Uses of Interface
fr.cnes.sirius.patrius.propagation.MassProvider

Packages that use MassProvider

Package	Description
fr.cnes.sirius.patrius.assembly.models
fr.cnes.sirius.patrius.forces.maneuvers
fr.cnes.sirius.patrius.propagation
fr.cnes.sirius.patrius.propagation.analytical
fr.cnes.sirius.patrius.propagation.analytical.tle
fr.cnes.sirius.patrius.propagation.analytical.twod
fr.cnes.sirius.patrius.propagation.events
fr.cnes.sirius.patrius.propagation.numerical
fr.cnes.sirius.patrius.propagation.numerical.multi

Uses of MassProvider in fr.cnes.sirius.patrius.assembly.models

Subinterfaces of MassProvider in fr.cnes.sirius.patrius.assembly.models

Modifier and Type	Interface and Description
interface	IInertiaModel

Classes in fr.cnes.sirius.patrius.assembly.models that implement MassProvider

Modifier and Type	Class and Description
class	InertiaComputedModel This class is an inertia model computed from the inertia properties of each parts of an Assembly object.
class	InertiaSimpleModel Simple inertia model : the mass, mass center and inertia matrix are directly given by the user.
class	MassModel This class represents a mass model for an assembly with parts that have mass properties.

Uses of MassProvider in fr.cnes.sirius.patrius.forces.maneuvers

Methods in fr.cnes.sirius.patrius.forces.maneuvers that return MassProvider

Modifier and Type	Method and Description
MassProvider	ContinuousThrustManeuver.getMassModel()

Constructors in fr.cnes.sirius.patrius.forces.maneuvers with parameters of type MassProvider

Constructor and Description
ContinuousThrustManeuver(AbsoluteDate date, double duration, PropulsiveProperty engine, IDependentVectorVariable<SpacecraftState> inDirection, MassProvider massProvider, TankProperty tank) Constructor for a variable direction in satellite frame.
ContinuousThrustManeuver(AbsoluteDate date, double duration, PropulsiveProperty engine, IDependentVectorVariable<SpacecraftState> inDirection, MassProvider massProvider, TankProperty tank, Frame frameIn) Constructor for a variable direction in provided frame.
ContinuousThrustManeuver(AbsoluteDate date, double duration, PropulsiveProperty engine, IDependentVectorVariable<SpacecraftState> inDirection, MassProvider massProvider, TankProperty tank, LOFType lofTyp) Constructor for a variable direction in provided local orbital frame.
ContinuousThrustManeuver(AbsoluteDate date, double duration, PropulsiveProperty engine, Vector3D inDirection, MassProvider massProvider, TankProperty tank) Constructor for a constant direction in satellite frame.
ContinuousThrustManeuver(AbsoluteDate date, double duration, PropulsiveProperty engine, Vector3D inDirection, MassProvider massProvider, TankProperty tank, Frame frameIn) Constructor for a constant direction in provided frame.
ContinuousThrustManeuver(AbsoluteDate date, double duration, PropulsiveProperty engine, Vector3D inDirection, MassProvider massProvider, TankProperty tank, LOFType lofTyp) Constructor for a constant direction in provided local orbital frame.
ContinuousThrustManeuver(EventDetector startEventDetector, EventDetector stopEventDetector, PropulsiveProperty engine, IDependentVectorVariable<SpacecraftState> inDirection, MassProvider massProvider, TankProperty tank) Constructor for a variable direction in satellite frame.
ContinuousThrustManeuver(EventDetector startEventDetector, EventDetector stopEventDetector, PropulsiveProperty engine, IDependentVectorVariable<SpacecraftState> inDirection, MassProvider massProvider, TankProperty tank, Frame frameIn) Constructor for a variable direction in provided frame.
ContinuousThrustManeuver(EventDetector startEventDetector, EventDetector stopEventDetector, PropulsiveProperty engine, IDependentVectorVariable<SpacecraftState> inDirection, MassProvider massProvider, TankProperty tank, LOFType lofTyp) Constructor for a variable direction in local orbital frame.
ContinuousThrustManeuver(EventDetector startEventDetector, EventDetector stopEventDetector, PropulsiveProperty engine, Vector3D inDirection, MassProvider massProvider, TankProperty tank) Constructor for a constant direction in satellite frame.
ContinuousThrustManeuver(EventDetector startEventDetector, EventDetector stopEventDetector, PropulsiveProperty engine, Vector3D inDirection, MassProvider massProvider, TankProperty tank, Frame frameIn) Constructor for a constant direction in provided frame.
ContinuousThrustManeuver(EventDetector startEventDetector, EventDetector stopEventDetector, PropulsiveProperty engine, Vector3D inDirection, MassProvider massProvider, TankProperty tank, LOFType lofTyp) Constructor for a constant direction in local orbital frame.
ImpulseManeuver(EventDetector inTrigger, Vector3D inDeltaVSat, double isp, MassProvider massModel, String part) Build a new instance.
ImpulseManeuver(EventDetector inTrigger, Vector3D inDeltaVSat, double isp, MassProvider massModel, String part, LOFType inLofType) Build a new instance with a LocalOrbitalFrame.
ImpulseManeuver(EventDetector inTrigger, Vector3D inDeltaVSat, Frame inFrame, double isp, MassProvider massModel, String part) Build a new instance.
ImpulseManeuver(EventDetector inTrigger, Vector3D inDeltaVSat, Frame inFrame, PropulsiveProperty engine, MassProvider massModel, TankProperty tank) Build a new instance using propulsive and engine property.
ImpulseManeuver(EventDetector inTrigger, Vector3D inDeltaVSat, PropulsiveProperty engine, MassProvider massModel, TankProperty tank) Build a new instance using propulsive and engine property.
ImpulseManeuver(EventDetector inTrigger, Vector3D inDeltaVSat, PropulsiveProperty engine, MassProvider massModel, TankProperty tank, LOFType inLofType) Build a new instance with a LocalOrbitalFrame and using propulsive and engine property.

