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| Packages that use AbsoluteDateInterval | |
|---|---|
| fr.cnes.sirius.patrius.events | |
| fr.cnes.sirius.patrius.events.multi | |
| fr.cnes.sirius.patrius.events.postprocessing | |
| fr.cnes.sirius.patrius.guidance | |
| org.orekit.attitudes | This package provides classes to represent simple attitudes. |
| org.orekit.frames.configuration | |
| org.orekit.propagation.precomputed | |
| org.orekit.utils | This package provides useful objects. |
| Uses of AbsoluteDateInterval in fr.cnes.sirius.patrius.events |
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| Methods in fr.cnes.sirius.patrius.events that return AbsoluteDateInterval | |
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AbsoluteDateInterval |
Phenomenon.getTimespan()
Get the timespan as an AbsoluteDateInterval. |
| Methods in fr.cnes.sirius.patrius.events with parameters of type AbsoluteDateInterval | |
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Map<CodingEventDetector,PhenomenaList> |
CodedEventsLogger.buildPhenomenaListMap(AbsoluteDateInterval definitionInterval,
SpacecraftState duringState)
Builds a map of PhenomenaList, one list per CodingEventDetector instance. |
Set<Phenomenon> |
PhenomenaList.getPhenomena(String code,
String comment,
AbsoluteDateInterval interval)
Finds one/more events in the list of Phenomenon following some criteria.When a comment and a time interval are available, the method looks for a specific phenomenon in the list, otherwise if only the code is given as input, it looks for a list of phenomena with the same code. |
| Uses of AbsoluteDateInterval in fr.cnes.sirius.patrius.events.multi |
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| Methods in fr.cnes.sirius.patrius.events.multi with parameters of type AbsoluteDateInterval | |
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Map<MultiCodingEventDetector,PhenomenaList> |
MultiCodedEventsLogger.buildPhenomenaListMap(AbsoluteDateInterval definitionInterval,
Map<String,SpacecraftState> duringState)
Builds a map of PhenomenaList, one list per MultiCodingEventDetector instance. |
| Uses of AbsoluteDateInterval in fr.cnes.sirius.patrius.events.postprocessing |
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| Methods in fr.cnes.sirius.patrius.events.postprocessing that return AbsoluteDateInterval | |
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AbsoluteDateInterval |
Timeline.getIntervalOfValidity()
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| Constructors in fr.cnes.sirius.patrius.events.postprocessing with parameters of type AbsoluteDateInterval | |
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TimeFilter(AbsoluteDateInterval timeInterval,
boolean removeAll)
Build an instance of TimeFilter from a time interval. |
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TimeFilter(List<String> listCode,
AbsoluteDateInterval timeInterval,
boolean removeAll)
Build an instance of TimeFilter from a time interval. |
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TimeFilter(String elementCode,
AbsoluteDateInterval timeInterval,
boolean removeAll)
Build an instance of TimeFilter from a time interval. |
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Timeline(CodedEventsLogger logger,
AbsoluteDateInterval interval)
Builds an instance of the timeline from a CodedEventsLogger, generating the list of detected events and
the list of corresponding phenomena.These events and phenomena are the output of a propagation with events detector; the coherence between events and phenomena should be guaranteed by the detection process during propagation. |
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| Uses of AbsoluteDateInterval in fr.cnes.sirius.patrius.guidance |
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| Methods in fr.cnes.sirius.patrius.guidance that return AbsoluteDateInterval | |
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AbsoluteDateInterval |
Vector3DPolynomialSegment.getTimeInterval()
Get the time interval of the guidance profile segment. |
AbsoluteDateInterval |
GuidanceProfile.getTimeInterval()
|
AbsoluteDateInterval |
QuaternionPolynomialSegment.getTimeInterval()
Get the time interval of the guidance profile segment. |
| Methods in fr.cnes.sirius.patrius.guidance that return types with arguments of type AbsoluteDateInterval | |
|---|---|
Map<AbsoluteDateInterval,double[]> |
QuaternionPolynomialProfile.getQ0Coefficients()
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Map<AbsoluteDateInterval,double[]> |
QuaternionPolynomialProfile.getQ1Coefficients()
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Map<AbsoluteDateInterval,double[]> |
QuaternionPolynomialProfile.getQ2Coefficients()
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Map<AbsoluteDateInterval,double[]> |
QuaternionPolynomialProfile.getQ3Coefficients()
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Map<AbsoluteDateInterval,double[]> |
AngularVelocitiesPolynomialProfile.getXCoefficients()
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Map<AbsoluteDateInterval,double[]> |
AngularVelocitiesPolynomialProfile.getYCoefficients()
|
Map<AbsoluteDateInterval,double[]> |
AngularVelocitiesPolynomialProfile.getZCoefficients()
|
