Package | Description |
---|---|
org.orekit.attitudes |
This package provides classes to represent simple attitudes.
|
org.orekit.gnss.attitude |
This package provides classes related to navigation satellites attitude modeling.
|
org.orekit.propagation |
Propagation
|
Modifier and Type | Method | Description |
---|---|---|
Attitude |
AttitudeProvider.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
AttitudesSequence.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
CelestialBodyPointed.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
FixedRate.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
GroundPointing.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
InertialProvider.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
LofOffset.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
LofOffsetPointing.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
SpinStabilized.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
TabulatedLofOffset.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
TabulatedProvider.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
YawCompensation.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
YawSteering.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Attitude |
YawCompensation.getBaseState(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the base system state at given date, without compensation.
|
Attitude |
YawSteering.getBaseState(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the base system state at given date, without compensation.
|
Attitude |
FixedRate.getReferenceAttitude() |
Get the reference attitude.
|
Attitude |
Attitude.interpolate(AbsoluteDate interpolationDate,
Stream<Attitude> sample) |
Get an interpolated instance.
|
Attitude |
Attitude.shiftedBy(double dt) |
Get a time-shifted attitude.
|
Attitude |
FieldAttitude.toAttitude() |
Converts to an Attitude instance.
|
Attitude |
Attitude.withReferenceFrame(Frame newReferenceFrame) |
Get a similar attitude with a specific reference frame.
|
Modifier and Type | Method | Description |
---|---|---|
Attitude |
Attitude.interpolate(AbsoluteDate interpolationDate,
Stream<Attitude> sample) |
Get an interpolated instance.
|
Constructor | Description |
---|---|
FieldAttitude(org.hipparchus.Field<T> field,
Attitude attitude) |
Builds an instance for a regular
Attitude . |
FixedRate(Attitude referenceAttitude) |
Creates a new instance.
|
Modifier and Type | Method | Description |
---|---|---|
Attitude |
AbstractGNSSAttitudeProvider.getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
|
Modifier and Type | Method | Description |
---|---|---|
Attitude |
SpacecraftState.getAttitude() |
Get the attitude.
|
Constructor | Description |
---|---|
SpacecraftState(Orbit orbit,
Attitude attitude) |
Build a spacecraft state from orbit and attitude provider.
|
SpacecraftState(Orbit orbit,
Attitude attitude,
double mass) |
Build a spacecraft state from orbit, attitude provider and mass.
|
SpacecraftState(Orbit orbit,
Attitude attitude,
double mass,
Map<String,double[]> additional) |
Build a spacecraft state from orbit, attitude provider and mass.
|
SpacecraftState(Orbit orbit,
Attitude attitude,
Map<String,double[]> additional) |
Build a spacecraft state from orbit and attitude provider.
|
Copyright © 2002-2019 CS Systèmes d'information. All rights reserved.