException implements Serializable

serialVersionUID: 1784999305030258247L

Class org.apache.commons.math3.linear.NonSquareMatrixException extends DimensionMismatchException implements Serializable

serialVersionUID: -660069396594485772L

Class org.apache.commons.math3.linear.NonSquareOperatorException extends DimensionMismatchException implements Serializable

serialVersionUID: -4145007524150846242L

Class org.apache.commons.math3.linear.NonSymmetricMatrixException extends MathIllegalArgumentException implements Serializable

serialVersionUID: -7518495577824189882L

Serialized Fields

row

int row

Row.

column

int column

Column.

threshold

double threshold

Threshold.

Class org.apache.commons.math3.linear.OpenMapRealMatrix extends AbstractRealMatrix implements Serializable

serialVersionUID: -5962461716457143437L

Serialized Fields

rows

int rows

Deprecated.

Number of rows of the matrix.

columns

int columns

Deprecated.

Number of columns of the matrix.

entries

OpenIntToDoubleHashMap entries

Deprecated.

Storage for (sparse) matrix elements.

Class org.apache.commons.math3.linear.OpenMapRealVector extends SparseRealVector implements Serializable

serialVersionUID: 8772222695580707260L

Serialized Fields

entries

OpenIntToDoubleHashMap entries

Deprecated.

Entries of the vector.

virtualSize

int virtualSize

Deprecated.

Dimension of the vector.

epsilon

double epsilon

Deprecated.

Tolerance for having a value considered zero.

Class org.apache.commons.math3.linear.SingularMatrixException extends MathIllegalArgumentException implements Serializable

serialVersionUID: -4206514844735401070L

Class org.apache.commons.math3.linear.SingularOperatorException extends MathIllegalArgumentException implements Serializable

serialVersionUID: -476049978595245033L

Class org.apache.commons.math3.linear.SparseFieldVector extends Object implements Serializable

serialVersionUID: 7841233292190413362L

Serialized Fields

field

Field<T> field

Deprecated.

Field to which the elements belong.

entries

OpenIntToFieldHashMap<T extends FieldElement<T>> entries

Deprecated.

Entries of the vector.

virtualSize

int virtualSize

Deprecated.

Dimension of the vector.

Class org.apache.commons.math3.linear.SymmetricMatrix extends AbstractRealMatrix implements Serializable

serialVersionUID: 4075733948947520081L

Serialized Fields

data

double[] data

Entries of the diagonal.

uplo

SymmetricMatrix.SYMMETRIC uplo

The triangle to be used to create the symmetric matrix.

n

int n

The dimension of the created matrix.

ld

int ld

The leading dimension of the created matrix.

Package org.apache.commons.math3.ode

Class org.apache.commons.math3.ode.ContinuousOutputModel extends Object implements Serializable

serialVersionUID: -1417964919405031606L

Serialized Fields

initialTime

double initialTime

Initial integration time.

finalTime

double finalTime

Final integration time.

forward

boolean forward

Integration direction indicator.

index

int index

Current interpolator index.

steps

List<E> steps

Steps table.

Class org.apache.commons.math3.ode.EquationsMapper extends Object implements Serializable

serialVersionUID: 20110925L

Serialized Fields

firstIndex

int firstIndex

Index of the first equation element in complete state arrays.

dimension

int dimension

Dimension of the secondary state parameters.

Class org.apache.commons.math3.ode.JacobianMatrices.MismatchedEquations extends MathIllegalArgumentException implements Serializable

serialVersionUID: 20120902L

Class org.apache.commons.math3.ode.UnknownParameterException extends MathIllegalArgumentException implements Serializable

serialVersionUID: 20120902L

Serialized Fields

name

String name

Parameter name.

Package org.apache.commons.math3.ode.nonstiff

Class org.apache.commons.math3.ode.nonstiff.RungeKutta6StepInterpolator extends org.apache.commons.math3.ode.nonstiff.RungeKuttaStepInterpolator implements Serializable

Serialization Methods

readExternal

public void readExternal(ObjectInput in)
                  throws IOException,
                         ClassNotFoundException

Throws:: IOException; ClassNotFoundException

writeExternal

public void writeExternal(ObjectOutput out)
                   throws IOException

Throws:: IOException

Package org.apache.commons.math3.ode.sampling

Class org.apache.commons.math3.ode.sampling.AbstractStepInterpolator extends Object implements Serializable

Serialization Methods

readExternal

public abstract void readExternal(ObjectInput in)
                           throws IOException,
                                  ClassNotFoundException

Throws:: IOException; ClassNotFoundException

writeExternal

public abstract void writeExternal(ObjectOutput out)
                            throws IOException

Throws:: IOException

Class org.apache.commons.math3.ode.sampling.NordsieckStepInterpolator extends AbstractStepInterpolator implements Serializable

serialVersionUID: -7179861704951334960L

Serialization Methods

readExternal

public void readExternal(ObjectInput in)
                  throws IOException,
                         ClassNotFoundException

Throws:: IOException; ClassNotFoundException

writeExternal

public void writeExternal(ObjectOutput out)
                   throws IOException

Throws:: IOException

Package org.apache.commons.math3.optim

Class org.apache.commons.math3.optim.PointValuePair extends Pair<double[],Double> implements Serializable

serialVersionUID: 20120513L

Serialization Methods

writeReplace

private Object writeReplace()

Replace the instance with a data transfer object for serialization.

Class org.apache.commons.math3.optim.PointVectorValuePair extends Pair<double[],double[]> implements Serializable

serialVersionUID: 20120513L

Serialization Methods

writeReplace

private Object writeReplace()

Replace the instance with a data transfer object for serialization.

Package org.apache.commons.math3.optim.linear

Class org.apache.commons.math3.optim.linear.LinearConstraint extends Object implements Serializable

serialVersionUID: -764632794033034092L

Serialization Methods

readObject

private void readObject(ObjectInputStream ois)
                 throws ClassNotFoundException,
                        IOException

Deserialize the instance.

Throws:: ClassNotFoundException - if a class in the stream cannot be found; IOException - if object cannot be read from the stream

writeObject

private void writeObject(ObjectOutputStream oos)
                  throws IOException

Serialize the instance.

Throws:: IOException - if object cannot be written to stream

Serialized Fields

relationship

Relationship relationship

Relationship between left and right hand sides (=, <=, >=).

value

double value

Value of the constraint (right hand side).

Class org.apache.commons.math3.optim.linear.LinearObjectiveFunction extends Object implements Serializable

serialVersionUID: -4531815507568396090L

Serialization Methods

readObject

private void readObject(ObjectInputStream ois)
                 throws ClassNotFoundException,
                        IOException

Deserialize the instance.

Throws:: ClassNotFoundException - if a class in the stream cannot be found; IOException - if object cannot be read from the stream

writeObject

private void writeObject(ObjectOutputStream oos)
                  throws IOException

Serialize the instance.

Throws:: IOException - if object cannot be written to stream

Serialized Fields

constantTerm

double constantTerm

Constant term of the linear equation.

Class org.apache.commons.math3.optim.linear.NoFeasibleSolutionException extends MathIllegalStateException implements Serializable

serialVersionUID: -3044253632189082760L

Class org.apache.commons.math3.optim.linear.UnboundedSolutionException extends MathIllegalStateException implements Serializable

serialVersionUID: 940539497277290619L

Package org.apache.commons.math3.optim.univariate

Class org.apache.commons.math3.optim.univariate.UnivariatePointValuePair extends Object implements Serializable

serialVersionUID: 1003888396256744753L

Serialized Fields

point

double point

Point.

value

double value

Value of the objective function at the point.

Package org.apache.commons.math3.optimization

Class org.apache.commons.math3.optimization.PointValuePair extends Pair<double[],Double> implements Serializable

serialVersionUID: 20120513L

Serialization Methods

writeReplace

private Object writeReplace()

Deprecated.

Replace the instance with a data transfer object for serialization.

Class org.apache.commons.math3.optimization.PointVectorValuePair extends Pair<double[],double[]> implements Serializable

serialVersionUID: 20120513L

Serialization Methods

writeReplace

private Object writeReplace()

Deprecated.

Replace the instance with a data transfer object for serialization.

Package org.apache.commons.math3.optimization.fitting

Class org.apache.commons.math3.optimization.fitting.WeightedObservedPoint extends Object implements Serializable

serialVersionUID: 5306874947404636157L

Serialized Fields

weight

double weight

Deprecated.

Weight of the measurement in the fitting process.

x

double x

Deprecated.

Abscissa of the point.

y

double y

Deprecated.

Observed value of the function at x.

Package org.apache.commons.math3.optimization.linear

Class org.apache.commons.math3.optimization.linear.LinearConstraint extends Object implements Serializable

serialVersionUID: -764632794033034092L

Serialization Methods

readObject

private void readObject(ObjectInputStream ois)
                 throws ClassNotFoundException,
                        IOException

Deprecated.

Deserialize the instance.

Throws:: ClassNotFoundException - if a class in the stream cannot be found; IOException - if object cannot be read from the stream

writeObject

private void writeObject(ObjectOutputStream oos)
                  throws IOException

Deprecated.

Serialize the instance.

Throws:: IOException - if object cannot be written to stream

Serialized Fields

relationship

Relationship relationship

Deprecated.

Relationship between left and right hand sides (=, <=, >=).

value

double value

Deprecated.

Value of the constraint (right hand side).

Class org.apache.commons.math3.optimization.linear.LinearObjectiveFunction extends Object implements Serializable

serialVersionUID: -4531815507568396090L

Serialization Methods

readObject

private void readObject(ObjectInputStream ois)
                 throws ClassNotFoundException,
                        IOException

Deprecated.

Deserialize the instance.

Throws:: ClassNotFoundException - if a class in the stream cannot be found; IOException - if object cannot be read from the stream

writeObject

private void writeObject(ObjectOutputStream oos)
                  throws IOException

Deprecated.

Serialize the instance.

Throws:: IOException - if object cannot be written to stream

Serialized Fields

constantTerm

double constantTerm

Deprecated.

Constant term of the linear equation.

Class org.apache.commons.math3.optimization.linear.NoFeasibleSolutionException extends MathIllegalStateException implements Serializable

serialVersionUID: -3044253632189082760L

Class org.apache.commons.math3.optimization.linear.UnboundedSolutionException extends MathIllegalStateException implements Serializable

serialVersionUID: 940539497277290619L

Package org.apache.commons.math3.optimization.univariate

Class org.apache.commons.math3.optimization.univariate.UnivariatePointValuePair extends Object implements Serializable

serialVersionUID: 1003888396256744753L

Serialized Fields

point

double point

Deprecated.

Point.

value

double value

Deprecated.

Value of the objective function at the point.

Package org.apache.commons.math3.random

Class org.apache.commons.math3.random.AbstractWell extends BitsStreamGenerator implements Serializable

serialVersionUID: -817701723016583596L

Serialized Fields

index

int index

Current index in the bytes pool.

v

int[] v

Bytes pool.

iRm1

int[] iRm1

Index indirection table giving for each index its predecessor taking table size into account.

iRm2

int[] iRm2

Index indirection table giving for each index its second predecessor taking table size into account.

i1

int[] i1

Index indirection table giving for each index the value index + m1 taking table size into account.

i2

int[] i2

Index indirection table giving for each index the value index + m2 taking table size into account.

i3

int[] i3

Index indirection table giving for each index the value index + m3 taking table size into account.

Class org.apache.commons.math3.random.BitsStreamGenerator extends Object implements Serializable

serialVersionUID: 20130104L

Serialized Fields

nextGaussian

double nextGaussian

Next gaussian.

Class org.apache.commons.math3.random.EmpiricalDistribution extends AbstractRealDistribution implements Serializable

serialVersionUID: 5729073523949762654L

Serialized Fields

binStats

List<E> binStats

List of SummaryStatistics objects characterizing the bins

sampleStats

SummaryStatistics sampleStats

Sample statistics

max

double max

Max loaded value

min

double min

Min loaded value

delta

double delta

Grid size

binCount

int binCount

number of bins

loaded

boolean loaded

is the distribution loaded?

upperBounds

double[] upperBounds

upper bounds of subintervals in (0,1) "belonging" to the bins

randomData

RandomDataGenerator randomData

RandomDataGenerator instance to use in repeated calls to getNext()

Class org.apache.commons.math3.random.ISAACRandom extends BitsStreamGenerator implements Serializable

serialVersionUID: 7288197941165002400L

Serialized Fields

rsl

int[] rsl

The results given to the user

mem

int[] mem

The internal state

count

int count

Count through the results in rsl[]

isaacA

int isaacA

Accumulator

isaacB

int isaacB

The last result

isaacC

int isaacC

Counter, guarantees cycle is at least 2^40

arr

int[] arr

Service variable.

isaacX

int isaacX

Service variable.

isaacI

int isaacI

Service variable.

isaacJ

int isaacJ

Service variable.

Class org.apache.commons.math3.random.JDKRandomGenerator extends Random implements Serializable

serialVersionUID: -7745277476784028798L

Class org.apache.commons.math3.random.MersenneTwister extends BitsStreamGenerator implements Serializable

serialVersionUID: 8661194735290153518L

Serialized Fields

mt

int[] mt

Bytes pool.

mti

int mti

Current index in the bytes pool.

Class org.apache.commons.math3.random.RandomAdaptor extends Random implements Serializable

serialVersionUID: 2306581345647615033L

Serialized Fields

randomGenerator

RandomGenerator randomGenerator

Wrapped randomGenerator instance

Class org.apache.commons.math3.random.RandomDataGenerator extends Object implements Serializable

serialVersionUID: -626730818244969716L

Serialized Fields

rand

RandomGenerator rand

underlying random number generator

secRand

SecureRandom secRand

underlying secure random number generator

Class org.apache.commons.math3.random.RandomDataImpl extends Object implements Serializable

serialVersionUID: -626730818244969716L

Serialized Fields

delegate

RandomDataGenerator delegate

Deprecated.

RandomDataGenerator delegate

Class org.apache.commons.math3.random.Well1024a extends AbstractWell implements Serializable

serialVersionUID: 5680173464174485492L

Class org.apache.commons.math3.random.Well19937a extends AbstractWell implements Serializable

serialVersionUID: -7462102162223815419L

Class org.apache.commons.math3.random.Well19937c extends AbstractWell implements Serializable

serialVersionUID: -7203498180754925124L

Class org.apache.commons.math3.random.Well44497a extends AbstractWell implements Serializable

serialVersionUID: -3859207588353972099L

Class org.apache.commons.math3.random.Well44497b extends AbstractWell implements Serializable

serialVersionUID: 4032007538246675492L

Class org.apache.commons.math3.random.Well512a extends AbstractWell implements Serializable

serialVersionUID: -6104179812103820574L

Package org.apache.commons.math3.stat

Class org.apache.commons.math3.stat.Frequency extends Object implements Serializable

serialVersionUID: -3845586908418844111L

Serialized Fields

freqTable

TreeMap<K,V> freqTable

underlying collection

Package org.apache.commons.math3.stat.clustering

Class org.apache.commons.math3.stat.clustering.Cluster extends Object implements Serializable

serialVersionUID: -3442297081515880464L

Serialized Fields

points

List<E> points

The points contained in this cluster.

center

Clusterable<T> center

Center of the cluster.

Class org.apache.commons.math3.stat.clustering.EuclideanDoublePoint extends Object implements Serializable

serialVersionUID: 8026472786091227632L

Serialized Fields

point

double[] point

Point coordinates.

Class org.apache.commons.math3.stat.clustering.EuclideanIntegerPoint extends Object implements Serializable

serialVersionUID: 3946024775784901369L

Serialized Fields

point

int[] point

Point coordinates.

Package org.apache.commons.math3.stat.descriptive

Class org.apache.commons.math3.stat.descriptive.AggregateSummaryStatistics extends Object implements Serializable

serialVersionUID: -8207112444016386906L

Serialized Fields

statisticsPrototype

SummaryStatistics statisticsPrototype

A SummaryStatistics serving as a prototype for creating SummaryStatistics contributing to this aggregate

statistics

SummaryStatistics statistics

The SummaryStatistics in which aggregate statistics are accumulated.

Class org.apache.commons.math3.stat.descriptive.DescriptiveStatistics extends Object implements Serializable

serialVersionUID: 4133067267405273064L

Serialized Fields

windowSize

int windowSize

hold the window size

eDA

ResizableDoubleArray eDA

Stored data values

meanImpl

UnivariateStatistic meanImpl

Mean statistic implementation - can be reset by setter.

geometricMeanImpl

UnivariateStatistic geometricMeanImpl

Geometric mean statistic implementation - can be reset by setter.

kurtosisImpl

UnivariateStatistic kurtosisImpl

Kurtosis statistic implementation - can be reset by setter.

maxImpl

UnivariateStatistic maxImpl

Maximum statistic implementation - can be reset by setter.

minImpl

UnivariateStatistic minImpl

Minimum statistic implementation - can be reset by setter.

percentileImpl

UnivariateStatistic percentileImpl

Percentile statistic implementation - can be reset by setter.

skewnessImpl

UnivariateStatistic skewnessImpl

Skewness statistic implementation - can be reset by setter.

varianceImpl

UnivariateStatistic varianceImpl

Variance statistic implementation - can be reset by setter.

sumsqImpl

UnivariateStatistic sumsqImpl

Sum of squares statistic implementation - can be reset by setter.

sumImpl

UnivariateStatistic sumImpl

Sum statistic implementation - can be reset by setter.

Class org.apache.commons.math3.stat.descriptive.MultivariateSummaryStatistics extends Object implements Serializable

serialVersionUID: 2271900808994826718L

Serialized Fields

k

int k

Dimension of the data.

n

long n

Count of values that have been added

sumImpl

StorelessUnivariateStatistic[] sumImpl

Sum statistic implementation - can be reset by setter.

sumSqImpl

StorelessUnivariateStatistic[] sumSqImpl

Sum of squares statistic implementation - can be reset by setter.

minImpl

StorelessUnivariateStatistic[] minImpl

Minimum statistic implementation - can be reset by setter.

maxImpl

StorelessUnivariateStatistic[] maxImpl

Maximum statistic implementation - can be reset by setter.

sumLogImpl

StorelessUnivariateStatistic[] sumLogImpl

Sum of log statistic implementation - can be reset by setter.

geoMeanImpl

StorelessUnivariateStatistic[] geoMeanImpl

Geometric mean statistic implementation - can be reset by setter.

meanImpl

StorelessUnivariateStatistic[] meanImpl

Mean statistic implementation - can be reset by setter.

covarianceImpl

VectorialCovariance covarianceImpl

Covariance statistic implementation - cannot be reset.

