Package | Description |
---|---|
org.orekit.attitudes |
This package provides classes to represent simple attitudes.
|
org.orekit.estimation.measurements |
The measurements package defines everything that is related to orbit
determination measurements.
|
org.orekit.frames |
This package provides classes to handle frames and transforms between them.
|
org.orekit.orbits |
This package provides classes to represent orbits.
|
org.orekit.propagation |
Propagation
|
org.orekit.propagation.integration |
Utilities for integration-based propagators (both numerical and semi-analytical).
|
org.orekit.propagation.numerical |
Top level package for numerical propagators.
|
org.orekit.utils |
This package provides useful objects.
|
Modifier and Type | Method | Description |
---|---|---|
<T extends RealFieldElement<T>> |
BodyCenterPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the target point position/velocity in specified frame.
|
abstract <T extends RealFieldElement<T>> |
GroundPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the target point position/velocity in specified frame.
|
<T extends RealFieldElement<T>> |
LofOffsetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the target point position/velocity in specified frame.
|
<T extends RealFieldElement<T>> |
NadirPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the target point position/velocity in specified frame.
|
<T extends RealFieldElement<T>> |
TargetPointing.getTargetPV(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the target point position/velocity in specified frame.
|
<T extends RealFieldElement<T>> |
YawCompensation.getTargetPV(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the target point position/velocity in specified frame.
|
<T extends RealFieldElement<T>> |
YawSteering.getTargetPV(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the target point position/velocity in specified frame.
|
Modifier and Type | Method | Description |
---|---|---|
static TimeStampedFieldPVCoordinates<DerivativeStructure> |
AbstractMeasurement.getCoordinates(SpacecraftState state,
int firstDerivative,
DSFactory factory) |
Get Cartesian coordinates as derivatives.
|
Modifier and Type | Method | Description |
---|---|---|
static <T extends RealFieldElement<T>> |
AbstractMeasurement.signalTimeOfFlight(TimeStampedFieldPVCoordinates<T> adjustableEmitterPV,
FieldVector3D<T> receiverPosition,
FieldAbsoluteDate<T> signalArrivalDate) |
Compute propagation delay on a link leg (typically downlink or uplink).
|
Modifier and Type | Method | Description |
---|---|---|
TimeStampedFieldPVCoordinates<T> |
FieldTransform.transformPVCoordinates(TimeStampedFieldPVCoordinates<T> pv) |
Transform
TimeStampedFieldPVCoordinates including kinematic effects. |
TimeStampedFieldPVCoordinates<T> |
FieldTransform.transformPVCoordinates(TimeStampedPVCoordinates pv) |
Transform
TimeStampedPVCoordinates including kinematic effects. |
<T extends RealFieldElement<T>> |
Transform.transformPVCoordinates(TimeStampedFieldPVCoordinates<T> pv) |
Transform
TimeStampedFieldPVCoordinates including kinematic effects. |
Modifier and Type | Method | Description |
---|---|---|
TimeStampedFieldPVCoordinates<T> |
FieldTransform.transformPVCoordinates(TimeStampedFieldPVCoordinates<T> pv) |
Transform
TimeStampedFieldPVCoordinates including kinematic effects. |
<T extends RealFieldElement<T>> |
Transform.transformPVCoordinates(TimeStampedFieldPVCoordinates<T> pv) |
Transform
TimeStampedFieldPVCoordinates including kinematic effects. |
Modifier and Type | Method | Description |
---|---|---|
TimeStampedFieldPVCoordinates<T> |
FieldOrbit.getPVCoordinates() |
Get the
TimeStampedPVCoordinates in definition frame. |
TimeStampedFieldPVCoordinates<T> |
FieldOrbit.getPVCoordinates(Frame outputFrame) |
Get the
TimeStampedPVCoordinates in a specified frame. |
TimeStampedFieldPVCoordinates<T> |
FieldOrbit.getPVCoordinates(FieldAbsoluteDate<T> otherDate,
Frame otherFrame) |
Get the
FieldPVCoordinates of the body in the selected frame. |
protected TimeStampedFieldPVCoordinates<T> |
FieldCartesianOrbit.initPVCoordinates() |
Compute the position/velocity coordinates from the canonical parameters.
|
protected TimeStampedFieldPVCoordinates<T> |
FieldCircularOrbit.initPVCoordinates() |
Compute the position/velocity coordinates from the canonical parameters.
|
protected TimeStampedFieldPVCoordinates<T> |
FieldEquinoctialOrbit.initPVCoordinates() |
Compute the position/velocity coordinates from the canonical parameters.
|
protected TimeStampedFieldPVCoordinates<T> |
FieldKeplerianOrbit.initPVCoordinates() |
Compute the position/velocity coordinates from the canonical parameters.
|
protected abstract TimeStampedFieldPVCoordinates<T> |
FieldOrbit.initPVCoordinates() |
Compute the position/velocity coordinates from the canonical parameters.
|
Constructor | Description |
---|---|
FieldCartesianOrbit(TimeStampedFieldPVCoordinates<T> pvaCoordinates,
Frame frame,
double mu) |
Constructor from Cartesian parameters.
