org.orekit.attitudes

Class FrameAlignedProvider

java.lang.Object

org.orekit.attitudes.FrameAlignedProvider

All Implemented Interfaces:

AttitudeProvider

public class FrameAlignedProvider
extends Object
implements AttitudeProvider

This class handles an attitude provider aligned with a frame or a fixed offset to it.

Instances of this class are guaranteed to be immutable.

Author:

Luc Maisonobe

Constructor Summary

Constructors

Constructor and Description
FrameAlignedProvider(Frame frame) Creates new instance aligned with the given frame.
FrameAlignedProvider(org.hipparchus.geometry.euclidean.threed.Rotation rotation) Creates new instance.
FrameAlignedProvider(org.hipparchus.geometry.euclidean.threed.Rotation rotation, Frame reference) Creates new instance with a fixed attitude in the given frame.

Method Summary

Modifier and Type	Method and Description
<T extends org.hipparchus.CalculusFieldElement<T>> FieldAttitude<T>	getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude corresponding to an orbital state.
Attitude	getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude corresponding to an orbital state.
<T extends org.hipparchus.CalculusFieldElement<T>> org.hipparchus.geometry.euclidean.threed.FieldRotation<T>	getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.
org.hipparchus.geometry.euclidean.threed.Rotation	getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) Compute the attitude-related rotation corresponding to an orbital state.
static AttitudeProvider	of(Frame satelliteFrame) Creates an attitude provider aligned with the given frame.

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Constructor Detail

FrameAlignedProvider

@DefaultDataContext
public FrameAlignedProvider(org.hipparchus.geometry.euclidean.threed.Rotation rotation)

Creates new instance.

This constructor uses the default data context.

Parameters:

rotation - rotation from EME2000 to the desired satellite frame

See Also:

FrameAlignedProvider(Rotation, Frame)

FrameAlignedProvider

public FrameAlignedProvider(Frame frame)

Creates new instance aligned with the given frame.

Parameters:

frame - the reference frame for the attitude.

FrameAlignedProvider

public FrameAlignedProvider(org.hipparchus.geometry.euclidean.threed.Rotation rotation,
                            Frame reference)

Creates new instance with a fixed attitude in the given frame.

Parameters:

rotation - rotation from reference to the desired satellite frame

reference - frame for rotation.

Since:

10.1

Method Detail

of

public static AttitudeProvider of(Frame satelliteFrame)

Creates an attitude provider aligned with the given frame.

This attitude provider returned by this method is designed to be as fast as possible for when attitude is irrelevant while still being a valid implementation of AttitudeProvider. To ensure good performance the specified attitude reference frame should be the same frame used for propagation so that computing the frame transformation is trivial.

Parameters:

satelliteFrame - with which the satellite is aligned.

Returns:

new attitude provider aligned with the given frame.

Since:

11.0

getAttitude

public Attitude getAttitude(PVCoordinatesProvider pvProv,
                            AbsoluteDate date,
                            Frame frame)

Compute the attitude corresponding to an orbital state.

Specified by:

getAttitude in interface AttitudeProvider

Parameters:

pvProv - local position-velocity provider around current date

date - current date

frame - reference frame from which attitude is computed

Returns:

attitude on the specified date and position-velocity state

getAttitude

public <T extends org.hipparchus.CalculusFieldElement<T>> FieldAttitude<T> getAttitude(FieldPVCoordinatesProvider<T> pvProv,
                                                                                       FieldAbsoluteDate<T> date,
                                                                                       Frame frame)

Compute the attitude corresponding to an orbital state.

Specified by:

getAttitude in interface AttitudeProvider

Type Parameters:

T - type of the field elements

Parameters:

pvProv - local position-velocity provider around current date

date - current date

frame - reference frame from which attitude is computed

Returns:

attitude on the specified date and position-velocity state

getAttitudeRotation

public org.hipparchus.geometry.euclidean.threed.Rotation getAttitudeRotation(PVCoordinatesProvider pvProv,
                                                                             AbsoluteDate date,
                                                                             Frame frame)

Compute the attitude-related rotation corresponding to an orbital state.

Specified by:

getAttitudeRotation in interface AttitudeProvider

Parameters:

pvProv - local position-velocity provider around current date

date - current date

frame - reference frame from which attitude is computed

Returns:

attitude-related rotation on the specified date and position-velocity state

getAttitudeRotation

public <T extends org.hipparchus.CalculusFieldElement<T>> org.hipparchus.geometry.euclidean.threed.FieldRotation<T> getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv,
                                                                                                                                        FieldAbsoluteDate<T> date,
                                                                                                                                        Frame frame)

Compute the attitude-related rotation corresponding to an orbital state.

Specified by:

getAttitudeRotation in interface AttitudeProvider

Type Parameters:

T - type of the field elements

Parameters:

pvProv - local position-velocity provider around current date

date - current date

frame - reference frame from which attitude is computed

Returns:

rotation on the specified date and position-velocity state