Uses of MassProvider in fr.cnes.sirius.patrius.propagation

Classes in fr.cnes.sirius.patrius.propagation that implement MassProvider

Modifier and Type	Class and Description
class	SimpleMassModel Simple implementation of MassProvider.

Methods in fr.cnes.sirius.patrius.propagation with parameters of type MassProvider

Modifier and Type	Method and Description
void	AbstractPropagator.addAdditionalStateProvider(MassProvider massProvider) Add a set of state parameters from MassProvider to be computed along with the orbit propagation.
SpacecraftState	SpacecraftState.addMassProvider(MassProvider massProvider) Add the values of mass parts from MassProvider to additional states map.

Constructors in fr.cnes.sirius.patrius.propagation with parameters of type MassProvider

Constructor and Description
SpacecraftState(Orbit orbitIn, Attitude attForces, Attitude attEvents, MassProvider massProvider) Build a spacecraft state from orbit, attitude for forces and events computation and mass provider.
SpacecraftState(Orbit orbitIn, Attitude attForces, Attitude attEvents, MassProvider massProvider, Map<String,double[]> additionalStatesIn) Build a spacecraft state from orbit, attitude for forces and events computation, mass provider and additional states map.
SpacecraftState(Orbit orbitIn, Attitude attitudeIn, MassProvider massProvider) Build a spacecraft state from orbit, attitude and mass provider.
SpacecraftState(Orbit orbitIn, MassProvider massProvider) Create a new instance from orbit and mass provider.

Uses of MassProvider in fr.cnes.sirius.patrius.propagation.analytical

Constructors in fr.cnes.sirius.patrius.propagation.analytical with parameters of type MassProvider

Constructor and Description
AbstractLyddanePropagator(Orbit secularOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, MassProvider massProvider) Generic constructor.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, double referenceRadiusIn, double muIn, Frame frame, double c20In, double c30In, double c40In, double c50In, double c60In, MassProvider massProvider, ParametersType paramsType) Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double referenceRadiusIn, double muIn, Frame frame, double c20In, double c30In, double c40In, double c50In, double c60In, MassProvider massProvider, ParametersType paramsType) Build a propagator from orbit, attitude provider, mass and potential.
EcksteinHechlerPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, Frame frame, double c20In, double c30In, double c40In, double c50In, double c60In, MassProvider massProvider, ParametersType paramsType) Build a propagator from orbit, mass and potential.
J2SecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, Frame frameIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, MassProvider massProvider) Generic constructor.
J2SecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, Frame frameIn, AttitudeProvider attitudeProvider, MassProvider massProvider) Generic constructor.
J2SecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, Frame frameIn, MassProvider massProvider) Constructor without attitude provider.
KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, double mu, MassProvider massProvider) Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
KeplerianPropagator(Orbit initialOrbit, AttitudeProvider attitudeProv, double mu, MassProvider massProvider) Build propagator from orbit, attitude provider, central attraction coefficient μ and mass.
LyddaneLongPeriodPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, MassProvider massProvider) Generic constructor.
LyddaneLongPeriodPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvider, MassProvider massProvider) Generic constructor.
LyddaneLongPeriodPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, MassProvider massProvider) Constructor without attitude provider.
LyddaneSecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvForces, AttitudeProvider attitudeProvEvents, MassProvider massProvider) Generic constructor.
LyddaneSecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, AttitudeProvider attitudeProvider, MassProvider massProvider) Generic constructor.
LyddaneSecularPropagator(Orbit initialOrbit, double referenceRadiusIn, double muIn, double c20In, double c30In, double c40In, double c50In, Frame frameIn, ParametersType parametersTypeIn, MassProvider massProvider) Constructor without attitude provider.