|
FieldCircularOrbit(TimeStampedFieldPVCoordinates<T> pvCoordinates,
Frame frame,
double mu) |
Constructor from Cartesian parameters.
|
FieldEquinoctialOrbit(TimeStampedFieldPVCoordinates<T> pvCoordinates,
Frame frame,
double mu) |
Constructor from Cartesian parameters.
|
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates<T> pvCoordinates,
Frame frame,
double mu) |
Constructor from Cartesian parameters.
|
FieldOrbit(TimeStampedFieldPVCoordinates<T> FieldPVCoordinates,
Frame frame,
double mu) |
Set the orbit from Cartesian parameters.
|
Modifier and Type | Method | Description |
---|---|---|
TimeStampedFieldPVCoordinates<T> |
FieldAbstractPropagator.getPVCoordinates(FieldAbsoluteDate<T> date,
Frame frame) |
Get the
FieldPVCoordinates of the body in the selected frame. |
TimeStampedFieldPVCoordinates<T> |
FieldSpacecraftState.getPVCoordinates() |
Get the
TimeStampedFieldPVCoordinates in orbit definition frame. |
TimeStampedFieldPVCoordinates<T> |
FieldSpacecraftState.getPVCoordinates(Frame outputFrame) |
Get the
TimeStampedFieldPVCoordinates in given output frame. |
Modifier and Type | Method | Description |
---|---|---|
TimeStampedFieldPVCoordinates<T> |
FieldIntegratedEphemeris.getPVCoordinates(FieldAbsoluteDate<T> date,
Frame frame) |
Get the
FieldPVCoordinates of the body in the selected frame. |
Modifier and Type | Method | Description |
---|---|---|
TimeStampedFieldPVCoordinates<T> |
FieldNumericalPropagator.getPVCoordinates(FieldAbsoluteDate<T> date,
Frame frame) |
Get the
FieldPVCoordinates of the body in the selected frame. |
Modifier and Type | Method | Description |
---|---|---|
<T extends RealFieldElement<T>> |
AngularCoordinates.applyTo(TimeStampedFieldPVCoordinates<T> pv) |
Apply the rotation to a pv coordinates.
|
TimeStampedFieldPVCoordinates<T> |
FieldAngularCoordinates.applyTo(TimeStampedFieldPVCoordinates<T> pv) |
Apply the rotation to a pv coordinates.
|
TimeStampedFieldPVCoordinates<T> |
FieldAngularCoordinates.applyTo(TimeStampedPVCoordinates pv) |
Apply the rotation to a pv coordinates.
|
<T extends RealFieldElement<T>> |
ExtendedPVCoordinatesProvider.getPVCoordinates(FieldAbsoluteDate<T> date,
Frame frame) |
Get the
FieldPVCoordinates of the body in the selected frame. |
TimeStampedFieldPVCoordinates<T> |
FieldPVCoordinatesProvider.getPVCoordinates(FieldAbsoluteDate<T> date,
Frame frame) |
Get the
FieldPVCoordinates of the body in the selected frame. |
static <T extends RealFieldElement<T>> |
TimeStampedFieldPVCoordinates.interpolate(FieldAbsoluteDate<T> date,
CartesianDerivativesFilter filter,
Collection<TimeStampedFieldPVCoordinates<T>> sample) |
Interpolate position-velocity.
|
static <T extends RealFieldElement<T>> |
TimeStampedFieldPVCoordinates.interpolate(FieldAbsoluteDate<T> date,
CartesianDerivativesFilter filter,
Stream<TimeStampedFieldPVCoordinates<T>> sample) |
Interpolate position-velocity.
|
TimeStampedFieldPVCoordinates<T> |
TimeStampedFieldPVCoordinates.shiftedBy(double dt) |
Get a time-shifted state.
|
TimeStampedFieldPVCoordinates<T> |
TimeStampedFieldPVCoordinates.shiftedBy(T dt) |
Get a time-shifted state.
|
Modifier and Type | Method | Description |
---|---|---|
<T extends RealFieldElement<T>> |
AngularCoordinates.applyTo(TimeStampedFieldPVCoordinates<T> pv) |
Apply the rotation to a pv coordinates.
|
TimeStampedFieldPVCoordinates<T> |
FieldAngularCoordinates.applyTo(TimeStampedFieldPVCoordinates<T> pv) |
Apply the rotation to a pv coordinates.
|
Modifier and Type | Method | Description |
---|---|---|
static <T extends RealFieldElement<T>> |
TimeStampedFieldPVCoordinates.interpolate(FieldAbsoluteDate<T> date,
CartesianDerivativesFilter filter,
Collection<TimeStampedFieldPVCoordinates<T>> sample) |
Interpolate position-velocity.
|
static <T extends RealFieldElement<T>> |
TimeStampedFieldPVCoordinates.interpolate(FieldAbsoluteDate<T> date,
CartesianDerivativesFilter filter,
Stream<TimeStampedFieldPVCoordinates<T>> sample) |
Interpolate position-velocity.
|
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