Class org.apache.commons.math3.stat.descriptive.StatisticalSummaryValues extends Object implements Serializable

serialVersionUID: -5108854841843722536L

Serialized Fields

mean

double mean

The sample mean

variance

double variance

The sample variance

n

long n

The number of observations in the sample

max

double max

The maximum value

min

double min

The minimum value

sum

double sum

The sum of the sample values

Class org.apache.commons.math3.stat.descriptive.SummaryStatistics extends Object implements Serializable

serialVersionUID: -2021321786743555871L

Serialized Fields

n

long n

count of values that have been added

secondMoment

SecondMoment secondMoment

SecondMoment is used to compute the mean and variance

sum

Sum sum

sum of values that have been added

sumsq

SumOfSquares sumsq

sum of the square of each value that has been added

min

Min min

min of values that have been added

max

Max max

max of values that have been added

sumLog

SumOfLogs sumLog

sumLog of values that have been added

geoMean

GeometricMean geoMean

geoMean of values that have been added

mean

Mean mean

mean of values that have been added

variance

Variance variance

variance of values that have been added

sumImpl

StorelessUnivariateStatistic sumImpl

Sum statistic implementation - can be reset by setter.

sumsqImpl

StorelessUnivariateStatistic sumsqImpl

Sum of squares statistic implementation - can be reset by setter.

minImpl

StorelessUnivariateStatistic minImpl

Minimum statistic implementation - can be reset by setter.

maxImpl

StorelessUnivariateStatistic maxImpl

Maximum statistic implementation - can be reset by setter.

sumLogImpl

StorelessUnivariateStatistic sumLogImpl

Sum of log statistic implementation - can be reset by setter.

geoMeanImpl

StorelessUnivariateStatistic geoMeanImpl

Geometric mean statistic implementation - can be reset by setter.

meanImpl

StorelessUnivariateStatistic meanImpl

Mean statistic implementation - can be reset by setter.

varianceImpl

StorelessUnivariateStatistic varianceImpl

Variance statistic implementation - can be reset by setter.

Class org.apache.commons.math3.stat.descriptive.SynchronizedDescriptiveStatistics extends DescriptiveStatistics implements Serializable

serialVersionUID: 1L

Class org.apache.commons.math3.stat.descriptive.SynchronizedMultivariateSummaryStatistics extends MultivariateSummaryStatistics implements Serializable

serialVersionUID: 7099834153347155363L

Class org.apache.commons.math3.stat.descriptive.SynchronizedSummaryStatistics extends SummaryStatistics implements Serializable

serialVersionUID: 1909861009042253704L

Package org.apache.commons.math3.stat.descriptive.moment

Class org.apache.commons.math3.stat.descriptive.moment.GeometricMean extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: -8178734905303459453L

Serialized Fields

sumOfLogs

StorelessUnivariateStatistic sumOfLogs

Wrapped SumOfLogs instance

Class org.apache.commons.math3.stat.descriptive.moment.Kurtosis extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: 2784465764798260919L

Serialized Fields

moment

org.apache.commons.math3.stat.descriptive.moment.FourthMoment moment

Fourth Moment on which this statistic is based

incMoment

boolean incMoment

Determines whether or not this statistic can be incremented or cleared.

Statistics based on (constructed from) external moments cannot be incremented or cleared.

Class org.apache.commons.math3.stat.descriptive.moment.Mean extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: -1296043746617791564L

Serialized Fields

moment

org.apache.commons.math3.stat.descriptive.moment.FirstMoment moment

First moment on which this statistic is based.

incMoment

boolean incMoment

Determines whether or not this statistic can be incremented or cleared.

Statistics based on (constructed from) external moments cannot be incremented or cleared.

Class org.apache.commons.math3.stat.descriptive.moment.SecondMoment extends org.apache.commons.math3.stat.descriptive.moment.FirstMoment implements Serializable

serialVersionUID: 3942403127395076445L

Serialized Fields

m2

double m2

second moment of values that have been added

Class org.apache.commons.math3.stat.descriptive.moment.SemiVariance extends AbstractUnivariateStatistic implements Serializable

serialVersionUID: -2653430366886024994L

Serialized Fields

biasCorrected

boolean biasCorrected

Determines whether or not bias correction is applied when computing the value of the statisic. True means that bias is corrected.

varianceDirection

SemiVariance.Direction varianceDirection

Determines whether to calculate downside or upside SemiVariance.

Class org.apache.commons.math3.stat.descriptive.moment.Skewness extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: 7101857578996691352L

Serialized Fields

moment

org.apache.commons.math3.stat.descriptive.moment.ThirdMoment moment

Third moment on which this statistic is based

incMoment

boolean incMoment

Determines whether or not this statistic can be incremented or cleared.

Statistics based on (constructed from) external moments cannot be incremented or cleared.

Class org.apache.commons.math3.stat.descriptive.moment.StandardDeviation extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: 5728716329662425188L

Serialized Fields

variance

Variance variance

Wrapped Variance instance

Class org.apache.commons.math3.stat.descriptive.moment.Variance extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: -9111962718267217978L

Serialized Fields

moment

SecondMoment moment

SecondMoment is used in incremental calculation of Variance

incMoment

boolean incMoment

Whether or not Variance.increment(double) should increment the internal second moment. When a Variance is constructed with an external SecondMoment as a constructor parameter, this property is set to false and increments must be applied to the second moment directly.

isBiasCorrected

boolean isBiasCorrected

Whether or not bias correction is applied when computing the value of the statistic. True means that bias is corrected. See Variance for details on the formula.

Class org.apache.commons.math3.stat.descriptive.moment.VectorialCovariance extends Object implements Serializable

serialVersionUID: 4118372414238930270L

Serialized Fields

sums

double[] sums

Sums for each component.

productsSums

double[] productsSums

Sums of products for each component.

isBiasCorrected

boolean isBiasCorrected

Indicator for bias correction.

n

long n

Number of vectors in the sample.

Class org.apache.commons.math3.stat.descriptive.moment.VectorialMean extends Object implements Serializable

serialVersionUID: 8223009086481006892L

Serialized Fields

means

Mean[] means

Means for each component.

Package org.apache.commons.math3.stat.descriptive.rank

Class org.apache.commons.math3.stat.descriptive.rank.Max extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: -5593383832225844641L

Serialized Fields

n

long n

Number of values that have been added

value

double value

Current value of the statistic

Class org.apache.commons.math3.stat.descriptive.rank.Median extends Percentile implements Serializable

serialVersionUID: -3961477041290915687L

Class org.apache.commons.math3.stat.descriptive.rank.Min extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: -2941995784909003131L

Serialized Fields

n

long n

Number of values that have been added

value

double value

Current value of the statistic

Class org.apache.commons.math3.stat.descriptive.rank.Percentile extends AbstractUnivariateStatistic implements Serializable

serialVersionUID: -8091216485095130416L

Serialized Fields

quantile

double quantile

Determines what percentile is computed when evaluate() is activated with no quantile argument

cachedPivots

int[] cachedPivots

Cached pivots.

Package org.apache.commons.math3.stat.descriptive.summary

Class org.apache.commons.math3.stat.descriptive.summary.Product extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: 2824226005990582538L

Serialized Fields

n

long n

The number of values that have been added

value

double value

The current Running Product.

Class org.apache.commons.math3.stat.descriptive.summary.Sum extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: -8231831954703408316L

Serialized Fields

n

long n

value

double value

The currently running sum.

Class org.apache.commons.math3.stat.descriptive.summary.SumOfLogs extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: -370076995648386763L

Serialized Fields

n

int n

Number of values that have been added

value

double value

The currently running value

Class org.apache.commons.math3.stat.descriptive.summary.SumOfSquares extends AbstractStorelessUnivariateStatistic implements Serializable

serialVersionUID: 1460986908574398008L

Serialized Fields

n

long n

value

double value

The currently running sumSq

Package org.apache.commons.math3.stat.regression

Class org.apache.commons.math3.stat.regression.ModelSpecificationException extends MathIllegalArgumentException implements Serializable

serialVersionUID: 4206514456095401070L

Class org.apache.commons.math3.stat.regression.RegressionResults extends Object implements Serializable

serialVersionUID: 1L

Serialized Fields

parameters

double[] parameters

regression slope parameters

varCovData

double[][] varCovData

variance covariance matrix of parameters

isSymmetricVCD

boolean isSymmetricVCD

boolean flag for variance covariance matrix in symm compressed storage

rank

int rank

rank of the solution

nobs

long nobs

number of observations on which results are based

containsConstant

boolean containsConstant

boolean flag indicator of whether a constant was included

globalFitInfo

double[] globalFitInfo

array storing global results, SSE, MSE, RSQ, adjRSQ

Class org.apache.commons.math3.stat.regression.SimpleRegression extends Object implements Serializable

serialVersionUID: -3004689053607543335L

Serialized Fields

sumX

double sumX

sum of x values

sumXX

double sumXX

total variation in x (sum of squared deviations from xbar)

sumY

double sumY

sum of y values

sumYY

double sumYY

total variation in y (sum of squared deviations from ybar)

sumXY

double sumXY

sum of products

n

long n

number of observations

xbar

double xbar

mean of accumulated x values, used in updating formulas

ybar

double ybar

mean of accumulated y values, used in updating formulas

hasIntercept

boolean hasIntercept

include an intercept or not

Package org.apache.commons.math3.transform

Class org.apache.commons.math3.transform.FastCosineTransformer extends Object implements Serializable

serialVersionUID: 20120212L

Serialized Fields

normalization

DctNormalization normalization

The type of DCT to be performed.

Class org.apache.commons.math3.transform.FastHadamardTransformer extends Object implements Serializable

serialVersionUID: 20120211L

Class org.apache.commons.math3.transform.FastSineTransformer extends Object implements Serializable

serialVersionUID: 20120211L

Serialized Fields

normalization

DstNormalization normalization

The type of DST to be performed.

Package org.apache.commons.math3.util

Class org.apache.commons.math3.util.BigReal extends Object implements Serializable

serialVersionUID: 4984534880991310382L

Serialized Fields

d

BigDecimal d

Underlying BigDecimal.

roundingMode

RoundingMode roundingMode

Rounding mode for divisions.

scale

int scale

BigDecimal scale

Class org.apache.commons.math3.util.BigRealField extends Object implements Serializable

serialVersionUID: 4756431066541037559L

Serialization Methods

readResolve

private Object readResolve()

Handle deserialization of the singleton.

Class org.apache.commons.math3.util.Decimal64 extends Number implements Serializable

serialVersionUID: 20120227L

Serialized Fields

value

double value

The primitive double value of this object.

Class org.apache.commons.math3.util.DefaultTransformer extends Object implements Serializable

serialVersionUID: 4019938025047800455L

Class org.apache.commons.math3.util.IterationEvent extends EventObject implements Serializable

serialVersionUID: 20120128L

Serialized Fields

iterations

int iterations

The number of iterations performed so far.

Class org.apache.commons.math3.util.OpenIntToDoubleHashMap extends Object implements Serializable

serialVersionUID: -3646337053166149105L

Serialization Methods

readObject

private void readObject(ObjectInputStream stream)
                 throws IOException,
                        ClassNotFoundException

Read a serialized object.

Throws:: IOException - if object cannot be read; ClassNotFoundException - if the class corresponding to the serialized object cannot be found

Serialized Fields

keys

int[] keys

Keys table.

values

double[] values

Values table.

states

byte[] states

States table.

missingEntries

double missingEntries

Return value for missing entries.

size

int size

Current size of the map.

mask

int mask

Bit mask for hash values.

Class org.apache.commons.math3.util.OpenIntToFieldHashMap extends Object implements Serializable

serialVersionUID: -9179080286849120720L

Serialization Methods

readObject

private void readObject(ObjectInputStream stream)
                 throws IOException,
                        ClassNotFoundException

Read a serialized object.

Throws:: IOException - if object cannot be read; ClassNotFoundException - if the class corresponding to the serialized object cannot be found

Serialized Fields

field

Field<T> field

Field to which the elements belong.

keys

int[] keys

Keys table.

values

FieldElement<T>[] values

Values table.

states

byte[] states

States table.

missingEntries

FieldElement<T> missingEntries

Return value for missing entries.

size

int size

Current size of the map.

mask

int mask

Bit mask for hash values.

Class org.apache.commons.math3.util.ResizableDoubleArray extends Object implements Serializable

serialVersionUID: -3485529955529426875L

Serialized Fields

contractionCriterion

double contractionCriterion

The contraction criteria determines when the internal array will be contracted to fit the number of elements contained in the element array + 1.

expansionFactor

double expansionFactor

The expansion factor of the array. When the array needs to be expanded, the new array size will be internalArray.length * expansionFactor if expansionMode is set to MULTIPLICATIVE_MODE, or internalArray.length + expansionFactor if expansionMode is set to ADDITIVE_MODE.

expansionMode

ResizableDoubleArray.ExpansionMode expansionMode

Determines whether array expansion by expansionFactor is additive or multiplicative.

internalArray

double[] internalArray

The internal storage array.

numElements

int numElements

The number of addressable elements in the array. Note that this has nothing to do with the length of the internal storage array.

startIndex

int startIndex

The position of the first addressable element in the internal storage array. The addressable elements in the array are internalArray[startIndex],...,internalArray[startIndex + numElements - 1].

Class org.apache.commons.math3.util.TransformerMap extends Object implements Serializable

serialVersionUID: 4605318041528645258L

Serialized Fields

defaultTransformer

NumberTransformer defaultTransformer

A default Number Transformer for Numbers and numeric Strings.

map

Map<K,V> map

The internal Map.

Package org.orekit.attitudes

Class org.orekit.attitudes.AbstractAttitudeLaw extends Object implements Serializable

serialVersionUID: -1910701919077112225L

Serialized Fields

spinDerivativesComputation

boolean spinDerivativesComputation

Flag to indicate if spin derivation computation is activated.

Class org.orekit.attitudes.AbstractIsisSpinBiasSlew extends AbstractSlew implements Serializable

serialVersionUID: -6790738169776896817L

Serialized Fields

initialOrFinalDate

AbsoluteDate initialOrFinalDate

Initial or final date of the slew.

typeOfDate

AbstractIsisSpinBiasSlew.TypeOfDate typeOfDate

Type of reference date: initial date or final date.

refFrame

Frame refFrame

Reference frame.

dtSCAO

double dtSCAO

Time step.

spinDerivativesComputation

boolean spinDerivativesComputation

Flag to indicate if spin derivation computation is activated.

slewAngle

double slewAngle

Angle of the rotation associated to the spin bias slew.

slewAxis

Vector3D slewAxis

Axis of the rotation associated to the spin bias slew.

durationWoTranq

double durationWoTranq

Duration of the spin bias slew, excluding the tranquillisation phase.

accelMax

double accelMax

Value of the acceleration step during the first phase.

decelMax

double decelMax

Value of the deceleration step during the last phase (assumed > 0).

accelDuration

double accelDuration

Duration of the acceleration phase.

decelDuration

double decelDuration

Duration of the deceleration phase.

ephem

TabulatedAttitude ephem

Attitude ephemerides of the slew, including the tranquillisation phase.

thetaMaxAllowed

double thetaMaxAllowed

Maximum slew angular amplitude allowed.

durationMax

double durationMax

Maximum duration expected for the slew, including the tranquilisation phase.

dtConvergenceThreshold

double dtConvergenceThreshold

Convergence threshold for the iterative computation of the slew duration.

inertiaMatrix

double[][] inertiaMatrix

Satellite inertia matrix in satellite reference frame.

rwTorqueAllocAccel

double rwTorqueAllocAccel

Torque allocation for each RW during the acceleration phase.

rwTorqueAllocDecel

double rwTorqueAllocDecel

Torque allocation for each RW during the deceleration phase.

rwDeltaMomentumAlloc

double rwDeltaMomentumAlloc

Angular momentum allocation for each RW during the manoeuvre.

rwMatrix

double[][] rwMatrix

cosine directors matrix of the reaction wheels in the satellite reference frame. Matrix 3xN_RW with N_RW wheels (Reaction wheels spin axes written in column in the satellite reference frame).

tranquillisationTime

double tranquillisationTime

Tranquilisation time after the end of the slew.

maxIterationsNumber

double maxIterationsNumber

Maximum number of iterations allowed for slew duration computation's convergence.

Class org.orekit.attitudes.AbstractSlew extends Object implements Serializable

serialVersionUID: 7637553563096392474L

Serialized Fields

iLaw

AttitudeProvider iLaw

The attitude law before the slew.

fLaw

AttitudeProvider fLaw

The attitude law after the slew.

intervalOfValidity

AbsoluteDateInterval intervalOfValidity

Interval of validity of the maneuver (with closed endpoints).

computed

boolean computed

True if the slew has already been computed.

currentProvider

PVCoordinatesProvider currentProvider

The PV coordinates provider that has been used to compute the maneuver.

Class org.orekit.attitudes.AeroAttitudeLaw extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -5371693012337184284L

Serialized Fields

angleOfAttack

IParameterizableFunction angleOfAttack

Angle of attack.

sideSlip

IParameterizableFunction sideSlip

Sideslip.

rollVelocity

IParameterizableFunction rollVelocity

Roll velocity.

earthBodyShape

ExtendedOneAxisEllipsoid earthBodyShape

Earth shape.

stepSpin

double stepSpin

Step for finite differences spin computation.

stepAcc

double stepAcc

Step for finite differences spin derivative computation.

Class org.orekit.attitudes.Attitude extends Object implements Serializable

serialVersionUID: -947817502698754209L

Serialized Fields

referenceFrame

Frame referenceFrame

Reference frame.

orientation

TimeStampedAngularCoordinates orientation

Attitude, spin and spin derivatives.

Class org.orekit.attitudes.AttitudeChronologicalComparator extends Object implements Serializable

serialVersionUID: 757983092465215089L

Class org.orekit.attitudes.AttitudeFrame extends Frame implements Serializable

serialVersionUID: 1239403019365033844L

Serialized Fields

attlaw

AttitudeProvider attlaw

The attitude law defining the orientation of the frame.