| Constructors in fr.cnes.sirius.patrius.guidance with parameters of type AbsoluteDateInterval | |
|---|---|
AngularVelocitiesHarmonicProfile(AbsoluteDate origin,
Rotation initialRotation,
Frame frame,
FourierSeries xAngle,
FourierSeries yAngle,
FourierSeries zAngle,
AbsoluteDateInterval timeInterval,
KinematicsToolkit.IntegrationType integType,
double integStep)
Create a harmonic, angular velocities guidance profile. |
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AngularVelocitiesPolynomialProfile(Frame frame,
AbsoluteDateInterval timeInterval,
Rotation initialRotation,
List<Vector3DPolynomialSegment> polynomials,
KinematicsToolkit.IntegrationType integType,
double integStep)
Create a polynomial, angular velocity guidance profile. |
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GuidanceProfile(AbsoluteDateInterval timeInterval)
Constructor |
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QuaternionHarmonicProfile(AbsoluteDate origin,
Frame frame,
FourierSeries q0,
FourierSeries q1,
FourierSeries q2,
FourierSeries q3,
AbsoluteDateInterval timeInterval)
Create a harmonic, quaternion guidance profile. |
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QuaternionPolynomialProfile(Frame frame,
AbsoluteDateInterval timeInterval,
List<QuaternionPolynomialSegment> polynomials)
Create a polynomial, quaternion guidance profile. |
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QuaternionPolynomialSegment(PolynomialFunctionLagrangeForm q0,
PolynomialFunctionLagrangeForm q1,
PolynomialFunctionLagrangeForm q2,
PolynomialFunctionLagrangeForm q3,
AbsoluteDate date0,
AbsoluteDateInterval timeInterval)
Build a quaternion polynomial guidance profile on a segment. The polynomial representing the quaternion components are on lagrange form. |
|
QuaternionPolynomialSegment(PolynomialFunction q0,
PolynomialFunction q1,
PolynomialFunction q2,
PolynomialFunction q3,
AbsoluteDate date0,
AbsoluteDateInterval timeInterval)
Build a quaternion polynomial guidance profile on a segment. The polynomial representing the quaternion components are generic polynomial functions. |
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Vector3DPolynomialSegment(PolynomialFunctionLagrangeForm x,
PolynomialFunctionLagrangeForm y,
PolynomialFunctionLagrangeForm z,
AbsoluteDate date0,
AbsoluteDateInterval timeInterval)
Build an angular velocity polynomial guidance profile on a segment. The polynomial representing the vector 3D components are on lagrange form. |
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Vector3DPolynomialSegment(PolynomialFunction x,
PolynomialFunction y,
PolynomialFunction z,
AbsoluteDate date0,
AbsoluteDateInterval timeInterval)
Build an angular velocity polynomial guidance profile on a segment. The polynomial representing the vector 3D components are generic polynomial functions. |
|
| Uses of AbsoluteDateInterval in org.orekit.attitudes |
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| Fields in org.orekit.attitudes declared as AbsoluteDateInterval | |
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protected AbsoluteDateInterval |
AbstractSlew.intervalOfValidity
Interval of validity of the maneuver (with closed endpoints). |
| Methods in org.orekit.attitudes that return AbsoluteDateInterval | |
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AbsoluteDateInterval |
AttitudeLawLeg.getTimeInterval()
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AbsoluteDateInterval |
TabulatedAttitude.getTimeInterval()
Return the time interval of validity |
AbsoluteDateInterval |
AbstractSlew.getTimeInterval()
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AbsoluteDateInterval |
AttitudeLegsSequence.getTimeInterval()
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AbsoluteDateInterval |
RelativeTabulatedAttitudeLeg.getTimeInterval()
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AbsoluteDateInterval |
AttitudeLeg.getTimeInterval()
Return the time interval of validity |
| Methods in org.orekit.attitudes with parameters of type AbsoluteDateInterval | |
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protected boolean |
FixedStepAttitudeEphemerisGenerator.addLastPoint(AbsoluteDateInterval ephemerisInterval)
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protected abstract boolean |
AbstractAttitudeEphemerisGenerator.addLastPoint(AbsoluteDateInterval ephemerisInterval)
Decide if adding the last point of the time interval to the ephemeris list. |
protected boolean |
VariableStepAttitudeEphemerisGenerator.addLastPoint(AbsoluteDateInterval ephemerisInterval)
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protected double |
FixedStepAttitudeEphemerisGenerator.computeStep(AbsoluteDate date,
AbsoluteDateInterval ephemerisInterval)
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protected abstract double |
AbstractAttitudeEphemerisGenerator.computeStep(AbsoluteDate date,
AbsoluteDateInterval ephemerisInterval)
Computes the step used during attitude ephemeris generation. |
protected double |
VariableStepAttitudeEphemerisGenerator.computeStep(AbsoluteDate date,
AbsoluteDateInterval ephemerisInterval)
Computes the step used during the variable step ephemeris generation. |
SortedSet<Attitude> |
