Package org.orekit.attitudes

Interface AttitudeRotationModel

All Superinterfaces:

ParameterDriversProvider

All Known Subinterfaces:

AttitudeProvider, AttitudeProviderModifier, BoundedAttitudeProvider, GNSSAttitudeProvider

All Known Implementing Classes:

AggregateBoundedAttitudeProvider, AlignedAndConstrained, AttitudesSequence, AttitudesSwitcher, BeidouGeo, BeidouIGSO, BeidouMeo, BodyCenterPointing, CelestialBodyPointed, FixedRate, FrameAlignedProvider, Galileo, GenericGNSS, Glonass, GPSBlockIIA, GPSBlockIIF, GPSBlockIIR, GroundPointing, GroundPointingAttitudeModifier, LofOffset, LofOffsetPointing, NadirPointing, SpinStabilized, TabulatedLofOffset, TabulatedProvider, TargetPointing, TorqueFree, YawCompensation, YawSteering

public interface AttitudeRotationModel
extends ParameterDriversProvider

Interface for (attitude) rotation models taking as inputs a spacecraft state and model parameters. The rotation is defined between a reference frame and the satellite one.

Since:

13.0

Author:

Romain Serra

See Also:

• SpacecraftState
• FieldSpacecraftState
• Rotation
• FieldRotation
• Attitude
• FieldAttitude
• Maneuver

Method Summary

Modifier and Type	Method	Description
<T extends CalculusFieldElement<T>> FieldRotation<T>	getAttitudeRotation(FieldSpacecraftState<T> state, T[] parameters)	Computed the rotation given the input state and parameters' values.
Rotation	getAttitudeRotation(SpacecraftState state, double[] parameters)	Computed the rotation given the input state and parameters' values.

Methods inherited from interface org.orekit.utils.ParameterDriversProvider

getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, getParametersDrivers, isSupported

Method Details

getAttitudeRotation

Rotation getAttitudeRotation(SpacecraftState state,
 double[] parameters)

Computed the rotation given the input state and parameters' values.

Parameters:

state - spacecraft state

parameters - values for parameter drivers

Returns:

attitude's rotation

getAttitudeRotation

<T extends CalculusFieldElement<T>>
FieldRotation<T> getAttitudeRotation(FieldSpacecraftState<T> state,
 T[] parameters)

Computed the rotation given the input state and parameters' values.

Type Parameters:

T - field type

Parameters:

state - spacecraft state

parameters - values for parameter drivers

Returns:

attitude's rotation