Class org.orekit.attitudes.AttitudeLawLeg extends Object implements Serializable

serialVersionUID: 165478998919828375L

Serialized Fields

law

AttitudeLaw law

Law provider.

interval

AbsoluteDateInterval interval

Interval of validity (with closed endpoints).

Class org.orekit.attitudes.AttitudeLegLaw extends Object implements Serializable

serialVersionUID: 1120527407708346861L

Serialized Fields

lawBefore

AttitudeLaw lawBefore

Law before interval of validity .

leg

AttitudeLeg leg

Law during interval of validity .

lawAfter

AttitudeLaw lawAfter

Law after interval of validity .

Class org.orekit.attitudes.AttitudeLegsSequence extends Object implements Serializable

serialVersionUID: -1887681878952009836L

Serialized Fields

attLegs

LinkedHashMap<K,V> attLegs

Map containing all attitude legs. The LinkedHashMap was chosen to associate a code to each attitude leg and at the same time to provide easy lookup and insertion at the beginning and end of the map.

timeInterval

AbsoluteDateInterval timeInterval

Time interval (mutable).

Class org.orekit.attitudes.AttitudesSequence extends Object implements Serializable

serialVersionUID: 5140034224175180354L

Serialized Fields

active

AttitudeLaw active

Active provider.

switchingMap

Map<K,V> switchingMap

Switching events map.

Class org.orekit.attitudes.AttitudeTransformProvider extends Object implements Serializable

serialVersionUID: -9164889216629455626L

Serialized Fields

attlaw

AttitudeLaw attlaw

The attitude law from which the transformation with respect to a parent frame is computed.

pvProv

PVCoordinatesProvider pvProv

PV coordinates provider for the spacecraft.

refFrame

Frame refFrame

The parent frame.

Class org.orekit.attitudes.BodyCenterGroundPointing extends GroundPointing implements Serializable

serialVersionUID: 6757742593371484171L

Class org.orekit.attitudes.BodyCenterPointing extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -6528493179834801802L

Serialized Fields

bodyFrame

Frame bodyFrame

Body frame.

Class org.orekit.attitudes.CelestialBodyPointed extends AbstractAttitudeLaw implements Serializable

serialVersionUID: 6222161082155807729L

Serialized Fields

celestialFrame

Frame celestialFrame

Frame in which CelestialBodyPointed.phasingCel is defined.

pointedBody

PVCoordinatesProvider pointedBody

Celestial body to point at.

phasingCel

Vector3D phasingCel

Phasing reference, in celestial frame.

pointingSat

Vector3D pointingSat

Satellite axis aiming at the pointed body, in satellite frame.

phasingSat

Vector3D phasingSat

Phasing reference, in satellite frame.

Class org.orekit.attitudes.ComposedAttitudeLaw extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -8663407950398620133L

Serialized Fields

mainLaw

AttitudeLaw mainLaw

Main attitude law.

modifierLaws

List<E> modifierLaws

Modifier laws.

Class org.orekit.attitudes.ConstantAttitudeLaw extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -2143350226737178213L

Serialized Fields

referenceFrame

Frame referenceFrame

Reference frame.

rotation

Rotation rotation

Rotation from reference frame to desired satellite frame.

Class org.orekit.attitudes.ConstantSpinSlew extends AbstractSlew implements Serializable

serialVersionUID: -6284538107289929309L

Serialized Fields

type

ConstantSpinSlew.Constraint type

Type of constraint of the slew

value

double value

Value of the constraint : duration or angular velocity

d

AbsoluteDate d

The date given by the user for the angular velocity constraint computation Can be the begin date or the end date

isStart

boolean isStart

If the date is start date or not

initAtt

Attitude initAtt

Attitude at the beginning (complete when slew is computed)

finalAtt

Attitude finalAtt

Attitude at the end (complete when slew is computed)

spin

Vector3D spin

Spin of the slew (complete when slew is computed)

spinDerivativesComputation

boolean spinDerivativesComputation

Flag to indicate if spin derivation computation is activated.

Class org.orekit.attitudes.FixedRate extends AbstractAttitudeLaw implements Serializable

serialVersionUID: 6874119218379303688L

Serialized Fields

referenceAttitude

Attitude referenceAttitude

Reference attitude.

Class org.orekit.attitudes.GroundPointing extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -1459257023765594793L

Serialized Fields

bodyFrame

Frame bodyFrame

Body frame.

shape

BodyShape shape

Body shape.

Class org.orekit.attitudes.GroundPointingWrapper extends GroundPointing implements Serializable

serialVersionUID: 262999520075931766L

Serialized Fields

groundPointingLaw

GroundPointing groundPointingLaw

Underlying ground pointing attitude provider.

Class org.orekit.attitudes.IsisAnalyticalSpinBiasSlew extends AbstractIsisSpinBiasSlew implements Serializable

serialVersionUID: 1884951936812056062L

Class org.orekit.attitudes.IsisNumericalSpinBiasSlew extends AbstractIsisSpinBiasSlew implements Serializable

serialVersionUID: -5530480164376213798L

Class org.orekit.attitudes.IsisSunPointing extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -396768615500080537L

Serialized Fields

sunDirection

IDirection sunDirection

Sun direction in GCRF frame.

Class org.orekit.attitudes.LofOffset extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -713570668596014285L

Serialized Fields

type

LOFType type

Type of Local Orbital Frame.

offset

Rotation offset

Rotation from local orbital frame.

inertialFrame

Frame inertialFrame

Inertial frame with respect to which orbit should be computed.

Class org.orekit.attitudes.LofOffsetPointing extends GroundPointing implements Serializable

serialVersionUID: -713570668596014285L

Serialized Fields

attitudeLaw

AttitudeProvider attitudeLaw

Rotation from local orbital frame.

satPointingVector

Vector3D satPointingVector

Chosen satellite axis for pointing, given in satellite frame.

Class org.orekit.attitudes.NadirPointing extends GroundPointing implements Serializable

serialVersionUID: 9077899256315179822L

Class org.orekit.attitudes.OrientationFrame extends Frame implements Serializable

serialVersionUID: 7680325947511606746L

Class org.orekit.attitudes.OrientationTransformProvider extends Object implements Serializable

serialVersionUID: -6420772272580569770L

Serialized Fields

orientationLaw

IOrientationLaw orientationLaw

The orientation law from which the transformation with respect to a parent frame is computed.

refFrame

Frame refFrame

The parent frame.

Class org.orekit.attitudes.RelativeTabulatedAttitudeLaw extends Object implements Serializable

serialVersionUID: 1L

Serialized Fields

attitudeLegLaw

AttitudeLegLaw attitudeLegLaw

Attitude Leg Law .

Class org.orekit.attitudes.RelativeTabulatedAttitudeLeg extends Object implements Serializable

serialVersionUID: 1L

Serialized Fields

refDate

AbsoluteDate refDate

Reference date

attitudes

AngularCoordinates[] attitudes

Array of chronologically ordered angular coordinates

durations

double[] durations

Array (same size of attitudes array) containing for each attitude time elapsed since reference date

refFrame

Frame refFrame

reference frame from which angular coordinates are computed

validityInterval

AbsoluteDateInterval validityInterval

validity interval of the law

useRotationRates

boolean useRotationRates

flag to indicate if rotation rates should be used for Hermite interpolation

interpOrder

int interpOrder

Number of points used for interpolation

spinDerivativesComputation

boolean spinDerivativesComputation

Flag to indicate if spin derivation computation is activated.

Class org.orekit.attitudes.SpinStabilized extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -7025790361794748354L

Serialized Fields

nonRotatingLaw

AttitudeLaw nonRotatingLaw

Underlying non-rotating attitude law.

start

AbsoluteDate start

Start date of the rotation.

axis

Vector3D axis

Rotation axis in satellite frame.

rate

double rate

Spin rate in radians per seconds.

spin

Vector3D spin

Spin vector.

Class org.orekit.attitudes.SunPointing extends TwoDirectionsAttitude implements Serializable

serialVersionUID: -580319565633029444L

Class org.orekit.attitudes.TabulatedAttitude extends Object implements Serializable

serialVersionUID: 6595548109504426959L

Serialized Fields

attitudes

Attitude[] attitudes

Array of Attitudes

durations

double[] durations

Array (same size of attitudes array) containing for each attitude time elapsed since first attitude

interpOrder

int interpOrder

Number of points used for interpolation

arraySize

int arraySize

arraySize

validityInterval

AbsoluteDateInterval validityInterval

validity interval

spinDerivativesComputation

boolean spinDerivativesComputation

Flag to indicate if spin derivation computation is activated.

Class org.orekit.attitudes.TargetGroundPointing extends GroundPointing implements Serializable

serialVersionUID: -8002434923471977301L

Serialized Fields

target

PVCoordinates target

Target in body frame.

Class org.orekit.attitudes.TargetPointing extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -8002434923471977301L

Serialized Fields

bodyFrame

Frame bodyFrame

Body frame.

target

PVCoordinates target

Target in body frame.

Class org.orekit.attitudes.TwoDirectionsAttitude extends AbstractAttitudeLaw implements Serializable

serialVersionUID: -5992543210599145752L

Serialized Fields

firstDir

IDirection firstDir

First direction.

secondDir

IDirection secondDir

Second direction.

firstSatAxis

Vector3D firstSatAxis

The first satellite axis is aligned with the first direction.

secondSatAxis

Vector3D secondSatAxis

The Second satellite axis is aligned with the second direction at best.

stepSpin

double stepSpin

Step for finite differences spin computation.

stepAcc

double stepAcc

Step for finite differences spin derivative computation.

Class org.orekit.attitudes.TwoSpinBiasSlew extends AbstractSlew implements Serializable

serialVersionUID: -3915599581319142244L

Serialized Fields

initDate

AbsoluteDate initDate

The slew initial date (the date of the change of the attitude law).

refFrame

Frame refFrame

Reference frame.

ephem

TabulatedAttitude ephem

The attitude ephemeris representing the slew.

dtSCAO

double dtSCAO

SCAO time step [s].

thetaMax

double thetaMax

The maximum angle of validity of the model [rad].

tau

double tau

Time constant of the filter [s].

seuilQcEntree

double seuilQcEntree

Initial orientation error threshold [rad].

bvHaut

double bvHaut

The angular velocity for big angular distances (used when seuil_qc_sortie < theta < sbv_haut) [rad/s].

sbvHaut

double sbvHaut

The switching angular distance [rad].

seuilQcSortie

double seuilQcSortie

Final orientation error threshold [rad].

bvBas

double bvBas

The angular velocity for small angular distances (used when sbv_haut < theta < thetaMax) [rad/s].

tStabSol

double tStabSol

Stabilisation margin [s].

spinDerivativesComputation

boolean spinDerivativesComputation

Flag to indicate if spin derivation computation is activated.

Class org.orekit.attitudes.YawCompensation extends GroundPointingWrapper implements Serializable

serialVersionUID: 1145977506851433023L

Class org.orekit.attitudes.YawSteering extends GroundPointingWrapper implements Serializable

serialVersionUID: -5804405406938727964L

Serialized Fields

sun

PVCoordinatesProvider sun

Sun motion model.

phasingAxis

Vector3D phasingAxis

Satellite axis that must be roughly in Sun direction.

Package org.orekit.bodies

Class org.orekit.bodies.AbstractCelestialBody extends Object implements Serializable

serialVersionUID: -8225707171826328799L

Serialized Fields

name

String name

Name of the body.

gm

double gm

Attraction coefficient of the body (m³/s²).

iauPole

IAUPole iauPole

IAU pole.

inertialFrame

Frame inertialFrame

Inertially oriented, body-centered frame.

bodyFrame

Frame bodyFrame

Body oriented, body-centered frame.

Class org.orekit.bodies.AbstractCelestialBody.BodyOriented extends Object implements Serializable

serialVersionUID: -1859795611761959145L

Class org.orekit.bodies.ExtendedOneAxisEllipsoid extends Object implements Serializable

serialVersionUID: -5136554736087949714L

Serialized Fields

ellipsoid

IEllipsoid ellipsoid

the spheroid

inFrame

Frame inFrame

the body frame

fIn

double fIn

Flattening

aeIn

double aeIn

Equatorial radius.

e2

double e2

Eccentricity power 2.

g2

double g2

g * g.

inName

String inName

shape name

Class org.orekit.bodies.GeodeticPoint extends Object implements Serializable

serialVersionUID: 7862466825590075399L

Serialized Fields

latitude

double latitude

Latitude of the point (rad).

longitude

double longitude

Longitude of the point (rad).

altitude

double altitude

Altitude of the point (m).

Class org.orekit.bodies.MeeusMoon extends AbstractCelestialBody implements Serializable

serialVersionUID: 755708934677699377L

Serialized Fields

longitudeTerms

int longitudeTerms

Number of terms for longitude computation.

latitudeTerms

int latitudeTerms

Number of terms for latitude computation.

distanceTerms

int distanceTerms

Number of terms for distance computation.

Class org.orekit.bodies.MeeusSun extends AbstractCelestialBody implements Serializable

serialVersionUID: 3593147893747468086L

Serialized Fields

meeusModel

MeeusSun.MODEL meeusModel

Meeus model to be used.

Class org.orekit.bodies.OneAxisEllipsoid extends Object implements Serializable

serialVersionUID: -1418386024561514172L

Serialized Fields

bodyFrame

Frame bodyFrame

Body frame related to body shape.

ae

double ae

Equatorial radius.

e2

double e2

Eccentricity power 2.

g

double g

1 minus flatness.

g2

double g2

g * g.

ae2

double ae2

Equatorial radius power 2.

closeApproachThreshold

double closeApproachThreshold

Convergence limit.

angularThreshold

double angularThreshold

Convergence limit.

threshold2

double threshold2

2nd convergence limit if first convergence failed.

Class org.orekit.bodies.PosVelChebyshev extends Object implements Serializable

serialVersionUID: -2220448511466595393L

Serialized Fields

start

AbsoluteDate start

Start of the validity range of the instance.

duration

double duration

Duration of validity range of the instance.

xCoeffs

double[] xCoeffs

Chebyshev polynomials coefficients for the X component.

yCoeffs

double[] yCoeffs

Chebyshev polynomials coefficients for the Y component.

zCoeffs

double[] zCoeffs

Chebyshev polynomials coefficients for the Z component.

Class org.orekit.bodies.UserCelestialBody extends AbstractCelestialBody implements Serializable

serialVersionUID: -749020299406400630L

Serialized Fields

pvCoordinateProvider

PVCoordinatesProvider pvCoordinateProvider

Position-Velocity of celestial body.

Package org.orekit.data

Class org.orekit.data.BodiesElements extends Object implements Serializable

serialVersionUID: 9193325350743225370L

Serialized Fields

l

double l

Mean anomaly of the Moon.

lPrime

double lPrime

Mean anomaly of the Sun.

f

double f

L - Ω where L is the mean longitude of the Moon.

d

double d

Mean elongation of the Moon from the Sun.

omega

double omega

Mean longitude of the ascending node of the Moon.

lMe

double lMe

Mean Mercury longitude.

lVe

double lVe

Mean Venus longitude.

lE

double lE

Mean Earth longitude.

lMa

double lMa

Mean Mars longitude.

lJu

double lJu

Mean Jupiter longitude.

lSa

double lSa

Mean Saturn longitude.

lUr

double lUr

Mean Uranus longitude.

lNe

double lNe

Mean Neptune longitude.

pa

double pa

General accumulated precession in longitude.

Class org.orekit.data.DataProvidersManager extends Object implements Serializable

serialVersionUID: -6462388122735180273L

Serialized Fields

providers

List<E> providers

Supported data providers.

loaded

Set<E> loaded

Loaded data.

Class org.orekit.data.PoissonSeries extends Object implements Serializable

serialVersionUID: -3016824169123970737L

Serialized Fields

coefficients

double[] coefficients

Coefficients of the polynomial part.

series

SeriesTerm[][] series

Non-polynomial series.

Class org.orekit.data.SeriesTerm extends Object implements Serializable

serialVersionUID: 7536446008538764006L

Serialized Fields

sinCoeff

double sinCoeff

Coefficient for the sine of the argument.

cosCoeff

double cosCoeff

Coefficient for the cosine of the argument.

Package org.orekit.errors

Class org.orekit.errors.FrameAncestorException extends OrekitException implements Serializable

serialVersionUID: -8279818119798166504L

Class org.orekit.errors.OrekitException extends Exception implements Serializable

serialVersionUID: 3366757982695469677L

Serialized Fields

context

ExceptionContext context

Exception context (may be null).

specifier

Localizable specifier

Format specifier (to be translated).

parts

Object[] parts

Parts to insert in the format (no translation).

Class org.orekit.errors.OrekitExceptionWrapper extends RuntimeException implements Serializable

serialVersionUID: -2369002825757407992L

Serialized Fields

wrappedException

OrekitException wrappedException

Underlying Orekit exception.

Class org.orekit.errors.OrekitRuntimeException extends RuntimeException implements Serializable

serialVersionUID: 879013611768983409L

Class org.orekit.errors.PropagationException extends OrekitException implements Serializable

serialVersionUID: 1684307015196169376L

Class org.orekit.errors.TimeStampedCacheException extends OrekitException implements Serializable

serialVersionUID: 9015424948577907926L

Package org.orekit.files.general

Class org.orekit.files.general.SatelliteInformation extends Object implements Serializable

serialVersionUID: -8329507360193822277L

Serialized Fields

satelliteId

String satelliteId

Id of the satellite as used in the orbit file.

accuracy

int accuracy

One standard deviation of the orbit entries in m.

Class org.orekit.files.general.SatelliteTimeCoordinate extends Object implements Serializable

serialVersionUID: -2099947583052252633L

Serialized Fields

epoch

AbsoluteDate epoch

Epoch for this entry.

coordinate

PVCoordinates coordinate

Position/velocity coordinates for this entry.

clockCorrection

double clockCorrection

Clock correction in micro-seconds.

clockRateChange

double clockRateChange

Clock rate change.