Uses of MassProvider in fr.cnes.sirius.patrius.propagation.analytical.tle

Methods in fr.cnes.sirius.patrius.propagation.analytical.tle with parameters of type MassProvider

Modifier and Type	Method and Description
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, MassProvider mass) Selects the extrapolator to use with the selected TLE.
static TLEPropagator	TLEPropagator.selectExtrapolator(TLE tle, AttitudeProvider attitudeProvider, MassProvider mass) Selects the extrapolator to use with the selected TLE.

Constructors in fr.cnes.sirius.patrius.propagation.analytical.tle with parameters of type MassProvider

Constructor and Description
TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProviderForces, AttitudeProvider attitudeProviderEvents, MassProvider mass) Protected constructor for derived classes.
TLEPropagator(TLE initialTLE, AttitudeProvider attitudeProvider, MassProvider mass) Protected constructor for derived classes.

Uses of MassProvider in fr.cnes.sirius.patrius.propagation.analytical.twod

Methods in fr.cnes.sirius.patrius.propagation.analytical.twod that return MassProvider

Modifier and Type	Method and Description
MassProvider	Analytical2DOrbitModel.getMassModel() Returns the spacecraft mass model.

Constructors in fr.cnes.sirius.patrius.propagation.analytical.twod with parameters of type MassProvider

Constructor and Description
Analytical2DOrbitModel(Analytical2DParameterModel a, Analytical2DParameterModel ex, Analytical2DParameterModel ey, Analytical2DParameterModel i, Analytical2DParameterModel lna, Analytical2DParameterModel alpha, int[] orders, MassProvider mass, double mu) Create an analytical 2D orbit model with specified parameter models, development orders, standard gravitational parameter and spacecraft mass.
Analytical2DOrbitModel(Analytical2DParameterModel a, Analytical2DParameterModel ex, Analytical2DParameterModel ey, Analytical2DParameterModel i, Analytical2DParameterModel lna, Analytical2DParameterModel alpha, MassProvider mass, double mu) Create an analytical 2D orbit model with specified parameter models, standard gravitational parameter and spacecraft mass.

Uses of MassProvider in fr.cnes.sirius.patrius.propagation.events

Constructors in fr.cnes.sirius.patrius.propagation.events with parameters of type MassProvider

Constructor and Description
NullMassDetector(double maxCheck, double threshold, MassProvider massModel) Inherited constructor.
NullMassDetector(int slopeSelection, double maxCheck, double threshold, MassProvider massModel) Inherited constructor.
NullMassDetector(MassProvider massModel) Build a new instance (based on DateDetector).
NullMassPartDetector(double maxCheck, double threshold, MassProvider massModel, String part) Inherited constructor.
NullMassPartDetector(int slopeSelection, double maxCheck, double threshold, MassProvider massModel, String part) Inherited constructor.
NullMassPartDetector(MassProvider massModel, String part) Build a new instance MaxCheck is set to 10.e9, so almost no other date can be added.

Uses of MassProvider in fr.cnes.sirius.patrius.propagation.numerical

Methods in fr.cnes.sirius.patrius.propagation.numerical with parameters of type MassProvider

Modifier and Type	Method and Description
void	NumericalPropagator.setMassProviderEquation(MassProvider massProvider) Add additional equations associated with the mass provider.

Uses of MassProvider in fr.cnes.sirius.patrius.propagation.numerical.multi

Methods in fr.cnes.sirius.patrius.propagation.numerical.multi with parameters of type MassProvider

Modifier and Type	Method and Description
void	MultiNumericalPropagator.setMassProviderEquation(MassProvider massProvider, String satId) Add additional equations associated with the mass provider.