public class LofOffsetPointing extends GroundPointing
The attitude pointing law is defined by an attitude provider and the satellite axis vector chosen for pointing.
Constructor and Description |
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LofOffsetPointing(Frame inertialFrame,
BodyShape shape,
AttitudeProvider attLaw,
org.hipparchus.geometry.euclidean.threed.Vector3D satPointingVector)
Creates new instance.
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Modifier and Type | Method and Description |
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<T extends org.hipparchus.CalculusFieldElement<T>> |
getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame)
Compute the attitude corresponding to an orbital state.
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Attitude |
getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
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<T extends org.hipparchus.CalculusFieldElement<T>> |
getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame)
Compute the attitude-related rotation corresponding to an orbital state.
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org.hipparchus.geometry.euclidean.threed.Rotation |
getAttitudeRotation(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude-related rotation corresponding to an orbital state.
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<T extends org.hipparchus.CalculusFieldElement<T>> |
getTargetPV(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame)
Compute the target point position/velocity in specified frame.
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TimeStampedPVCoordinates |
getTargetPV(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the target point position/velocity in specified frame.
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getBodyFrame, getTargetPosition, getTargetPosition
public LofOffsetPointing(Frame inertialFrame, BodyShape shape, AttitudeProvider attLaw, org.hipparchus.geometry.euclidean.threed.Vector3D satPointingVector)
inertialFrame
- frame in which orbital velocities are computedshape
- Body shapeattLaw
- Attitude lawsatPointingVector
- satellite vector defining the pointing directionpublic Attitude getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
getAttitude
in interface AttitudeProvider
getAttitude
in class GroundPointing
pvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computedpublic <T extends org.hipparchus.CalculusFieldElement<T>> FieldAttitude<T> getAttitude(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)
getAttitude
in interface AttitudeProvider
getAttitude
in class GroundPointing
T
- type of the field elementspvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computedpublic org.hipparchus.geometry.euclidean.threed.Rotation getAttitudeRotation(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
getAttitudeRotation
in interface AttitudeProvider
getAttitudeRotation
in class GroundPointing
pvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computedpublic <T extends org.hipparchus.CalculusFieldElement<T>> org.hipparchus.geometry.euclidean.threed.FieldRotation<T> getAttitudeRotation(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)
getAttitudeRotation
in interface AttitudeProvider
getAttitudeRotation
in class GroundPointing
T
- type of the field elementspvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computedpublic TimeStampedPVCoordinates getTargetPV(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame)
getTargetPV
in class GroundPointing
pvProv
- provider for PV coordinatesdate
- date at which target point is requestedframe
- frame in which observed ground point should be providedpublic <T extends org.hipparchus.CalculusFieldElement<T>> TimeStampedFieldPVCoordinates<T> getTargetPV(FieldPVCoordinatesProvider<T> pvProv, FieldAbsoluteDate<T> date, Frame frame)
getTargetPV
in class GroundPointing
T
- type of the field elementspvProv
- provider for PV coordinatesdate
- date at which target point is requestedframe
- frame in which observed ground point should be providedCopyright © 2002-2023 CS GROUP. All rights reserved.