Package org.orekit.files.sp3

Class org.orekit.files.sp3.SP3File extends Object implements Serializable

serialVersionUID: 3333652174843017654L

Serialized Fields

type

SP3File.SP3FileType type

File type.

timeSystem

OrbitFile.TimeSystem timeSystem

Time system.

epoch

AbsoluteDate epoch

Epoch of the file.

gpsWeek

int gpsWeek

GPS week.

secondsOfWeek

double secondsOfWeek

Seconds of the current GPS week.

julianDay

int julianDay

Julian day.

dayFraction

double dayFraction

Day fraction.

epochInterval

double epochInterval

Time-interval between epochs.

numberOfEpochs

int numberOfEpochs

Number of epochs.

coordinateSystem

String coordinateSystem

Coordinate system.

dataUsed

String dataUsed

Data used indicator.

orbitType

SP3File.SP3OrbitType orbitType

Orbit type.

agency

String agency

Agency providing the file.

satellites

List<E> satellites

A list containing additional satellite information.

satelliteInfo

Map<K,V> satelliteInfo

A mapping of satellite id to its corresponding SatelliteInformation object.

satelliteCoords

Map<K,V> satelliteCoords

A map containing all satellite coordinates.

Package org.orekit.forces

Package org.orekit.forces.atmospheres

Class org.orekit.forces.atmospheres.DTM2000 extends Object implements Serializable

serialVersionUID: -8901940398967553588L

Serialized Fields

dtt

double[] dtt

Partial derivatives.

dh

double[] dh

dhe

double[] dhe

dox

double[] dox

daz2

double[] daz2

do2

double[] do2

daz

double[] daz

dt0

double[] dt0

dtp

double[] dtp

cachedDay

double cachedDay

Number of days in current year.

cachedF

double[] cachedF

Instant solar flux. f[1] = instantaneous flux; f[2] = 0. (not used).

cachedFbar

double[] cachedFbar

Mean solar flux. fbar[1] = mean flux; fbar[2] = 0. (not used).

akp

double[] akp

Kp coefficients.

akp[1] = 3-hourly kp
akp[2] = 0 (not used)
akp[3] = mean kp of last 24 hours
akp[4] = 0 (not used)

cachedAlti

double cachedAlti

Geodetic altitude in km (minimum altitude: 120 km).

cachedHl

double cachedHl

Local solar time (rad).

alat

double alat

Geodetic Latitude (rad).

xlon

double xlon

Geodetic longitude (rad).

cachedTemperature

double cachedTemperature

Cache mecanism - Temperature at altitude z (K).

tinf

double tinf

Exospheric temperature.

tp120

double tp120

Vertical gradient of T a 120 km.

ro

double ro

Total density (g/cm3).

wmm

double wmm

Mean atomic mass.

d

double[] d

Partial densities in (g/cm3). d(1) = hydrogen d(2) = helium d(3) = atomic oxygen d(4) = molecular nitrogen d(5) = molecular oxygen d(6) = atomic nitrogen

p10

double p10

Legendre coefficients.

p20

double p20

p30

double p30

p40

double p40

p50

double p50

p60

double p60

p11

double p11

p21

double p21

p31

double p31

p41

double p41

p51

double p51

p22

double p22

p32

double p32

p42

double p42

p52

double p52

p62

double p62

p33

double p33

p10mg

double p10mg

p20mg

double p20mg

p40mg

double p40mg

hl0

double hl0

Local time intermediate values.

ch

double ch

sh

double sh

c2h

double c2h

s2h

double s2h

c3h

double c3h

s3h

double s3h

sun

PVCoordinatesProvider sun

Sun position.

inputParams

DTM2000InputParameters inputParams

External data container.

earth

BodyShape earth

Earth body shape.

cachedOutputData

AtmosphereData cachedOutputData

Cache mecanism - Output atmosphere data.

cachedDate

AbsoluteDate cachedDate

Cache mecanism - Input date.

cachedFrame

Frame cachedFrame

Cache mecanism - Input frame.

cachedPosition

Vector3D cachedPosition

Cache mecanism - Input position.

Class org.orekit.forces.atmospheres.HarrisPriester extends Object implements Serializable

serialVersionUID: 2772347498196369601L

Serialized Fields

n

double n

Cosine exponent from 2 to 6 according to inclination.

sun

PVCoordinatesProvider sun

Sun position.

earth

BodyShape earth

Earth body shape.

tabAltRho

double[][] tabAltRho

Density table.

Class org.orekit.forces.atmospheres.JB2006 extends Object implements Serializable

serialVersionUID: -4201270765122160831L

Serialized Fields

cachedTemperature

double[] cachedTemperature

Cache mecanism - Output temperatures.

TEMP(1): Exospheric Temperature above Input Position (deg K)
TEMP(2): Temperature at Input Position (deg K)

rho

double rho

Total Mass-Density at Input Position (kg/m³).

sun

PVCoordinatesProvider sun

Sun position.

inputParams

JB2006InputParameters inputParams

External data container.

earth

BodyShape earth

Earth body shape.

cachedDensity

double cachedDensity

Cache mecanism - Output density.

cachedDate

AbsoluteDate cachedDate

Cache mecanism - Input date.

cachedFrame

Frame cachedFrame

Cache mecanism - Input frame.

cachedPosition

Vector3D cachedPosition

Cache mecanism - Input position.

Class org.orekit.forces.atmospheres.MSISE2000 extends Object implements Serializable

serialVersionUID: -7842070913367047706L

Serialized Fields

atmosModel

NRLMSISE00 atmosModel

An instance of the MSIS00 model.

flags

Flags flags

Flags for the MSIS00 density computation.

earth

BodyShape earth

Earth Shape

sun

CelestialBody sun

Sun

inputParams

MSISE2000InputParameters inputParams

Solar activity data container

calendar

Calendar calendar

Calendar (internal variable, set there for computation time saving).

cachedTemperature

double cachedTemperature

Cache mecanism - Output temperature.

cachedOutputData

AtmosphereData cachedOutputData

Cache mecanism - Output atmosphere data.

cachedDate

AbsoluteDate cachedDate

Cache mecanism - Input date.

cachedFrame

Frame cachedFrame

Cache mecanism - Input frame.

cachedPosition

Vector3D cachedPosition

Cache mecanism - Input position.

Class org.orekit.forces.atmospheres.SimpleExponentialAtmosphere extends Object implements Serializable

serialVersionUID: 2772347498196369601L

Serialized Fields

shape

BodyShape shape

Earth shape model.

rho0

double rho0

Reference density.

h0

double h0

Reference altitude.

hscale

double hscale

Reference altitude scale.

Class org.orekit.forces.atmospheres.US76 extends Object implements Serializable

serialVersionUID: -4112665369108873996L

Serialized Fields

earth

BodyShape earth

Earth Shape

tmol

double tmol

Molecular temperature

hpot

double hpot

Geopotential altitude

rn

double rn

Layer molar number

rnn

double rnn

Molar number

xmol

double xmol

Total molar mass

cachedPres

double cachedPres

Cache mecanism - Output pressure.

cachedDensity

double cachedDensity

Cache mecanism - Output density.

cachedTemp

double cachedTemp

Cache mecanism - Output temperature.

cachedDate

AbsoluteDate cachedDate

Cache mecanism - Input date.

cachedFrame

Frame cachedFrame

Cache mecanism - Input frame.

cachedPosition

Vector3D cachedPosition

Cache mecanism - Input position.

Package org.orekit.forces.atmospheres.solarActivity.specialized

Class org.orekit.forces.atmospheres.solarActivity.specialized.DTM2000SolarData extends Object implements Serializable

serialVersionUID: -5212198874900835369L

Serialized Fields

to

double to

Constant

data

SolarActivityDataProvider data

Solar data

Class org.orekit.forces.atmospheres.solarActivity.specialized.MarshallSolarActivityFutureEstimation extends Object implements Serializable

serialVersionUID: -5212198874900835369L

Serialized Fields

dataPattern

Pattern dataPattern

Pattern for the data fields of MSAFE data.

data

SortedSet<E> data

Data set.

strengthLevel

MarshallSolarActivityFutureEstimation.StrengthLevel strengthLevel

Selected strength level of activity.

firstDate

AbsoluteDate firstDate

First available date.

lastDate

AbsoluteDate lastDate

Last available date.

previousParam

org.orekit.forces.atmospheres.solarActivity.specialized.MarshallSolarActivityFutureEstimation.LineParameters previousParam

Previous set of solar activity parameters.

currentParam

org.orekit.forces.atmospheres.solarActivity.specialized.MarshallSolarActivityFutureEstimation.LineParameters currentParam

Current set of solar activity parameters.

supportedNames

String supportedNames

Regular expression for supported files names.

Package org.orekit.forces.drag

Class org.orekit.forces.drag.DragForce extends JacobiansParameterizable implements Serializable

serialVersionUID: 5386256916056674950L

Serialized Fields

densityMap

Map<K,V> densityMap

Density cache map.

relativeVelocityMap

Map<K,V> relativeVelocityMap

Relative velocity cache map.

dragAccMap

Map<K,V> dragAccMap

Drag acceleration cache map.

k

IParamDiffFunction k

k multiplicative factor.

atmosphere

Atmosphere atmosphere

Atmospheric model.

spacecraft

DragSensitive spacecraft

Spacecraft.

computePartialDerivativesWrtPosition

boolean computePartialDerivativesWrtPosition

True if acceleration partial derivatives with respect to position have to be computed.

computePartialDerivativesWrtVelocity

boolean computePartialDerivativesWrtVelocity

True if acceleration partial derivatives with respect to velocity have to be computed.

Package org.orekit.forces.gravity

Class org.orekit.forces.gravity.BalminoAttractionModel extends JacobiansParameterizable implements Serializable

serialVersionUID: 3308248172613083145L

Serialized Fields

order

int order

Max order.

degree

int degree

Max degree.

C

double[][] C

Normalized C coefficients.

S

double[][] S

Normalized S coefficients.

poly

HelmholtzPolynomial poly

Helmholtz polynomials.

bodyFrame

Frame bodyFrame

Central body frame.

denCPD

double[][] denCPD

Denormalized coefficients for acceleration partial derivatives with respect to state computation.

denSPD

double[][] denSPD

Denormalized coefficients for acceleration partial derivatives with respect to state computation.

paramMu

Parameter paramMu

Central attraction coefficient parameter.

paramAe

Parameter paramAe

Equatorial radius parameter.

Class org.orekit.forces.gravity.CunninghamAttractionModel extends JacobiansParameterizable implements Serializable

serialVersionUID: 759122284106467933L

Serialized Fields

C

double[][] C

First normalized potential tesseral coefficients array.

S

double[][] S

Second normalized potential tesseral coefficients array.

CPD

double[][] CPD

First normalized potential tesseral coefficients array for acceleration partial derivatives with respect to state computation.

SPD

double[][] SPD

Second normalized potential tesseral coefficients array for acceleration partial derivatives with respect to state computation.

degree

int degree

Degree of potential.

order

int order

Order of potential.

bodyFrame

Frame bodyFrame

Rotating body.

paramMu

Parameter paramMu

Central attraction coefficient parameter.

paramAe

Parameter paramAe

Equatorial radius parameter.

Class org.orekit.forces.gravity.DrozinerAttractionModel extends Parameterizable implements Serializable

serialVersionUID: -6897768625006106349L

Serialized Fields

C

double[][] C

First normalized potential tesseral coefficients array.

S

double[][] S

Second normalized potential tesseral coefficients array.

centralBodyFrame

Frame centralBodyFrame

Frame for the central body.

degree

int degree

Number of zonal coefficients.

order

int order

Number of tesseral coefficients.

paramMu

Parameter paramMu

Central attraction coefficient parameter.

paramAe

Parameter paramAe

Equatorial radius parameter.

computePartialDerivativesWrtPosition

boolean computePartialDerivativesWrtPosition

True if acceleration partial derivatives with respect to position have to be computed.

computePartialDerivativesWrtVelocity

boolean computePartialDerivativesWrtVelocity

True if acceleration partial derivatives with respect to velocity have to be computed.

Class org.orekit.forces.gravity.NewtonianAttraction extends JacobiansParameterizable implements Serializable

serialVersionUID: -7754312556095545327L

Serialized Fields

paramMu

Parameter paramMu

Central attraction coefficient parameter.

computePartialDerivativesWrtPosition

boolean computePartialDerivativesWrtPosition

True if acceleration partial derivatives with respect to position have to be computed.

Class org.orekit.forces.gravity.ThirdBodyAttraction extends JacobiansParameterizable implements Serializable

serialVersionUID: -1703641239448217284L

Serialized Fields

body

CelestialBody body

The body to consider.

paramMu

Parameter paramMu

Central attraction coefficient parameter.

computePartialDerivativesWrtPosition

boolean computePartialDerivativesWrtPosition

True if acceleration partial derivatives with respect to position have to be computed.

Package org.orekit.forces.gravity.tides

Class org.orekit.forces.gravity.tides.AbstractTides extends JacobiansParameterizable implements Serializable

serialVersionUID: 1383292841711855839L

Serialized Fields

paramMu

Parameter paramMu

Central attraction coefficient parameter.

paramAe

Parameter paramAe

Equatorial radius parameter.

coefficientsC

double[][] coefficientsC

First normalized potential tesseral coefficients array.

coefficientsS

double[][] coefficientsS

Second normalized potential tesseral coefficients array.

coefficientsCPD

double[][] coefficientsCPD

First normalized potential tesseral coefficients array for partial derivatives computation.

coefficientsSPD

double[][] coefficientsSPD

Second normalized potential tesseral coefficients array for partial derivatives computation.

bodyFrame

Frame bodyFrame

Frame for the central body.

l

int l

Degree.

m

int m

Order.

helm

HelmholtzPolynomial helm

Helmholtz polynomials

denCPD

double[][] denCPD

Denormalized coefficients for partial derivatives.

denSPD

double[][] denSPD

Denormalized coefficients for partial derivatives.

Class org.orekit.forces.gravity.tides.OceanTides extends AbstractTides implements Serializable

serialVersionUID: 7083827601800332989L

Serialized Fields

l

int l

Degree for acceleration computation.

m

int m

Order for acceleration computation.

lgrad

int lgrad

Degree for partial derivatives computation.

mgrad

int mgrad

Order for partial derivatives computation.

computePartialDerivativesWrtPosition

boolean computePartialDerivativesWrtPosition

True if acceleration partial derivatives with respect to position have to be computed.

heightsP

TreeMap<K,V> heightsP

Heights map

heightsS

TreeMap<K,V> heightsS

Heights map

names

TreeMap<K,V> names

Names map

oceanTidesData

IOceanTidesDataProvider oceanTidesData

Ocean tides data

mainWaves

Set<E> mainWaves

Doodson numbers of waves that have height data

fileWaves

Set<E> fileWaves

Doodson numbers of waves that have height data

secWaves

TreeMap<K,V> secWaves

Doodson numbers of secondary waves and their pivots

withAdmittanceIn

boolean withAdmittanceIn

Boolean to ignore or take into account secondary waves

phases

TreeMap<K,V> phases

Doodson-Warburg conventions

admittanceCoefficients

TreeMap<K,V> admittanceCoefficients

Admittance coefficients : key is Doodson number, value is array {Kc, Ks}

defaultSteps

double defaultSteps

Steps of 12 hours for admittance coefficients computation

loveNumbers

double[] loveNumbers

Love numbers.

loveNumbersPD

double[] loveNumbersPD

Love numbers for partial derivatives.

paramRho

Parameter paramRho

Density at surface parameter.

dataArray

org.orekit.forces.gravity.tides.OceanTides.StaticData dataArray

Interval variable stored at constructor to speed-up acceleration computation at runtime.

dataArrayPD

org.orekit.forces.gravity.tides.OceanTides.StaticData dataArrayPD

Interval variable stored at constructor to speed-up partial derivatives computation at runtime.

Class org.orekit.forces.gravity.tides.TerrestrialTides extends AbstractTides implements Serializable

serialVersionUID: 302414702448996411L

Serialized Fields

bodiesP

CelestialBody[] bodiesP

Perturbating bodies.

thirdBodyCorrectionUpToDegree3

boolean thirdBodyCorrectionUpToDegree3

Deformation due to third body attraction (degree3).

ellipticityCorrection

boolean ellipticityCorrection

Ellipticity correction.

frequencyCorrection

boolean frequencyCorrection

Frequency correction.

standard

ITerrestrialTidesDataProvider standard

Terrestrial tide data provider.

computePartialDerivativesWrtPosition

boolean computePartialDerivativesWrtPosition

True if acceleration partial derivatives with respect to position have to be computed.

Package org.orekit.forces.gravity.variations

Class org.orekit.forces.gravity.variations.VariablePotentialAttractionModel extends JacobiansParameterizable implements Serializable

serialVersionUID: 1548110713737633271L

Serialized Fields

d

int d

Degree

o

int o

Order

dGrad

int dGrad

Degree for partial derivatives computation

oGrad

int oGrad

Order for partial derivatives computation

dO

int dO

Degree correction

oO

int oO

Order correction

dOGrad

int dOGrad

Degree correction for partial derivatives computation

oOGrad

int oOGrad

Order correction for partial derivatives computation

cData

double[][] cData

C coefficients

sData

double[][] sData

S coefficients

cPDData

double[][] cPDData

C coefficients for acceleration partial derivatives with respect to state computation

sPDData

double[][] sPDData

S coefficients for acceleration partial derivatives with respect to state computation

cDataNormed

double[][] cDataNormed

C coefficients

sDataNormed

double[][] sDataNormed

S coefficients

cPDDataNormed

double[][] cPDDataNormed

C coefficients acceleration partial derivatives with respect to state computation

sPDDataNormed

double[][] sPDDataNormed

S coefficients acceleration partial derivatives with respect to state computation

optional

boolean optional

Optional terms

computeOnce

boolean computeOnce

Compute optional terms once only flag

bodyFrame

Frame bodyFrame

Body frame

setData

VariablePotentialCoefficientsSet[][] setData

Set array

setPDData

VariablePotentialCoefficientsSet[][] setPDData

Set array for acceleration partial derivatives with respect to state computation

refDate

AbsoluteDate refDate

Reference date for optional terms computation (from provider)

helm

HelmholtzPolynomial helm

Helmholtz polynomials

paramMu

Parameter paramMu

Central attraction coefficient parameter.

paramAe

Parameter paramAe

Equatorial radius parameter.

denCPD

double[][] denCPD

Denormalized coefficients for acceleration partial derivatives with respect to state computation.

denSPD

double[][] denSPD

Denormalized coefficients for acceleration partial derivatives with respect to state computation.

