Uses of Class
org.orekit.attitudes.Attitude

Packages that use Attitude

Package	Description
org.orekit.attitudes	This package provides classes to represent simple attitudes.
org.orekit.forces.maneuvers.propulsion	This package provides propulsion models intended to be used with class Maneuver.
org.orekit.propagation	Propagation

Uses of Attitude in org.orekit.attitudes

Methods in org.orekit.attitudes that return Attitude

Modifier and Type	Method and Description
Attitude	YawCompensation.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	AttitudeProvider.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	FixedRate.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	GroundPointing.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	LofOffsetPointing.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	YawSteering.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	CelestialBodyPointed.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.

Method parameters in org.orekit.attitudes with type arguments of type Attitude

Modifier and Type	Method and Description
Attitude	Attitude.interpolate(AbsoluteDate interpolationDate, Stream<Attitude> sample) Get an interpolated instance.

Constructors in org.orekit.attitudes with parameters of type Attitude

Constructor and Description
FieldAttitude(Field<T> field, Attitude attitude) Builds an instance for a regular Attitude.
FixedRate(Attitude referenceAttitude) Creates a new instance.

Uses of Attitude in org.orekit.forces.maneuvers.propulsion

Methods in org.orekit.forces.maneuvers.propulsion that return Attitude

Modifier and Type	Method and Description
Attitude	ThrustDirectionAndAttitudeProvider.getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
protected Attitude	ThrustDirectionAndAttitudeProvider.getAttitudeFromFrame(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude for DIRECTION_IN_FRAME or DIRECTION_IN_LOF types.

Methods in org.orekit.forces.maneuvers.propulsion with parameters of type Attitude

Modifier and Type	Method and Description
default Vector3D	ThrustPropulsionModel.getAcceleration(SpacecraftState s, Attitude maneuverAttitude, double[] parameters) Get the acceleration of the spacecraft during maneuver and in maneuver frame.
Vector3D	PropulsionModel.getAcceleration(SpacecraftState s, Attitude maneuverAttitude, double[] parameters) Get the acceleration of the spacecraft during maneuver and in maneuver frame.

Uses of Attitude in org.orekit.propagation

Methods in org.orekit.propagation that return Attitude

Modifier and Type	Method and Description
Attitude	SpacecraftState.getAttitude() Get the attitude.

Constructors in org.orekit.propagation with parameters of type Attitude

Constructor and Description
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude) Build a spacecraft state from orbit and attitude provider.
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude, double mass) Build a spacecraft state from orbit, attitude provider and mass.
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude, double mass, Map<String,double[]> additional) Build a spacecraft state from orbit, attitude provider and mass.
SpacecraftState(AbsolutePVCoordinates absPva, Attitude attitude, Map<String,double[]> additional) Build a spacecraft state from orbit and attitude provider.
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.