AttitudeRotationModel (OREKIT 13.0-SNAPSHOT API)

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, ThrustDirectionAndAttitudeProvider, 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

All Methods Instance Methods Abstract Methods
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 Detail
  - 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