Package org.orekit.forces.maneuvers

Class org.orekit.forces.maneuvers.ConstantThrustError extends JacobiansParameterizable implements Serializable

serialVersionUID: -5479613740327735623L

Serialized Fields

firingStartDetector

EventDetector firingStartDetector

Firing start detector.

firingStopDetector

EventDetector firingStopDetector

Firing stop detector.

maneuverFrame

Frame maneuverFrame

Frame of the acceleration direction If null and no LOF has been provided, the acceleration is expressed in the satellite frame.

frameLofType

LOFType frameLofType

Local orbital frame type. If null and no frame has been provided, the acceleration is expressed in the satellite frame.

errorx

IParamDiffFunction errorx

The parameterizable and differentiable function representing the x component of the thrust error.

errory

IParamDiffFunction errory

The parameterizable and differentiable function representing the y component of the thrust error.

errorz

IParamDiffFunction errorz

The parameterizable and differentiable function representing the z component of the thrust error.

firing

boolean firing

State of the maneuver engine.

Class org.orekit.forces.maneuvers.ImpulseManeuver extends AbstractDetector implements Serializable

serialVersionUID: -7150871329986590368L

Serialized Fields

trigger

EventDetector trigger

Triggering event.

deltaVSat

Vector3D deltaVSat

Velocity increment in the frame defined by the user.

frame

Frame frame

Frame of the velocity increment. If null, the velocity increment is expressed in the satellite frame

lofType

LOFType lofType

Local orbital frame type.

vExhaust

double vExhaust

Engine exhaust velocity.

mass

MassProvider mass

Mass provider.

partName

String partName

Part name.

forwardLocal

boolean forwardLocal

If true, the integration variable (time) increases during integration.

Class org.orekit.forces.maneuvers.SmallManeuverAnalyticalModel extends Object implements Serializable

serialVersionUID: 5046690115016896090L

Serialized Fields

state0

SpacecraftState state0

State at maneuver date (before maneuver occurrence).

inertialDV

Vector3D inertialDV

Inertial velocity increment.

massRatio

double massRatio

Mass change ratio.

type

OrbitType type

Type of orbit used for internal Jacobians.

j0

double[][] j0

Initial Keplerian (or equinoctial) Jacobian with respect to maneuver.

j0Dot

double[][] j0Dot

Time derivative of the initial Keplerian (or equinoctial) Jacobian with respect to maneuver.

ksi

double ksi

Mean anomaly change factor.

partName

String partName

Name of the part firing.

Package org.orekit.forces.radiation

Class org.orekit.forces.radiation.RediffusedRadiationPressure extends JacobiansParameterizable implements Serializable

serialVersionUID: -6974428498597145839L

Serialized Fields

sun

CelestialBody sun

Sun model.

bodyFrame

Frame bodyFrame

body frame

nCorona

int nCorona

number of corona.

nMeridian

int nMeridian

number of meridian.

emissivityModel

IEmissivityModel emissivityModel

emissivity model

radiativeModel

RediffusedRadiationSensitive radiativeModel

rediffused radiative pressure model.

computingAcc

int computingAcc

computing of acceleration

computePartialDerivativesWrtPosition

boolean computePartialDerivativesWrtPosition

True if acceleration partial derivatives with respect to position have to be computed.

Class org.orekit.forces.radiation.SolarRadiationPressure extends JacobiansParameterizable implements Serializable

serialVersionUID: -4510170320082379419L

Serialized Fields

kRef

Parameter kRef

Reference flux normalized for a 1m distance (N).

sun

PVCoordinatesProvider sun

Sun model.

equatorialRadius

double equatorialRadius

Earth model.

spacecraft

RadiationSensitive spacecraft

Spacecraft.

computePartialDerivativesWrtPosition

boolean computePartialDerivativesWrtPosition

True if acceleration partial derivatives with respect to position have to be computed.

Package org.orekit.forces.relativistic

Class org.orekit.forces.relativistic.CoriolisRelativisticEffect extends JacobiansParameterizable implements Serializable

serialVersionUID: 3037029521564550509L

Serialized Fields

mu

double mu

Sun central attraction coefficient.

pv

PVCoordinatesProvider pv

Sun PV coordinates.

computePartialDerivativesWrtVel

boolean computePartialDerivativesWrtVel

True if acceleration partial derivatives wrt velocity have to be computed.

Class org.orekit.forces.relativistic.LenseThirringRelativisticEffect extends JacobiansParameterizable implements Serializable

serialVersionUID: 626504608796493978L

Serialized Fields

bodymu

double bodymu

Central body attraction coefficient.

bodyframe

Frame bodyframe

Frame defining pole of central body.

computePartialDerivativesWrtPos

boolean computePartialDerivativesWrtPos

True if acceleration partial derivatives wrt position have to be computed.

computePartialDerivativesWrtVel

boolean computePartialDerivativesWrtVel

True if acceleration partial derivatives wrt velocity have to be computed.

Class org.orekit.forces.relativistic.SchwarzschildRelativisticEffect extends JacobiansParameterizable implements Serializable

serialVersionUID: 1811756242976899848L

Serialized Fields

bodymu

double bodymu

Central body attraction coefficient.

computePartialDerivativesWrtPos

boolean computePartialDerivativesWrtPos

True if acceleration partial derivatives wrt position have to be computed.

computePartialDerivativesWrtVel

boolean computePartialDerivativesWrtVel

True if acceleration partial derivatives wrt velocity have to be computed.

Package org.orekit.frames

Class org.orekit.frames.FactoryManagedFrame extends Frame implements Serializable

serialVersionUID: 1566019035725009300L

Serialization Methods

writeReplace

private Object writeReplace()

Replace the instance to be serialized with the instance of the proxy.

This proxy class serializes only the name of the key.

This conception pattern ensures that at most one instance of each FactoryManagedFrame exists even if it is deserialized several times.

Serialized Fields

factoryKey

Predefined factoryKey

Key of the frame within the factory.

Class org.orekit.frames.Frame extends Object implements Serializable

serialVersionUID: -6981146543760234087L

Serialized Fields

parent

Frame parent

Parent frame (only the root frame doesn't have a parent).

transformProvider

TransformProvider transformProvider

Provider for transform from parent frame to instance.

depth

int depth

Depth of the frame with respect to tree root.

name

String name

Instance name.

pseudoInertial

boolean pseudoInertial

Indicator for pseudo-inertial frames.

Class org.orekit.frames.FramesFactory extends Object implements Serializable

serialVersionUID: 1720647682459923909L

Class org.orekit.frames.H0MinusNFrame extends Frame implements Serializable

serialVersionUID: -7728736096497526402L

Serialized Fields

h0

AbsoluteDate h0

Reference date.

n

double n

Reference date shift.

longitude

double longitude

The rotation angle around the ITRF Z axis.

Class org.orekit.frames.LocalOrbitalFrame extends Frame implements Serializable

serialVersionUID: -4469440345574964950L

Class org.orekit.frames.LocalOrbitalFrame.LocalProvider extends Object implements Serializable

serialVersionUID: 386815086579675823L

Serialized Fields

type

LOFType type

Frame type.

provider

PVCoordinatesProvider provider

Provider used to compute frame motion.

reference

Frame reference

Reference frame.

Class org.orekit.frames.SpacecraftFrame extends Frame implements Serializable

serialVersionUID: 6012707827832395314L

Serialized Fields

propagator

Propagator propagator

Deprecated.

Propagator to use.

Class org.orekit.frames.TopocentricFrame extends Frame implements Serializable

serialVersionUID: -5997915708080966466L

Serialized Fields

parentShape

BodyShape parentShape

Body shape on which the local point is defined.

point

GeodeticPoint point

Point where the topocentric frame is defined.

orientation

double orientation

Oriented angle between the local north and the x axis (counterclockwise).

Class org.orekit.frames.UpdatableFrame extends Frame implements Serializable

serialVersionUID: -2075893064211339303L

Class org.orekit.frames.UpdatableFrame.UpdatableProvider extends Object implements Serializable

serialVersionUID: 4436954500689776331L

Serialized Fields

transform

AtomicReference<V> transform

Current transform.

Package org.orekit.frames.configuration

Class org.orekit.frames.configuration.DiurnalRotation extends Object implements Serializable

serialVersionUID: -3155586485425973676L

Serialized Fields

tides

TidalCorrectionModel tides

Correction due to tidal effects.

libration

LibrationCorrectionModel libration

Correction due to libration.

Class org.orekit.frames.configuration.FramesConfigurationImplementation extends Object implements Serializable

serialVersionUID: -7815355641864558021L

Serialized Fields

history2000

EOP2000History history2000

EOP history (IAU2000).

polarMotion

PolarMotion polarMotion

Polar motion model.

diurnalRotation

DiurnalRotation diurnalRotation

Diurnal rotation model.

precessionNutation

PrecessionNutation precessionNutation

Precession nutation model.

Class org.orekit.frames.configuration.PolarMotion extends Object implements Serializable

serialVersionUID: -1495152425256550661L

Serialized Fields

tides

TidalCorrectionModel tides

Correction due to tidal effects.

libration

LibrationCorrectionModel libration

Correction due to libration.

sp

SPrimeModel sp

S' correction.

useEop

boolean useEop

Flag for use of EOP data.

Class org.orekit.frames.configuration.PrecessionNutation extends Object implements Serializable

serialVersionUID: -3700748706951357410L

Serialized Fields

model

PrecessionNutationModel model

Precession Nutation model.

useEop

boolean useEop

Flag for use of EOP data (nutation corrections).

Package org.orekit.frames.configuration.eop

Class org.orekit.frames.configuration.eop.AbstractEOPHistory extends Object implements Serializable

serialVersionUID: 5659073889129159070L

Serialized Fields

interpolation_points

int interpolation_points

Number of points to use in interpolation.

entries

SortedSet<E> entries

Earth Orientation Parameter entries.

cache

TimeStampedCache<T extends TimeStamped> cache

EOP history entries.

interpolator

EOPInterpolators interpolator

Interpolation method.

Class org.orekit.frames.configuration.eop.EOP1980Entry extends EOPEntry implements Serializable

serialVersionUID: -8820663105212993131L

Class org.orekit.frames.configuration.eop.EOP1980History extends AbstractEOPHistory implements Serializable

serialVersionUID: 3000752420705950441L

Class org.orekit.frames.configuration.eop.EOP2000Entry extends EOPEntry implements Serializable

serialVersionUID: -6291063706005945705L

Class org.orekit.frames.configuration.eop.EOP2000History extends AbstractEOPHistory implements Serializable

serialVersionUID: 7042023586838112732L

Class org.orekit.frames.configuration.eop.EOP2000HistoryConstantOutsideInterval extends EOP2000History implements Serializable

serialVersionUID: 4948633092701598354L

Class org.orekit.frames.configuration.eop.EOPEntry extends Object implements Serializable

serialVersionUID: -3150843129484837222L

Serialized Fields

date

AbsoluteDate date

Entry date (absolute date).

dt

double dt

UT1-TAI.

lod

double lod

Length of day.

x

double x

X component of pole motion.

y

double y

Y component of pole motion.

dx

double dx

nutation correction for the X component of pole motion (IAU 2000) or longitude offset (IAU 1980).

dy

double dy

nutation correction for the Y component of pole motion (IAU 2000) or obliquity offset (IAU 1980).

Class org.orekit.frames.configuration.eop.NoEOP2000History extends EOP2000History implements Serializable

serialVersionUID: -7542790039542590139L

Class org.orekit.frames.configuration.eop.NutationCorrection extends Object implements Serializable

serialVersionUID: -2075750534145826411L

Serialized Fields

dy

double dy

δΔε₁₉₈₀ parameter (radians) or δX₂₀₀₀ parameter (radians).

dx

double dx

δΔψ₁₉₈₀ parameter (radians) or δY₂₀₀₀ parameter (radians).

Class org.orekit.frames.configuration.eop.PoleCorrection extends Object implements Serializable

serialVersionUID: 8695216598525302806L

Serialized Fields

xp

double xp

x_p parameter (radians).

yp

double yp

y_p parameter (radians).

Package org.orekit.frames.configuration.libration

Class org.orekit.frames.configuration.libration.IERS2010LibrationCorrection extends Object implements Serializable

serialVersionUID: 6397798546342916829L

Serialized Fields

lastPoleDate

AbsoluteDate lastPoleDate

Date of last pole correction computation.

lastPole

PoleCorrection lastPole

Last pole correction computation result.

lastPoleToken

Object lastPoleToken

Token for synchronization.

Class org.orekit.frames.configuration.libration.LibrationCorrectionPerThread extends Object implements Serializable

serialVersionUID: 5187461817288608329L

Serialized Fields

threadLocalModel

ThreadLocal<T> threadLocalModel

Will hold all thread-specific model instances.

Class org.orekit.frames.configuration.libration.NoLibrationCorrection extends Object implements Serializable

serialVersionUID: -808628503671630206L

Package org.orekit.frames.configuration.sp

Class org.orekit.frames.configuration.sp.IERS2003SPCorrection extends Object implements Serializable

serialVersionUID: 6357789880736142045L

Class org.orekit.frames.configuration.sp.IERS2010SPCorrection extends Object implements Serializable

serialVersionUID: -2941881252333180557L

Class org.orekit.frames.configuration.sp.NoSpCorrection extends Object implements Serializable

serialVersionUID: 2249593760120752952L

Package org.orekit.frames.transformations

Class org.orekit.frames.transformations.CIRFProvider extends Object implements Serializable

serialVersionUID: -8378289692425977657L

Class org.orekit.frames.transformations.EME2000Provider extends FixedTransformProvider implements Serializable

serialVersionUID: -6134137187835219727L

Class org.orekit.frames.transformations.EODProvider extends Object implements Serializable

serialVersionUID: 5619295588275758784L

Class org.orekit.frames.transformations.FixedTransformProvider extends Object implements Serializable

serialVersionUID: 7143912747227560905L

Serialized Fields

transform

Transform transform

Fixed transform.

Class org.orekit.frames.transformations.GTODProvider extends Object implements Serializable

serialVersionUID: -1727797229994466102L

Class org.orekit.frames.transformations.H0MinusNProvider extends FixedTransformProvider implements Serializable

serialVersionUID: -5974155860988189102L

Class org.orekit.frames.transformations.HelmertTransformation extends Object implements Serializable

serialVersionUID: -1900615992141291146L

Serialized Fields

cartesian

PVCoordinates cartesian

Cartesian part of the transform.

rotationVector

Vector3D rotationVector

Global rotation vector (applying rotation is done by computing cross product).

rotationRate

Vector3D rotationRate

First time derivative of the rotation (norm representing angular rate).

epoch

AbsoluteDate epoch

Reference epoch of the transform.

Class org.orekit.frames.transformations.InterpolatingTransformProvider extends Object implements Serializable

serialVersionUID: -1750070230136582364L

Serialization Methods

writeReplace

private Object writeReplace()

Replace the instance with a data transfer object for serialization.

This intermediate class serializes only the data needed for generation, but does not serializes the cache itself (in fact the cache is not serializable).

Serialized Fields

rawProvider

TransformProvider rawProvider

Provider for raw (non-interpolated) transforms.

useVelocities

boolean useVelocities

Flag for use of sample transforms velocities.

useRotationRates

boolean useRotationRates

Flag for use sample points rotation rates.

earliest

AbsoluteDate earliest

Earliest supported date.

latest

AbsoluteDate latest

Latest supported date.

step

double step

Grid points time step.

Class org.orekit.frames.transformations.ITRFEquinoxProvider extends Object implements Serializable

serialVersionUID: 6723470955343821599L

Serialized Fields

eopHistory

EOP1980History eopHistory

EOP history.

Class org.orekit.frames.transformations.ITRFProvider extends Object implements Serializable

serialVersionUID: -8320047148885526349L

Class org.orekit.frames.transformations.MODProvider extends Object implements Serializable

serialVersionUID: 8795437689936129851L

Class org.orekit.frames.transformations.TEMEProvider extends Object implements Serializable

serialVersionUID: 2701925895720334216L

Class org.orekit.frames.transformations.TIRFProvider extends Object implements Serializable

serialVersionUID: 7243684504752696164L

Class org.orekit.frames.transformations.TODProvider extends Object implements Serializable

serialVersionUID: 7013467596084047566L

Serialized Fields

eopHistory

EOP1980History eopHistory

EOP history.

Class org.orekit.frames.transformations.Transform extends Object implements Serializable

serialVersionUID: -8809893979516295102L

Serialized Fields

date

AbsoluteDate date

Date of the transform.

cartesian

PVCoordinates cartesian

Cartesian coordinates of the target frame with respect to the original frame.

angular

AngularCoordinates angular

Angular coordinates of the target frame with respect to the original frame.

Class org.orekit.frames.transformations.VEISProvider extends Object implements Serializable

serialVersionUID: 6918291423091809232L

Serialized Fields

eopHistory

EOP1980History eopHistory

EOP history.

Package org.orekit.models.earth

Class org.orekit.models.earth.FixedDelayModel extends Object implements Serializable

serialVersionUID: -92320711761929077L

Serialization Methods

readResolve

private Object readResolve()

Make sure the unserializable bivariate interpolation function is properly rebuilt.

Serialized Fields

xArr

double[] xArr

Abscissa grid for the bi-variate interpolation function read from the file.

yArr

double[] yArr

Ordinate grid for the bi-variate interpolation function read from the file.

fArr

double[][] fArr

Values samples for the bi-variate interpolation function read from the file.

height

double height

The height of the station in m above sea level [m].

Class org.orekit.models.earth.GeoMagneticElements extends Object implements Serializable

serialVersionUID: 1881493738280586855L

Serialized Fields

b

Vector3D b

The magnetic field vector (North=X, East=Y, Nadir=Z).

inclination

double inclination

The magnetic inclination in deg. down is positive, up is negative

declination

double declination

The magnetic declination in deg. east is positive, west is negative

totalIntensity

double totalIntensity

The magnetic total intensity, in nano Teslas.

horizontalIntensity

double horizontalIntensity

The magnetic horizontal intensity, in nano Teslas.

Package org.orekit.orbits

Class org.orekit.orbits.ApsisOrbit extends Orbit implements Serializable

serialVersionUID: 5565190329070785158L

Serialized Fields

parameters

ApsisRadiusParameters parameters

Orbital parameters.

