Package org.orekit.attitudes
Class LofOffsetPointing
- java.lang.Object
-
- org.orekit.attitudes.GroundPointing
-
- org.orekit.attitudes.LofOffsetPointing
-
- All Implemented Interfaces:
AttitudeProvider
,EventDetectorsProvider
,ParameterDriversProvider
public class LofOffsetPointing extends GroundPointing
This class provides a default attitude provider.The attitude pointing law is defined by an attitude provider and the satellite axis vector chosen for pointing.
- Author:
- Véronique Pommier-Maurussane
-
-
Field Summary
-
Fields inherited from interface org.orekit.propagation.events.EventDetectorsProvider
DATATION_ACCURACY
-
-
Constructor Summary
Constructors Constructor Description LofOffsetPointing(Frame inertialFrame, BodyShape shape, AttitudeProvider attLaw, Vector3D satPointingVector)
Creates new instance.
-
Method Summary
All Methods Instance Methods Concrete Methods Modifier and Type Method Description <T extends 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 CalculusFieldElement<T>>
FieldRotation<T>getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)
Compute the attitude-related rotation corresponding to an orbital state.Rotation
getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Compute the attitude-related rotation corresponding to an orbital state.protected <T extends CalculusFieldElement<T>>
FieldVector3D<T>getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)
Compute the target point position in specified frame.protected Vector3D
getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Compute the target point position in specified frame.<T extends CalculusFieldElement<T>>
TimeStampedFieldPVCoordinates<T>getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)
Compute the target point position/velocity in specified frame.TimeStampedPVCoordinates
getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Compute the target point position/velocity in specified frame.-
Methods inherited from class org.orekit.attitudes.GroundPointing
getBodyFrame
-
Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
-
Methods inherited from interface org.orekit.attitudes.AttitudeProvider
getEventDetectors, getFieldEventDetectors, getParametersDrivers
-
Methods inherited from interface org.orekit.propagation.events.EventDetectorsProvider
getEventDetectors, getFieldEventDetectors
-
Methods inherited from interface org.orekit.utils.ParameterDriversProvider
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported
-
-
-
-
Constructor Detail
-
LofOffsetPointing
public LofOffsetPointing(Frame inertialFrame, BodyShape shape, AttitudeProvider attLaw, Vector3D satPointingVector)
Creates new instance.- Parameters:
inertialFrame
- frame in which orbital velocities are computedshape
- Body shapeattLaw
- Attitude lawsatPointingVector
- satellite vector defining the pointing direction- Since:
- 7.1
-
-
Method Detail
-
getAttitude
public Attitude getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Compute the attitude corresponding to an orbital state.- Specified by:
getAttitude
in interfaceAttitudeProvider
- Overrides:
getAttitude
in classGroundPointing
- Parameters:
pvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computed- Returns:
- attitude on the specified date and position-velocity state
-
getAttitude
public <T extends 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 interfaceAttitudeProvider
- Overrides:
getAttitude
in classGroundPointing
- Type Parameters:
T
- type of the field elements- Parameters:
pvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computed- Returns:
- attitude on the specified date and position-velocity state
-
getAttitudeRotation
public Rotation getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Compute the attitude-related rotation corresponding to an orbital state.- Specified by:
getAttitudeRotation
in interfaceAttitudeProvider
- Overrides:
getAttitudeRotation
in classGroundPointing
- Parameters:
pvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computed- Returns:
- attitude-related rotation on the specified date and position-velocity state
-
getAttitudeRotation
public <T extends CalculusFieldElement<T>> 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 interfaceAttitudeProvider
- Overrides:
getAttitudeRotation
in classGroundPointing
- Type Parameters:
T
- type of the field elements- Parameters:
pvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computed- Returns:
- rotation on the specified date and position-velocity state
-
getTargetPV
public TimeStampedPVCoordinates getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Compute the target point position/velocity in specified frame.- Specified by:
getTargetPV
in classGroundPointing
- Parameters:
pvProv
- provider for PV coordinatesdate
- date at which target point is requestedframe
- frame in which observed ground point should be provided- Returns:
- observed ground point position (element 0) and velocity (at index 1) in specified frame
-
getTargetPosition
protected Vector3D getTargetPosition(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
Compute the target point position in specified frame.- Overrides:
getTargetPosition
in classGroundPointing
- Parameters:
pvProv
- provider for PV coordinatesdate
- date at which target point is requestedframe
- frame in which observed ground point should be provided- Returns:
- observed ground point position in specified frame
-
getTargetPV
public <T extends CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T> getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)
Compute the target point position/velocity in specified frame.- Specified by:
getTargetPV
in classGroundPointing
- Type Parameters:
T
- type of the field elements- Parameters:
pvProv
- provider for PV coordinatesdate
- date at which target point is requestedframe
- frame in which observed ground point should be provided- Returns:
- observed ground point position (element 0) and velocity (at index 1) in specified frame
-
getTargetPosition
protected <T extends CalculusFieldElement<T>> FieldVector3D<T> getTargetPosition(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)
Compute the target point position in specified frame.- Overrides:
getTargetPosition
in classGroundPointing
- Type Parameters:
T
- type of the field elements- Parameters:
pvProv
- provider for PV coordinatesdate
- date at which target point is requestedframe
- frame in which observed ground point should be provided- Returns:
- observed ground point position in specified frame
-
-