AbstractAttitudeEphemerisGenerator.generateEphemeris(AbsoluteDateInterval ephemerisInterval,
Frame frame)
Computes attitude ephemeris using a fixed or variable time step and choosing the interval of validity. |
TabulatedAttitude |
TabulatedAttitude.setTimeInterval(AbsoluteDateInterval interval)
Return a new law with the specified interval. |
| Uses of AbsoluteDateInterval in org.orekit.frames.configuration |
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| Methods in org.orekit.frames.configuration that return AbsoluteDateInterval | |
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AbsoluteDateInterval |
FramesConfigurationImplementation.getTimeIntervalOfValidity()
Get the time interval of validity. |
AbsoluteDateInterval |
FramesConfiguration.getTimeIntervalOfValidity()
Time interval of validity for the EOP files. |
| Uses of AbsoluteDateInterval in org.orekit.propagation.precomputed |
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| Fields in org.orekit.propagation.precomputed declared as AbsoluteDateInterval | |
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protected AbsoluteDateInterval |
AbstractEphemeris.interpolationInterval
Ephemeris interval of validity. |
| Methods in org.orekit.propagation.precomputed that return AbsoluteDateInterval | |
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protected AbsoluteDateInterval |
AbstractEphemeris.intervalValidity(SpacecraftState[] tab)
Corrects the min and max dates with the constraint of the number of interpolations points required. |
| Methods in org.orekit.propagation.precomputed with parameters of type AbsoluteDateInterval | |
|---|---|
static SpacecraftState[] |
AbstractEphemeris.generateSpacecraftState(PVCoordinatesProvider pvProv,
AttitudeProvider attProvForces,
AttitudeProvider attProvEvents,
double step,
AbsoluteDateInterval ptsInterval,
Frame frame,
double mu)
Creates a spacecraft array with constant step size. |
| Constructors in org.orekit.propagation.precomputed with parameters of type AbsoluteDateInterval | |
|---|---|
HermiteEphemeris(PVCoordinatesProvider pvProv,
AttitudeProvider attProvForces,
AttitudeProvider attProvEvents,
double step,
AbsoluteDateInterval intervalOfPoints,
Frame frame2,
double mu2)
Deprecated. Constructor n°1 using a PV coordinates provider and an AttitudeProvider to build the interpolation points. |
|
LagrangeEphemeris(PVCoordinatesProvider pvProv,
AttitudeProvider attProvForces,
AttitudeProvider attProvEvents,
double step,
AbsoluteDateInterval intervalOfPoints,
Frame frame,
double mu)
Deprecated. Constructor using a PV coordinates provider and an AttitudeProvider to build the interpolation points, defaulting to 8th order for the Lagrange interpolator. |
|
LagrangeEphemeris(PVCoordinatesProvider pvProv,
AttitudeProvider attProvForces,
AttitudeProvider attProvEvents,
double step,
AbsoluteDateInterval intervalOfPoints,
Frame frame,
double mu,
int order)
Deprecated. Constructor using a PV coordinates provider and an AttitudeProvider to build the interpolation points. |
|
| Uses of AbsoluteDateInterval in org.orekit.utils |
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| Methods in org.orekit.utils that return AbsoluteDateInterval | |
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AbsoluteDateInterval |
AbsoluteDateIntervalsList.getInclusiveInterval()
Gets the shortest interval containing all the intervals belonging to the list. While a date included in at least one of the listed intervals must be contained in this global interval, the opposite is not guaranteed (the inclusive interval can contain dates that do not belong to any listed interval). |
AbsoluteDateInterval |
AbsoluteDateInterval.getIntersectionWith(AbsoluteDateInterval interval)
Intersects the interval with another interval if possible (i.e. |
AbsoluteDateInterval |
AbsoluteDateInterval.mergeTo(AbsoluteDateInterval interval)
Merges the interval with another interval if possible (i.e. |
| Methods in org.orekit.utils with parameters of type AbsoluteDateInterval | |
|---|---|
int |
AbsoluteDateInterval.compareDurationTo(AbsoluteDateInterval interval)
Checks if the duration of the interval is longer, shorter or equal to the duration of another interval. It returns a positive integer if the duration is longer, a negative integer if the duration is shorter and zero if the durations of the two intervals are identical. The method checks also the lower and upper end points of the intervals, considering that an interval with an open end point is shorter than an interval with the same duration and a closed end point. |
double |
AbsoluteDateInterval.durationFrom(AbsoluteDateInterval interval)
Computes the duration in seconds between the two intervals. The duration between two intervals is the duration between the end of the earlier interval and the beginning of the later. If the intervals overlap, this duration is 0. The sign of the result is positive if the given interval comes earlier. |
AbsoluteDateInterval |
AbsoluteDateInterval.getIntersectionWith(AbsoluteDateInterval interval)
Intersects the interval with another interval if possible (i.e. |
AbsoluteDateInterval |
AbsoluteDateInterval.mergeTo(AbsoluteDateInterval interval)
Merges the interval with another interval if possible (i.e. |
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