Class org.orekit.orbits.CartesianOrbit extends Orbit implements Serializable

serialVersionUID: -5411308212620896302L

Serialized Fields

parameters

CartesianParameters parameters

Orbital parameters.

Class org.orekit.orbits.CircularOrbit extends Orbit implements Serializable

serialVersionUID: 5565190329070485158L

Serialized Fields

parameters

CircularParameters parameters

Orbital parameters.

Class org.orekit.orbits.EquatorialOrbit extends Orbit implements Serializable

serialVersionUID: 7593919633854535287L

Serialized Fields

parameters

EquatorialParameters parameters

Orbital parameters.

Class org.orekit.orbits.EquinoctialOrbit extends Orbit implements Serializable

serialVersionUID: -2000712440570076839L

Serialized Fields

parameters

EquinoctialParameters parameters

Orbital parameters.

Class org.orekit.orbits.KeplerianOrbit extends Orbit implements Serializable

serialVersionUID: 7593919633854535287L

Serialized Fields

parameters

KeplerianParameters parameters

Orbital parameters.

Class org.orekit.orbits.Orbit extends Object implements Serializable

serialVersionUID: 438733454597999578L

Serialized Fields

frame

Frame frame

Frame in which are defined the orbital parameters.

date

AbsoluteDate date

Date of the orbital parameters.

mu

double mu

Value of mu used to compute position and velocity (m³/s²).

pvCoordinates

PVCoordinates pvCoordinates

Computed PVCoordinates.

Package org.orekit.orbits.orbitalparameters

Class org.orekit.orbits.orbitalparameters.AbstractOrbitalParameters extends Object implements Serializable

serialVersionUID: -5728128534060266772L

Serialized Fields

mu

double mu

Value of mu used to compute position and velocity (m³/s²).

Class org.orekit.orbits.orbitalparameters.ApsisAltitudeParameters extends AbstractOrbitalParameters implements Serializable

serialVersionUID: -3849427714766900278L

Serialized Fields

periapsisAltitude

double periapsisAltitude

Periapsis altitude (m).

apoapsisAltitude

double apoapsisAltitude

Apoapsis altitude (m).

ae

double ae

Equatorial radius (m).

kepParameters

KeplerianParameters kepParameters

Keplerian parameters.

Class org.orekit.orbits.orbitalparameters.ApsisRadiusParameters extends AbstractOrbitalParameters implements Serializable

serialVersionUID: -4701713076176839228L

Serialized Fields

periapsis

double periapsis

Periapsis (m).

apoapsis

double apoapsis

Apoapsis (m).

kepParameters

KeplerianParameters kepParameters

Keplerian parameters.

Class org.orekit.orbits.orbitalparameters.CartesianParameters extends AbstractOrbitalParameters implements Serializable

serialVersionUID: -1963812828506172328L

Serialized Fields

pvCoordinates

PVCoordinates pvCoordinates

PV coordinates (x, y, z, xDot, yDot, zDot) (m and m/s).

Class org.orekit.orbits.orbitalparameters.CircularParameters extends AbstractOrbitalParameters implements Serializable

serialVersionUID: -5285991585368439144L

Serialized Fields

a

double a

Semi-major axis (m).

ex

double ex

First component of the circular eccentricity vector.

ey

double ey

Second component of the circular eccentricity vector.

i

double i

Inclination (rad).

raan

double raan

Right Ascension of Ascending Node (rad).

alphaV

double alphaV

True latitude argument (rad).

Class org.orekit.orbits.orbitalparameters.EquatorialParameters extends AbstractOrbitalParameters implements Serializable

serialVersionUID: 4180472353882013018L

Serialized Fields

a

double a

Semi-major axis (m).

e

double e

Eccentricity.

pomega

double pomega

ω + Ω (rad).

ix

double ix

first component of inclination vector (rad). ix = 2 sin(i/2) cos(Ω).

iy

double iy

second component of inclination vector (rad). iy = 2 sin(i/2) sin(Ω)

v

double v

anomaly (rad).

Class org.orekit.orbits.orbitalparameters.EquinoctialParameters extends AbstractOrbitalParameters implements Serializable

serialVersionUID: 4685153744711684793L

Serialized Fields

a

double a

Semi-major axis (m).

ex

double ex

First component of the eccentricity vector.

ey

double ey

Second component of the eccentricity vector.

hx

double hx

First component of the inclination vector.

hy

double hy

Second component of the inclination vector.

lv

double lv

True longitude argument (rad).

Class org.orekit.orbits.orbitalparameters.KeplerianParameters extends AbstractOrbitalParameters implements Serializable

serialVersionUID: -2848224139796971882L

Serialized Fields

a

double a

Semi-major axis (m).

e

double e

Eccentricity. (e >= 0)

i

double i

Inclination (rad).

pa

double pa

Perigee Argument (rad).

raan

double raan

Right Ascension of Ascending Node (rad).

v

double v

True anomaly (rad).

Class org.orekit.orbits.orbitalparameters.ReentryParameters extends AbstractOrbitalParameters implements Serializable

serialVersionUID: -3761689716075493731L

Serialized Fields

altitude

double altitude

Altitude (m).

latitude

double latitude

Latitude (m).

longitude

double longitude

Longitude (m).

velocity

double velocity

Velocity (m/s).

slope

double slope

Slope of velocity (rad).

azimuth

double azimuth

Azimuth of velocity (rad).

ae

double ae

Equatorial radius (m).

f

double f

Flattening.

Class org.orekit.orbits.orbitalparameters.StelaEquinoctialParameters extends AbstractOrbitalParameters implements Serializable

serialVersionUID: -3632727570913759537L

Serialized Fields

a

double a

Semi-major axis (m).

ex

double ex

First component of the eccentricity vector.

ey

double ey

Second component of the eccentricity vector.

ix

double ix

First component of the inclination vector.

iy

double iy

Second component of the inclination vector.

lM

double lM

Mean longitude argument (rad).

Package org.orekit.parameter

Class org.orekit.parameter.ConstantFunction extends ParamDiffFunction implements Serializable

serialVersionUID: -4651028856848403142L

Serialized Fields

parameter

Parameter parameter

Constant Parameter.

Class org.orekit.parameter.JacobiansParameterizable extends Parameterizable implements Serializable

serialVersionUID: 152206315837807025L

Serialized Fields

jacobiansParameters

ArrayList<E> jacobiansParameters

List of jacobian parameters. Only one instance of a parameter is allowed in the list.

Class org.orekit.parameter.LinearFunction extends ParamDiffFunction implements Serializable

serialVersionUID: -1536194879895016776L

Serialized Fields

a

Parameter a

Function slope.

b

Parameter b

ordinate origin.

date0

AbsoluteDate date0

The initial date.

Class org.orekit.parameter.ParamDiffFunction extends Parameterizable implements Serializable

serialVersionUID: -4609973799432090702L

Class org.orekit.parameter.Parameter extends Object implements Serializable

serialVersionUID: -723041676269653611L

Serialized Fields

value

double value

Parameter value.

name

String name

Parameter name.

Class org.orekit.parameter.Parameterizable extends Object implements Serializable

serialVersionUID: 3408804493769459294L

Serialized Fields

parameters

ArrayList<E> parameters

List of parameters. Only one instance of a parameter is allowed in the list.

Class org.orekit.parameter.PiecewiseFunction extends ParamDiffFunction implements Serializable

serialVersionUID: -4651028856848403142L

Serialized Fields

listOfFunction

ArrayList<E> listOfFunction

list of Functions.

listOfAbscissa

ArrayList<E> listOfAbscissa

list of connection points abscissa (date). The size of this list is listOfFunction.size() - 1

Package org.orekit.propagation

Class org.orekit.propagation.AbstractPropagator extends Object implements Serializable

serialVersionUID: 2434402795728927604L

Serialized Fields

mode

int mode

Propagation mode.

fixedStepSize

double fixedStepSize

Fixed step size.

stepHandler

OrekitStepHandler stepHandler

Step handler.

eventsStates

List<E> eventsStates

Event steps.

statesInitialized

boolean statesInitialized

Initialization indicator of events states.

additionalStateProviders

List<E> additionalStateProviders

Additional state providers.

interpolator

org.orekit.propagation.AbstractPropagator.BasicStepInterpolator interpolator

Internal steps interpolator.

startDate

AbsoluteDate startDate

Start date.

pvProvider

PVCoordinatesProvider pvProvider

Provider for attitude computation.

attitudeProviderForces

AttitudeProvider attitudeProviderForces

Attitude provider for forces computation.

attitudeProviderEvents

AttitudeProvider attitudeProviderEvents

Attitude provider for events computation.

attitudeProviderByDefault

AttitudeProvider attitudeProviderByDefault

Attitude provider given by default for one attitude.

isLastStep

boolean isLastStep

Indicator for last step.

isLastDetection

boolean isLastDetection

Indicator for last detection of the current detector.

initialState

SpacecraftState initialState

Initial state.

propagationFrame

Frame propagationFrame

Frame used for propagation.

Class org.orekit.propagation.AnalyticalIntegratedEphemeris extends AbstractPropagator implements Serializable

serialVersionUID: -2679532330842851649L

Serialized Fields

initialDates

List<E> initialDates

List of initial dates.

finalDates

List<E> finalDates

List of final dates.

initialStates

List<E> initialStates

List of initial state at initial date.

propagator

AbstractPropagator propagator

Propagator.

isForward

boolean isForward

True if propagation is forward, false if propagation is backward.

Class org.orekit.propagation.SpacecraftState extends Object implements Serializable

serialVersionUID: 3141803003950085500L

Serialized Fields

orbit

Orbit orbit

Orbital state.

attitude

Attitude attitude

Attitude for forces computation (attitude by default).

attitudeEvents

Attitude attitudeEvents

Attitude for events computation.

additionalStates

Map<K,V> additionalStates

Additional states.

Package org.orekit.propagation.analytical

Class org.orekit.propagation.analytical.AbstractLyddanePropagator extends AbstractPropagator implements Serializable

serialVersionUID: -1868667581720973969L

Serialized Fields

secularOrbitIn

Orbit secularOrbitIn

Secular orbit.

referenceRadius

double referenceRadius

Reference radius of the central body attraction model (m).

mu

double mu

Central attraction coefficient (m³/s²).

c20

double c20

Un-normalized 2nd zonal coefficient (about -1.08e-3 for Earth).

c30

double c30

Un-normalized 3rd zonal coefficient (about +2.53e-6 for Earth).

c40

double c40

Un-normalized 4th zonal coefficient (about +1.62e-6 for Earth).

c50

double c50

Un-normalized 5th zonal coefficient (about +2.28e-7 for Earth).

frame

Frame frame

Frame in which model coefficients are expressed.

Class org.orekit.propagation.analytical.AdapterPropagator extends AbstractPropagator implements Serializable

serialVersionUID: -5953975769121996528L

Serialized Fields

reference

Propagator reference

Underlying reference propagator.

effects

List<E> effects

Effects to add.

Class org.orekit.propagation.analytical.AnalyticalEphemerisModeHandler extends Object implements Serializable

serialVersionUID: -2554972295829753354L

Serialized Fields

initialDates

List<E> initialDates

List of initial dates.

finalDates

List<E> finalDates

List of final dates.

initialStates

List<E> initialStates

List of initial state at initial date.

propagator

AbstractPropagator propagator

Propagator.

isForward

boolean isForward

True if propagation is forward, false if propagation is backward.

attitudeForcesProvider

AttitudeProvider attitudeForcesProvider

Attitude provider for forces computation.

attitudeEventsProvider

AttitudeProvider attitudeEventsProvider

Attitude provider for events computation.

Class org.orekit.propagation.analytical.EcksteinHechlerPropagator extends AbstractPropagator implements Serializable

serialVersionUID: 1268374325750125229L

Serialized Fields

referenceRadius

double referenceRadius

Reference radius of the central body attraction model (m).

mu

double mu

Central attraction coefficient (m³/s²).

c20

double c20

Un-normalized zonal coefficient (about -1.08e-3 for Earth).

c30

double c30

Un-normalized zonal coefficient (about +2.53e-6 for Earth).

c40

double c40

Un-normalized zonal coefficient (about +1.62e-6 for Earth).

c50

double c50

Un-normalized zonal coefficient (about +2.28e-7 for Earth).

c60

double c60

Un-normalized zonal coefficient (about -5.41e-7 for Earth).

bodyFrame

Frame bodyFrame

Frame in which model coefficients are expressed.

internalParameters

org.orekit.propagation.analytical.EcksteinHechlerPropagator.PropagationParameters internalParameters

Propagation parameters : replaces old mean, q, ql, g1 ... g6, cos, 4 x sim parameters

Class org.orekit.propagation.analytical.J2DifferentialEffect extends Object implements Serializable

serialVersionUID: 3681516488729752197L

Serialized Fields

referenceDate

AbsoluteDate referenceDate

Reference date.

dPaDot

double dPaDot

Differential drift on perigee argument.

dRaanDot

double dRaanDot

Differential drift on ascending node.

applyBefore

boolean applyBefore

Indicator for applying effect before reference date.

Class org.orekit.propagation.analytical.J2SecularPropagator extends AbstractPropagator implements Serializable

serialVersionUID: -2889686029910875957L

Serialized Fields

referenceRadius

double referenceRadius

Reference radius of the central body attraction model (m).

mu

double mu

Central attraction coefficient (m³/s²).

c20

double c20

Un-normalized 2nd zonal coefficient (about -1.08e-3 for Earth).

frame

Frame frame

Frame in which model coefficients are expressed.

initialOrbitBodyFrame

KeplerianOrbit initialOrbitBodyFrame

Initial orbit in body frame (stored only to speed-up computation times).

Class org.orekit.propagation.analytical.KeplerianPropagator extends AbstractPropagator implements Serializable

serialVersionUID: 2094439036855266946L

Serialized Fields

initialState

SpacecraftState initialState

Initial state.

Class org.orekit.propagation.analytical.LyddaneLongPeriodPropagator extends AbstractLyddanePropagator implements Serializable

serialVersionUID: -7188025130926790802L

Class org.orekit.propagation.analytical.LyddaneSecularPropagator extends AbstractLyddanePropagator implements Serializable

serialVersionUID: 5508421209800631622L

Package org.orekit.propagation.analytical.covariance

Class org.orekit.propagation.analytical.covariance.OrbitCovariance extends Object implements Serializable

serialVersionUID: 4738799398400178791L

Serialized Fields

date

AbsoluteDate date

Date

frame

Frame frame

Reference Frame

type

OrbitType type

Coordinates Type

covariance

SymmetricMatrix covariance

Covariance Matrix

Package org.orekit.propagation.analytical.tle

Class org.orekit.propagation.analytical.tle.TLE extends Object implements Serializable

serialVersionUID: -1596648022319057689L

Serialized Fields

satelliteNumber

int satelliteNumber

The satellite number.

classification

char classification

Classification (U for unclassified).

launchYear

int launchYear

Launch year.

launchNumber

int launchNumber

Launch number.

launchPiece

String launchPiece

Piece of launch (from "A" to "ZZZ").

ephemerisType

int ephemerisType

Type of ephemeris.

elementNumber

int elementNumber

Element number.

epoch

AbsoluteDate epoch

the TLE current date.

meanMotion

double meanMotion

Mean motion (rad/s).

meanMotionFirstDerivative

double meanMotionFirstDerivative

Mean motion first derivative (rad/s²).

meanMotionSecondDerivative

double meanMotionSecondDerivative

Mean motion second derivative (rad/s³).

eccentricity

double eccentricity

Eccentricity.

inclination

double inclination

Inclination (rad).

pa

double pa

Argument of perigee (rad).

raan

double raan

Right Ascension of the Ascending node (rad).

meanAnomaly

double meanAnomaly

Mean anomaly (rad).

revolutionNumberAtEpoch

int revolutionNumberAtEpoch

Revolution number at epoch.

bStar

double bStar

Ballistic coefficient.

line1

String line1

First line.

line2

String line2

Second line.

Class org.orekit.propagation.analytical.tle.TLEPropagator extends AbstractPropagator implements Serializable

serialVersionUID: 6389584529961457799L

Serialized Fields

tle

TLE tle

Initial state.

xnode

double xnode

final RAAN.

a

double a

final semi major axis.

e

double e

final eccentricity.

i

double i

final inclination.

omega

double omega

final perigee argument.

xl

double xl

L from SPTRCK #3.

a0dp

double a0dp

original recovered semi major axis.

xn0dp

double xn0dp

original recovered mean motion.

cosi0

double cosi0

cosinus original inclination.

theta2

double theta2

cos io squared.

sini0

double sini0

sinus original inclination.

xmdot

double xmdot

common parameter for mean anomaly (M) computation.

omgdot

double omgdot

common parameter for perigee argument (omega) computation.

xnodot

double xnodot

common parameter for raan (OMEGA) computation.

e0sq

double e0sq

original eccentricity squared.

beta02

double beta02

1 - e2.

beta0

double beta0

sqrt (1 - e2).

perige

double perige

perigee, expressed in KM and ALTITUDE.

etasq

double etasq

eta squared.

eeta

double eeta

original eccentricity * eta.

s4

double s4

s* new value for the contant s.

tsi

double tsi

tsi from SPTRCK #3.

eta

double eta

eta from SPTRCK #3.

coef

double coef

coef for SGP C3 computation.

coef1

double coef1

coef for SGP C5 computation.

c1

double c1

C1 from SPTRCK #3.

c2

double c2

C2 from SPTRCK #3.

c4

double c4

C4 from SPTRCK #3.

xnodcf

double xnodcf

common parameter for raan (OMEGA) computation.

t2cof

double t2cof

3/2 * C1.

frame

Frame frame

TLE frame.

Class org.orekit.propagation.analytical.tle.TLESeries extends Object implements Serializable

serialVersionUID: -1120722267423537022L

Serialized Fields

supportedNames

String supportedNames

Regular expression for supported files names.

availableSatNums

Set<E> availableSatNums

Available satellite numbers.

tles

SortedSet<E> tles

Set containing all TLE entries.

filterSatelliteNumber

int filterSatelliteNumber

Satellite number used for filtering.

filterLaunchYear

int filterLaunchYear

Launch year used for filtering (all digits).

filterLaunchNumber

int filterLaunchNumber

Launch number used for filtering.

filterLaunchPiece

String filterLaunchPiece

Launch piece used for filtering.

TLE previous

Previous TLE in the cached selection.

TLE next

Next TLE in the cached selection.

lastTLE

TLE lastTLE

Last used TLE.

lastPropagator

TLEPropagator lastPropagator

Associated propagator.

firstDate

AbsoluteDate firstDate

Date of the first TLE.

lastDate

AbsoluteDate lastDate

Date of the last TLE.

ignoreNonTLELines

boolean ignoreNonTLELines

Indicator for non-TLE extra lines.

Package org.orekit.propagation.analytical.twod

Class org.orekit.propagation.analytical.twod.Analytical2DOrbitModel extends Object implements Serializable

serialVersionUID: 4776243268159796018L

Serialized Fields

smaModel

Analytical2DParameterModel smaModel

Orbit parameter model

exModel

Analytical2DParameterModel exModel

Orbit parameter model

eyModel

Analytical2DParameterModel eyModel

Orbit parameter model

incModel

Analytical2DParameterModel incModel

Orbit parameter model

lnaModel

Analytical2DParameterModel lnaModel

Orbit parameter model

aolModel

Analytical2DParameterModel aolModel

Orbit parameter model

massModel

MassProvider massModel

Spacecraft mass

muValue

double muValue

Standard gravitational parameter

devOrders

int[] devOrders

Trigonometric development orders [a, ex, ey, i lna, alpha]

Class org.orekit.propagation.analytical.twod.Analytical2DParameterModel extends Object implements Serializable

serialVersionUID: 2274624455870068728L

Serialized Fields

centeredModel

UnivariateDateFunction centeredModel

Centered part of the analytical model.

trigonometricCoefficients

double[][] trigonometricCoefficients

Trigonometric development coefficients.

Class org.orekit.propagation.analytical.twod.Analytical2DPropagator extends AbstractPropagator implements Serializable

serialVersionUID: -4001156899150568452L

Serialized Fields

orbitModel

Analytical2DOrbitModel orbitModel

Analytical 2D orbit model

devOrders

int[] devOrders

Orders of trigonometric developments. [sma, ex, ey, inc, lna, aol].

Package org.orekit.propagation.events

Class org.orekit.propagation.events.AbstractDetector extends Object implements Serializable

serialVersionUID: -8212002898109868489L

Serialized Fields

maxCheck

double maxCheck

Max check interval.

threshold

double threshold

Convergence threshold.

slopeSelection

int slopeSelection

Select all events, increasing g related events or decreasing g related events only.

Class org.orekit.propagation.events.AdaptedEventDetector extends Object implements Serializable

serialVersionUID: -5983739314228874403L

Serialized Fields

orbitType

OrbitType orbitType

Propagation orbit type.

angleType

PositionAngle angleType

Position angle type.

attitudeProviderForces

AttitudeProvider attitudeProviderForces

Attitude provider for forces computation.

attitudeProviderEvents

AttitudeProvider attitudeProviderEvents

Attitude provider for events computation.

detector

EventDetector detector

Underlying event detector.

referenceDate

AbsoluteDate referenceDate

Reference date from which t is counted.

mu

double mu

Central body attraction coefficient (m³/s²).

integrationFrame

Frame integrationFrame

integrationFrame frame in which integration is performed.

asinfos

Map<K,V> asinfos

Information needed to map the state array to additional states data.

Class org.orekit.propagation.events.AlignmentDetector extends AbstractDetector implements Serializable

serialVersionUID: -5512125598111644915L

Serialized Fields

body

PVCoordinatesProvider body

Body to align.

alignAngle

double alignAngle

Alignment angle (rad).

cosAlignAngle

double cosAlignAngle

Cosinus of alignment angle.

sinAlignAngle

double sinAlignAngle

Sinus of alignment angle.

actionAtAlignmentStart

EventDetector.Action actionAtAlignmentStart

Action performed when the alignment start.

actionAtAlignmentEnd

EventDetector.Action actionAtAlignmentEnd

Action performed when the alignment end.

removeAtAlignmentStart

boolean removeAtAlignmentStart

True if detector should be removed at alignment start.

removeAtAlignmentEnd

boolean removeAtAlignmentEnd

True if detector should be removed at alignment end.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.AltitudeDetector extends AbstractDetector implements Serializable

serialVersionUID: -1552109617025755015L

Serialized Fields

altitude

double altitude

Threshold altitude value (m).

bodyShape

BodyShape bodyShape

Body shape with respect to which altitude should be evaluated.

actionAtAscending

EventDetector.Action actionAtAscending

Action performed at altitude detection when ascending.

actionAtDescending

EventDetector.Action actionAtDescending

Action performed at altitude detection when descending.

removeAtAscending

boolean removeAtAscending

True if detector should be removed at ascending altitude detection.

removeAtDescending

boolean removeAtDescending

True if detector should be removed at ascending altitude detection.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.AnomalyDetector extends AbstractDetector implements Serializable

serialVersionUID: 1950385578566948721L

Serialized Fields

anomaly

double anomaly

Anomaly triggering the event.

type

PositionAngle type

Anomaly type.

actionAnomaly

EventDetector.Action actionAnomaly

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed.

Class org.orekit.propagation.events.AOLDetector extends AbstractDetector implements Serializable

serialVersionUID: 1950385578566948721L

Serialized Fields

aol

double aol

Angle triggering the event.

typeToDetect

PositionAngle typeToDetect

Type of angle triggering the event.

refFrame

Frame refFrame

Reference frame to compute AOL.

actionAOL

EventDetector.Action actionAOL

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed.

Class org.orekit.propagation.events.ApparentElevationDetector extends AbstractDetector implements Serializable

serialVersionUID: 2611286321482306850L

Serialized Fields

pressure

double pressure

Local pressure.

temperature

double temperature

Local temperature.

correfrac

double correfrac

Refraction correction from local pressure and temperature.

elevation

double elevation

Threshold apparent elevation value.

topo

TopocentricFrame topo

Topocentric frame in which elevation should be evaluated.

actionAtRaising

EventDetector.Action actionAtRaising

Action performed at apparent elevation detection at raising.

actionAtSetting

EventDetector.Action actionAtSetting

Action performed at apparent elevation detection at setting.

removeAtRaising

boolean removeAtRaising

True if detector should be removed at apparent elevation detection at raising.

removeAtSetting

boolean removeAtSetting

True if detector should be removed at apparent elevation detection at setting.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.ApsideDetector extends AbstractDetector implements Serializable

serialVersionUID: -7542434866922384844L

Serialized Fields

actionAtApogee

EventDetector.Action actionAtApogee

Action performed at apogee detection.

actionAtPerigee

EventDetector.Action actionAtPerigee

Action performed at perigee detection.

removeAtApogee

boolean removeAtApogee

True if detector should be removed at apogee detection.

removeAtPerigee

boolean removeAtPerigee

True if detector should be removed at perigee detection.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.BetaAngleDetector extends AbstractDetector implements Serializable

serialVersionUID: -523367166332164051L

Serialized Fields

angle

double angle

Angle triggering the event.

actionBetaAngle

EventDetector.Action actionBetaAngle

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed.

Class org.orekit.propagation.events.CircularFieldOfViewDetector extends AbstractDetector implements Serializable

serialVersionUID: 4571340030201230951L

Serialized Fields

targetPVProvider

PVCoordinatesProvider targetPVProvider

Position/velocity provider of the considered target.

center

Vector3D center

Direction of the fov center.

halfAperture

double halfAperture

Fov half aperture angle.

actionAtFovEntry

EventDetector.Action actionAtFovEntry

Action performed at fov entry.

actionAtFovExit

EventDetector.Action actionAtFovExit

Action performed at fov exit.

removeAtFovEntry

boolean removeAtFovEntry

True if detector should be removed at fov entry.

removeAtFovExit

boolean removeAtFovExit

True if detector should be removed at fov exit.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.DateDetector extends AbstractDetector implements Serializable

serialVersionUID: -334171965326514174L

Serialized Fields

gDate

AbsoluteDate gDate

Last date for g computation.

eventDateList

ArrayList<E> eventDateList

List of event dates.

currentIndex

int currentIndex

Current event date.

actionDate

EventDetector.Action actionDate

Action performed.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed.

Class org.orekit.propagation.events.DihedralFieldOfViewDetector extends AbstractDetector implements Serializable

serialVersionUID: 4571340030201230951L

Serialized Fields

targetPVProvider

PVCoordinatesProvider targetPVProvider

Position/velocity provider of the considered target.

center

Vector3D center

Direction of the fov center.

normalCenterPlane1

Vector3D normalCenterPlane1

Fov dihedral axis 1.

halfAperture1

double halfAperture1

Fov dihedral half aperture angle 1.

normalCenterPlane2

Vector3D normalCenterPlane2

Fov dihedral axis 2.

halfAperture2

double halfAperture2

Fov dihedral half aperture angle 2.

actionAtFovEntry

EventDetector.Action actionAtFovEntry

Action performed at fov entry.

actionAtFovExit

EventDetector.Action actionAtFovExit

Action performed at fov exit.

removeAtFovEntry

boolean removeAtFovEntry

True if detector should be removed at fov entry.

removeAtFovExit

boolean removeAtFovExit

True if detector should be removed at fov exit.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.DistanceDetector extends AbstractDetector implements Serializable

serialVersionUID: 8595027493313459831L

Serialized Fields

distance

double distance

Distance triggering the event.

body

PVCoordinatesProvider body

Distant body.

actionDistance

EventDetector.Action actionDistance

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed

Class org.orekit.propagation.events.EclipseDetector extends AbstractDetector implements Serializable

serialVersionUID: -541311550206363031L

Serialized Fields

occultingBody

PVCoordinatesProvider occultingBody

Occulting body.

occultingRadiusProvider

LocalRadiusProvider occultingRadiusProvider

Occulting body radius provider.

isOccultedBodyADirection

boolean isOccultedBodyADirection

True if the occulted body is a direction, false if it is a PVCoordinatesProvider.

occultedDirection

IDirection occultedDirection

Occulted direction.

occultedBody

PVCoordinatesProvider occultedBody

Occulted body.

occultedRadius

double occultedRadius

Occulted body radius (m).

totalEclipse

boolean totalEclipse

Umbra, if true, or penumbra, if false, detection flag.

lightingRatioDetection

boolean lightingRatioDetection

True if the eclipse detection is based on a lighting ratio value.

ratio

double ratio

The lighting ratio value (0 < ratio < 1, 0 for total eclipses, 1 for penumbra events).

actionAtEntry

EventDetector.Action actionAtEntry

Action performed when entering the eclipse.

actionAtExit

EventDetector.Action actionAtExit

Action performed when exiting the eclipse.

removeAtEntry

boolean removeAtEntry

True if detector should be removed when the spacecraft point enters the zone.

removeAtExit

boolean removeAtExit

True if detector should be removed when the spacecraft point leaves the zone.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.ElevationDetector extends AbstractDetector implements Serializable

serialVersionUID: 4571340030201230951L

Serialized Fields

elevation

double elevation

Threshold elevation value.

topo

TopocentricFrame topo

Topocentric frame in which elevation should be evaluated.

actionAtRaising

EventDetector.Action actionAtRaising

Action performed when propagation at raising.

actionAtSetting

EventDetector.Action actionAtSetting

Action performed when propagation at setting.

removeAtRaising

boolean removeAtRaising

True if detector should be removed at raising.

removeAtSetting

boolean removeAtSetting

True if detector should be removed at setting.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.EventShifter extends AbstractDetector implements Serializable

serialVersionUID: 4910163524748330428L

Serialized Fields

detector

EventDetector detector

Event detector for the raw unshifted event.

useShiftedStates

boolean useShiftedStates

Indicator for using shifted or unshifted states at event occurrence.

increasingOffset

double increasingOffset

Offset to apply to find increasing events.

decreasingOffset

double decreasingOffset

Offset to apply to find decreasing events.

Class org.orekit.propagation.events.EventsLogger extends Object implements Serializable

serialVersionUID: -8643810076248572648L

Serialized Fields

log

List<E> log

List of occurred events.

Class org.orekit.propagation.events.EventsLogger.LoggedEvent extends Object implements Serializable

serialVersionUID: -4491889728766419035L

Serialized Fields

detector

EventDetector detector

Event detector triggered.

state

SpacecraftState state

Triggering state.

increasing

boolean increasing

Increasing/decreasing status.

Class org.orekit.propagation.events.EventState extends Object implements Serializable

serialVersionUID: 4489391420715269318L

Serialized Fields

detector

EventDetector detector

Event detector.

initialDate

AbsoluteDate initialDate

Time at the beginning of the propagation.

t0

AbsoluteDate t0

Time at the beginning of the step.

t00

AbsoluteDate t00

Time at the beginning of the step.

g0

double g0

Value of the event detector at the beginning of the step.

g0Old

double g0Old

Value of the event detector at the beginning of the step.

pendingEvent

boolean pendingEvent

Indicator of event expected during the step.

pendingEventTime

AbsoluteDate pendingEventTime

Occurrence time of the pending event.

previousEventTime

AbsoluteDate previousEventTime

Occurrence time of the previous event.

forward

boolean forward

Integration direction.

increasing

boolean increasing

ariation direction around pending event. True: g function is going up, false: it is going down. This boolean is only kept to record slope of g function in case of event at t = 0.

nextAction

EventDetector.Action nextAction

Next action indicator.

remove

boolean remove

True if detector should be removed.

solver

UnivariateSolver solver

Root-finding algorithm to use to detect state events.

Class org.orekit.propagation.events.ExtremaDistanceDetector extends AbstractDetector implements Serializable

serialVersionUID: -6420170265427361960L

Serialized Fields

body

PVCoordinatesProvider body

Distant body.

actionMIN

EventDetector.Action actionMIN

Action performed at local minimum detection.

actionMAX

EventDetector.Action actionMAX

Action performed at local maximum detection.

removeMIN

boolean removeMIN

True if detector should be removed at minimum detection.

removeMAX

boolean removeMAX

True if detector should be removed at maximum detection.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.ExtremaElevationDetector extends AbstractDetector implements Serializable

serialVersionUID: -4883716696126831700L

Serialized Fields

topo

TopocentricFrame topo

Topocentric frame in which elevation should be evaluated.

actionExtremaElevation

EventDetector.Action actionExtremaElevation

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should de removed

Class org.orekit.propagation.events.ExtremaLatitudeDetector extends AbstractDetector implements Serializable

serialVersionUID: 8796265658333773051L

Serialized Fields

bodyFrameIn

Frame bodyFrameIn

The body frame.

actionExtremaLatitude

EventDetector.Action actionExtremaLatitude

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should de removed

Class org.orekit.propagation.events.ExtremaLongitudeDetector extends AbstractDetector implements Serializable

serialVersionUID: -247746125541484370L

Serialized Fields

bodyFrameIn

Frame bodyFrameIn

The body frame.

actionExtremaLongitude

EventDetector.Action actionExtremaLongitude

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should de removed

Class org.orekit.propagation.events.ExtremaThreeBodiesAngleDetector extends AbstractDetector implements Serializable

serialVersionUID: 8713027255126860524L

Serialized Fields

inSpacecraftId1

String inSpacecraftId1

the main spacecraft id

inSpacecraftId2

String inSpacecraftId2

the secondary spacecraft id

inSpacecraftId3

String inSpacecraftId3

the third spacecraft id

body1

PVCoordinatesProvider body1

First body.

body2

PVCoordinatesProvider body2

Second body.

body3

PVCoordinatesProvider body3

Third body.

actionMIN

EventDetector.Action actionMIN

Action performed at local minimum detection.

actionMAX

EventDetector.Action actionMAX

Action performed at local maximum detection.

removeMIN

boolean removeMIN

True if detector should be removed at local minimum detection.

removeMAX

boolean removeMAX

True if detector should be removed at local maximum detection.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

firstCall

boolean firstCall

True if g() method is called for the first time.

type

org.orekit.propagation.events.ExtremaThreeBodiesAngleDetector.PropagationType type

Type of the propagation (mono or multi).

Class org.orekit.propagation.events.GroundMaskElevationDetector extends AbstractDetector implements Serializable

serialVersionUID: -8124322408349693773L

Serialized Fields

azelmask

double[][] azelmask

Azimuth-elevation mask.

topo

TopocentricFrame topo

Topocentric frame in which azimuth and elevation should be evaluated.

actionAtRaising

EventDetector.Action actionAtRaising

Action performed when propagation at raising.

actionAtSetting

EventDetector.Action actionAtSetting

Action performed when propagation at setting.

removeAtRaising

boolean removeAtRaising

True if detector should be removed at raising.

removeAtSetting

boolean removeAtSetting

True if detector should be removed at setting.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.LatitudeDetector extends AbstractDetector implements Serializable

serialVersionUID: 2777403982588190629L

Serialized Fields

latToDetect

double latToDetect

latitude to detect

earthShape

BodyShape earthShape

the earth shape

actionAtIncreasing

EventDetector.Action actionAtIncreasing

Action performed when g increase.

actionAtDecreasing

EventDetector.Action actionAtDecreasing

Action performed when g decreasing.

removeAtIncreasing

boolean removeAtIncreasing

True if detector should be removed when g increase.

removeAtDecreasing

boolean removeAtDecreasing

True if detector should be removed when g decrease.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed (updated by eventOccured).

Class org.orekit.propagation.events.LocalTimeAngleDetector extends AbstractDetector implements Serializable

serialVersionUID: -8185366674138568798L

Serialized Fields

time

double time

Local time angle triggering the event.

localTimeObject

LocalTimeAngle localTimeObject

Local time.

lastLocalTimeDiff

double lastLocalTimeDiff

Last g() call local time difference to the reference to detect.

way

int way

Evolution way of the local time to the reference to detect.

actionLocalTime

EventDetector.Action actionLocalTime

Action performed.

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed.

Class org.orekit.propagation.events.LongitudeDetector extends AbstractDetector implements Serializable

serialVersionUID: -8263650183133893663L

Serialized Fields

longToDetect

double longToDetect

longitude to detect

centralBodyFrame

Frame centralBodyFrame

the frame of the central body

lastLongitudeDiff

double lastLongitudeDiff

last g() call longitude difference to the reference to detect

way

int way

evolution way of the longitude difference to the reference to detect

actionLong

EventDetector.Action actionLong

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed

Class org.orekit.propagation.events.NadirSolarIncidenceDetector extends AbstractDetector implements Serializable

serialVersionUID: 3009120047664790195L

Serialized Fields

inSun

PVCoordinatesProvider inSun

The Sun.

inEarth

BodyShape inEarth

The earth shape.

indenceRef

double indenceRef

incidence to detect

actionNadir

EventDetector.Action actionNadir

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed

Class org.orekit.propagation.events.NodeDetector extends AbstractDetector implements Serializable

serialVersionUID: 601812664015866572L

Serialized Fields

frame

Frame frame

Frame in which the equator is defined.

action_at_ascending_node

EventDetector.Action action_at_ascending_node

Action performed at ascending node detection.

action_at_descending_node

EventDetector.Action action_at_descending_node

Action performed at descending node detection.

remove_at_ascending_node

boolean remove_at_ascending_node

True if detector should be removed at ascending node detection.

remove_at_descending_node

boolean remove_at_descending_node

True if detector should be removed at descending node detection.

remove

boolean remove

True if detector should be removed (updated by eventOccurred).

Class org.orekit.propagation.events.NthOccurrenceDetector extends Object implements Serializable

serialVersionUID: -4109259106114272017L

Serialized Fields

event

EventDetector event

Event

nth

int nth

Occurrence to detect.

action

EventDetector.Action action

Behavior upon detection.

n

int n

Number of detected occurrences.

removeAtOcc

boolean removeAtOcc

True if detector should be removed after detection.

shouldBeRemoved

boolean shouldBeRemoved

Internal variable to indicate if event has been detected and detector should be removed after detection.

Class org.orekit.propagation.events.NullMassDetector extends AbstractDetector implements Serializable

serialVersionUID: 1L

Serialized Fields

mass

MassProvider mass

Mass provider.

triggered

boolean triggered

True is detector has been triggered.

Class org.orekit.propagation.events.NullMassPartDetector extends AbstractDetector implements Serializable

serialVersionUID: -8442909251407235384L

Serialized Fields

mass

MassProvider mass

Mass provider.

partName

String partName

Name of the part.

Class org.orekit.propagation.events.SolarTimeAngleDetector extends AbstractDetector implements Serializable

serialVersionUID: -9173356074954765598L

Serialized Fields

time

double time

Solar time angle triggering the event.

sun

CelestialBody sun

The Sun.

actionSolarTime

EventDetector.Action actionSolarTime

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed

Class org.orekit.propagation.events.ThreeBodiesAngleDetector extends AbstractDetector implements Serializable

serialVersionUID: -5302659256921813170L

Serialized Fields

inSpacecraftId1

String inSpacecraftId1

the main spacecraft id

inSpacecraftId2

String inSpacecraftId2

the secondary spacecraft id

inSpacecraftId3

String inSpacecraftId3

the third spacecraft id

body1

PVCoordinatesProvider body1

First body.

body2

PVCoordinatesProvider body2

Second body.

body3

PVCoordinatesProvider body3

Third body.

alignAngle

double alignAngle

Alignment angle (rad).

actionThreeBodiesAngle

EventDetector.Action actionThreeBodiesAngle

Action performed

shouldBeRemoved

boolean shouldBeRemoved

True if detector should be removed

firstCall

boolean firstCall

True if g() method is called for the first time.

type

org.orekit.propagation.events.ThreeBodiesAngleDetector.PropagationType type

Type of the propagation (mono or multi).

Package org.orekit.propagation.numerical

Class org.orekit.propagation.numerical.AdditionalStateInfo extends Object implements Serializable

serialVersionUID: 5113897187247487175L

Serialized Fields

size

int size

Size of the additional state.

index

int index

Index of the additional state in the state vector.

Class org.orekit.propagation.numerical.AttitudeEquation extends Object implements Serializable

serialVersionUID: 4597478286897057093L

Serialized Fields

name

String name

Equation name.

type

AttitudeEquation.AttitudeType type

Equation type.

Class org.orekit.propagation.numerical.Jacobianizer extends JacobiansParameterizable implements Serializable

serialVersionUID: 7736576299828036068L

Serialized Fields

forceModel

ForceModel forceModel

Wrapped force model instance.

hPos

double hPos

Step used for finite difference computation with respect to spacecraft position.

hParam

Map<K,V> hParam

Step used for finite difference computation with respect to parameters value.

nominal

org.orekit.propagation.numerical.Jacobianizer.AccelerationRetriever nominal

Dedicated adder used to retrieve nominal acceleration.

shifted

org.orekit.propagation.numerical.Jacobianizer.AccelerationRetriever shifted

Dedicated adder used to retrieve shifted acceleration.

Class org.orekit.propagation.numerical.JacobiansMapper extends Object implements Serializable

serialVersionUID: -2125324068169838971L

Serialized Fields

name

String name

Name.

parameters

int parameters

Number of Parameters.

parametersList

List<E> parametersList

Parameters list.

orbitType

OrbitType orbitType

Orbit type.

angleType

PositionAngle angleType

Position angle type.

Class org.orekit.propagation.numerical.NumericalPropagator extends Object implements Serializable

serialVersionUID: 3022312736994891425L

Serialized Fields

attitudeProviderForces

AttitudeProvider attitudeProviderForces

Attitude provider for forces computation.

attitudeProviderEvents

AttitudeProvider attitudeProviderEvents

Attitude provider for events computation.

attitudeProviderByDefault

AttitudeProvider attitudeProviderByDefault

Attitude provider given by default for one attitude.

newtonianAttraction

NewtonianAttraction newtonianAttraction

Central body attraction.

forceModels

List<E> forceModels

Force models used during the extrapolation of the Orbit, without jacobians.

detectors

List<E> detectors

Event detectors not related to force models.

stateVector

double[] stateVector

State vector.

startDate

AbsoluteDate startDate

Start date.

referenceDate

AbsoluteDate referenceDate

Reference date.

initialState

SpacecraftState initialState

Initial state to propagate.

currentState

SpacecraftState currentState

Current state to propagate.

calls

int calls

Counter for differential equations calls.

massModelHandler

AdaptedStepHandler massModelHandler

Mass model handler. If mass model equations are added to the propagator, the following handler is added in order to update the mass model with the final state value

nullMassDetector

NullMassDetector nullMassDetector

Null mass detector.

mode

int mode

Current mode.

orbitType

OrbitType orbitType

Propagation orbit type.

angleType

PositionAngle angleType

Position angle type.

addEquationsAndTolerances

List<E> addEquationsAndTolerances

Additional equations and associated integrator tolerances.

addStateInfos

Map<K,V> addStateInfos

Additional states informations.

propagationFrame

Frame propagationFrame

Frame used for propagation.

addStatesAbsoluteTolerances

double[] addStatesAbsoluteTolerances

User-specified absolute tolerances for additional states. Built from the additional tolerances of each additional equation.

addStatesRelativeTolerances

double[] addStatesRelativeTolerances

User-specified relative tolerances for additional states. Built from the additional tolerances of each additional equation.

Class org.orekit.propagation.numerical.ParameterConfiguration extends Object implements Serializable

serialVersionUID: 2247518849090889379L

Serialized Fields

jacobianParameter

Parameter jacobianParameter

Jacobian Parameter name.

hP

double hP

Parameter step for finite difference computation of partial derivative with respect to that parameter.

provider

IJacobiansParameterizable provider

Provider handling this parameter.

Class org.orekit.propagation.numerical.PartialDerivativesEquations extends Object implements Serializable

serialVersionUID: -556926704905099805L

Serialized Fields

ORBIT_DIMENSION

int ORBIT_DIMENSION

State vector dimension without additional parameters.

propagator

NumericalPropagator propagator

Selected parameters for Jacobian computation.

jacobiansProviders

List<E> jacobiansProviders

Jacobians providers.

selectedParameters

List<E> selectedParameters

List of parameters selected for Jacobians computation.

name

String name

Name.

isInitialJacobians

boolean isInitialJacobians

True if the initial Jacobians have not been initialized yet.

paramDim

int paramDim

Parameters vector dimension.

hPos

double hPos

Step used for finite difference computation with respect to spacecraft position.

dirty

boolean dirty

Boolean for force models / selected parameters consistency.

Package org.orekit.propagation.precomputed

Class org.orekit.propagation.precomputed.AbstractEphemeris extends AbstractPropagator implements Serializable

serialVersionUID: -2834940771588586668L

Serialized Fields

sortingAlgorithm

ISearchIndex sortingAlgorithm

Search index algorithm.

minDate

AbsoluteDate minDate

First date in range.

maxDate

AbsoluteDate maxDate

Last date in range.

areAddStatesSupported

boolean areAddStatesSupported

True if the spacecraft states contains additional states.

areAttitudesSupported

boolean areAttitudesSupported

True if the spacecraft states contains one or two attitudes.

isFirstIntervalInterp

boolean isFirstIntervalInterp

True if it is the first interpolation on this interval.

interpolationInterval

AbsoluteDateInterval interpolationInterval

Ephemeris interval of validity.

interpOrder

int interpOrder

Interpolation order. For example, it equals 2 for an Hermite interpolation, and should be even for a Lagrange interpolation.

stateTab

SpacecraftState[] stateTab

The SpacecraftStates array, chronologically sorted.

durationFromTab

double[] durationFromTab

The array of time duration from the first entry of data, chronologically sorted.

mu

double mu

Mu.

frame

Frame frame

Reference frame.

previousIndex

int previousIndex

At each call, the index is kept.

Class org.orekit.propagation.precomputed.Ephemeris extends AbstractPropagator implements Serializable

serialVersionUID: -1523460404698149239L

Serialization Methods

writeReplace

private Object writeReplace()

Replace the instance with a data transfer object for serialization.

This intermediate class serializes only the data needed for generation, but does not serializes the cache itself (in fact the cache is not serializable).

Serialized Fields

minDate

AbsoluteDate minDate

First date in range.

maxDate

AbsoluteDate maxDate

Last date in range.

Class org.orekit.propagation.precomputed.HermiteEphemeris extends AbstractEphemeris implements Serializable

serialVersionUID: 3907194454748535541L

Serialized Fields

dataAcc

Vector3D[] dataAcc

Deprecated.

Tabulated acc.

interpolatorPV

HermiteInterpolator interpolatorPV

Deprecated.

The Hermite Interpolator for position and velocity.

useAcceleration

boolean useAcceleration

Deprecated.

True if the spacecraft states contains a Vector3D with accelerations.

Class org.orekit.propagation.precomputed.IntegratedEphemeris extends AbstractPropagator implements Serializable

serialVersionUID: -2135002726640830424L

Serialized Fields

orbitType

OrbitType orbitType

Propagation orbit type.

angleType

PositionAngle angleType

Position angle type.

referenceFrame

Frame referenceFrame

Reference frame.

addStateInfos

Map<K,V> addStateInfos

Additional states informations.

mu

double mu

Central body gravitational constant.

startDates

List<E> startDates

List of start dates of the integration (can be min or max).

minDates

List<E> minDates

List of first date of the ranges.

maxDates

List<E> maxDates

List of last date of the ranges.

models

List<E> models

List of underlying raw mathematical models.

Class org.orekit.propagation.precomputed.LagrangeEphemeris extends AbstractEphemeris implements Serializable

serialVersionUID: -2879123785617566620L

Serialized Fields

interpolator

PolynomialFunctionLagrangeForm interpolator

Deprecated.

At each call, the Lagrange interpolator is kept.

t

double[] t

Deprecated.

Vector of durationFrom between the 1st interpolation point and all the interpolating points .

Package org.orekit.propagation.sampling

Class org.orekit.propagation.sampling.AdaptedStepHandler extends Object implements Serializable

serialVersionUID: -8067262257341902186L

Serialized Fields

orbitType

OrbitType orbitType

Propagation orbit type.

angleType

PositionAngle angleType

Position angle type.

attProviderForces

AttitudeProvider attProviderForces

Attitude provider for forces computation.

attProviderEvents

AttitudeProvider attProviderEvents

Attitude provider for events computation.

addStateInfos

Map<K,V> addStateInfos

Additional states informations.

initializedReference

AbsoluteDate initializedReference

Reference date.

interpolatedDate

AbsoluteDate interpolatedDate

Interpolated date ; by default, end of the current step.

initializedFrame

Frame initializedFrame

Reference frame.

initializedMu

double initializedMu

Central body attraction coefficient.

handler

OrekitStepHandler handler

Underlying handler.

activate

boolean activate

Flag for handler .

rawInterpolator

StepInterpolator rawInterpolator

Underlying raw rawInterpolator.

Class org.orekit.propagation.sampling.BasicStepInterpolator extends Object implements Serializable

serialVersionUID: 7847540541046397037L

Serialized Fields

propagator

Propagator propagator

Underlying propagator.

previousDate

AbsoluteDate previousDate

Previous date.

currentDate

AbsoluteDate currentDate

Current date.

interpolatedState

SpacecraftState interpolatedState

Interpolated State.

forward

boolean forward

Forward propagation indicator.

Class org.orekit.propagation.sampling.OrekitStepHandlerMultiplexer extends Object implements Serializable

serialVersionUID: -5957903354538173269L

Serialized Fields

handlers

List<E> handlers

Underlying step handlers.

Class org.orekit.propagation.sampling.OrekitStepNormalizer extends Object implements Serializable

serialVersionUID: 6335110162884693078L

Serialized Fields

h

double h

Fixed time step.

handler

OrekitFixedStepHandler handler

Underlying step handler.

lastDate

AbsoluteDate lastDate

Last step date.

lastState

SpacecraftState lastState

Last State vector.

forward

boolean forward

Integration direction indicator.

Package org.orekit.time

Class org.orekit.time.AbsoluteDate extends Object implements Serializable

serialVersionUID: 617061803741806846L

Serialized Fields

epoch

long epoch

Reference epoch in seconds from 2000-01-01T12:00:00 TAI.

Beware, it is not AbsoluteDate.J2000_EPOCH since it is in TAI and not in TT.

offset

double offset

Offset from the reference epoch in seconds.

Class org.orekit.time.ChronologicalComparator extends Object implements Serializable

serialVersionUID: 3092980292741000025L

Class org.orekit.time.DateComponents extends Object implements Serializable

serialVersionUID: -2462694707837970938L

Serialized Fields

year

int year

Year number.

month

int month

Month number.

day

int day

Day number.

Class org.orekit.time.DateTimeComponents extends Object implements Serializable

serialVersionUID: 5061129505488924484L

Serialized Fields

date

DateComponents date

Date component.

time

TimeComponents time

Time component.

Class org.orekit.time.TimeComponents extends Object implements Serializable

serialVersionUID: -8566834296299377436L

Serialized Fields

hour

int hour

Hour number.

minute

int minute

Minute number.

second

double second

Second number.

Class org.orekit.time.TimeScalesFactory extends Object implements Serializable

serialVersionUID: -2063625014942931917L

Package org.orekit.utils

Class org.orekit.utils.AbsoluteDateInterval extends ComparableInterval<AbsoluteDate> implements Serializable

serialVersionUID: -2265247850750610628L

Class org.orekit.utils.AbsoluteDateIntervalsList extends TreeSet<AbsoluteDateInterval> implements Serializable

serialVersionUID: -5112507046887326180L

Class org.orekit.utils.AngularCoordinates extends Object implements Serializable

serialVersionUID: 3750363056414336775L

Serialized Fields

rotation

Rotation rotation

Rotation.

rotationRate

Vector3D rotationRate

Rotation rate.

rotationAcceleration

Vector3D rotationAcceleration

Rotation acceleration.

Class org.orekit.utils.CardanMountPosition extends Object implements Serializable

serialVersionUID: -3033892402533461901L

Serialized Fields

x

double x

Angle of the roation around x axis.

y

double y

Angle of the rotation around y' axis (image of y axis by the rotation around x axis).

r

double r

Distance from the origin of the frame.

Class org.orekit.utils.CardanMountPV extends Object implements Serializable

serialVersionUID: -7989767234360618822L

Serialized Fields

x

double x

Angle of the roation around x axis.

y

double y

Angle of the rotation around y' axis (image of y axis by the rotation around x axis).

r

double r

Distance from the origin of the frame.

xRate

double xRate

The angle rate of the rotation around x axis.

yRate

double yRate

The angle rate of the rotation around y' axis (image of y axis by the rotation around x axis).

rRate

double rRate

The range rate.

Class org.orekit.utils.ComparableInterval extends GenericInterval<T extends Comparable<T>> implements Serializable

serialVersionUID: -3043430443585844772L

Serialized Fields

hashCode

int hashCode

Hash code.

Class org.orekit.utils.GenericInterval extends Object implements Serializable

serialVersionUID: 4134192354278539190L

Serialized Fields

lowerEndpoint

IntervalEndpointType lowerEndpoint

Interval type for the lower end of the interval.

upperEndpoint

IntervalEndpointType upperEndpoint

Interval type for the upper end of the interval.

lowerData

Object lowerData

lower end data value.

upperData

Object upperData

upper end data value.

Class org.orekit.utils.PVCoordinates extends Object implements Serializable

serialVersionUID: 4157449919684833834L

Serialized Fields

position

Vector3D position

The position.

velocity

Vector3D velocity

The velocity.

acceleration

Vector3D acceleration

The acceleration.

Class org.orekit.utils.TimeStampedAngularCoordinates extends AngularCoordinates implements Serializable

serialVersionUID: 20140723L

Serialized Fields

date

AbsoluteDate date

The date.

Class org.orekit.utils.TimeStampedPVCoordinates extends PVCoordinates implements Serializable

serialVersionUID: 20140723L

Serialized Fields

date

AbsoluteDate date

The date.

Class org.orekit.utils.TopocentricPosition extends Object implements Serializable

serialVersionUID: -5115813588245021791L

Serialized Fields

e

double e

Elevation angle.

a

double a

Azimuth angle.

r

double r

Distance from the origin.

Class org.orekit.utils.TopocentricPV extends Object implements Serializable

serialVersionUID: 6047068671778435002L

Serialized Fields

e

double e

Elevation angle.

a

double a

Azimuth angle.

r

double r

Distance from the origin.

eRate

double eRate

Elevation rate.

aRate

double aRate

Azimuth rate.

rRate

double rRate

Range rate.

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