public class RelativeTabulatedAttitudeLeg extends Object implements AttitudeLeg
TabulatedAttitude
class.Constructor and Description |
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RelativeTabulatedAttitudeLeg(AbsoluteDate referenceDate,
Frame frame,
List<Pair<Double,AngularCoordinates>> angularCoordinates)
Build a RelativeTabulatedAttitudeLeg with a reference date, a list of angular coordinates
associated with a double representing the time elapsed since the reference date.
|
RelativeTabulatedAttitudeLeg(AbsoluteDate referenceDate,
List<Pair<Double,AngularCoordinates>> angularCoordinates,
int nbInterpolationPoints,
Frame frame)
Build a RelativeTabulatedAttitudeLeg with a reference date, a list of angular coordinates
associated with a double representing the time elapsed since the reference date
and a number of points used for interpolation.
|
RelativeTabulatedAttitudeLeg(AbsoluteDate referenceDate,
List<Pair<Double,Rotation>> orientations,
Frame frame)
Build a RelativeTabulatedAttitudeLeg with a reference date, a list of Rotations
associated with a double representing the time elapsed since the reference date.
|
RelativeTabulatedAttitudeLeg(AbsoluteDate referenceDate,
List<Pair<Double,Rotation>> orientations,
Frame frame,
int nbInterpolationPoints)
Build a RelativeTabulatedAttitudeLeg with a reference date, a list of Rotations
associated with a double representing the time elapsed since the reference date
and a number of points used for interpolation.
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Modifier and Type | Method and Description |
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Attitude |
getAttitude(Orbit orbit)
Compute the attitude corresponding to an orbital state.
|
Attitude |
getAttitude(PVCoordinatesProvider pvProv,
AbsoluteDate date,
Frame frame)
Compute the attitude corresponding to an orbital state.
|
AbsoluteDateInterval |
getTimeInterval()
Return the time interval of validity
|
void |
setSpinDerivativesComputation(boolean computeSpinDerivatives)
Method to activate spin derivative computation.
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public RelativeTabulatedAttitudeLeg(AbsoluteDate referenceDate, List<Pair<Double,Rotation>> orientations, Frame frame) throws PatriusException
TabulatedAttitude
)
Rotations rates (set to 0's) will not be used for interpolation.referenceDate
- reference dateorientations
- rotations. WARNING : these must be chronologically ordered.frame
- reference frame from which attitude is computedPatriusException
- thrown if there is not enough data for Hermite interpolationpublic RelativeTabulatedAttitudeLeg(AbsoluteDate referenceDate, List<Pair<Double,Rotation>> orientations, Frame frame, int nbInterpolationPoints) throws PatriusException
referenceDate
- reference dateorientations
- rotations. WARNING : these must be chronologically ordered.frame
- reference frame from which attitude is computednbInterpolationPoints
- nbInterpolationPoints number of points used for interpolationPatriusException
- thrown if there is not enough data for Hermite interpolationpublic RelativeTabulatedAttitudeLeg(AbsoluteDate referenceDate, Frame frame, List<Pair<Double,AngularCoordinates>> angularCoordinates) throws PatriusException
TabulatedAttitude
)referenceDate
- reference dateangularCoordinates
- angular coordinates. WARNING : these must be chronologically ordered.frame
- reference frame from which attitude is computedPatriusException
- thrown if there is not enough data for Hermite interpolationpublic RelativeTabulatedAttitudeLeg(AbsoluteDate referenceDate, List<Pair<Double,AngularCoordinates>> angularCoordinates, int nbInterpolationPoints, Frame frame) throws PatriusException
referenceDate
- reference dateangularCoordinates
- angular coordinates WARNING : these must be chronologically ordered.frame
- reference frame from which attitude is computednbInterpolationPoints
- nbInterpolationPoints number of points used for interpolationPatriusException
- thrown if there is not enough data for Hermite interpolationpublic AbsoluteDateInterval getTimeInterval() throws PatriusException
AttitudeLeg
getTimeInterval
in interface AttitudeLeg
PatriusException
- if the time interval is not computed (for a slew)public Attitude getAttitude(PVCoordinatesProvider pvProv, AbsoluteDate date, Frame frame) throws PatriusException
getAttitude
in interface AttitudeProvider
pvProv
- local position-velocity provider around current datedate
- current dateframe
- reference frame from which attitude is computedPatriusException
- if attitude cannot be computedpublic Attitude getAttitude(Orbit orbit) throws PatriusException
getAttitude
in interface AttitudeProvider
orbit
- current orbitPatriusException
- if attitude cannot be computedpublic void setSpinDerivativesComputation(boolean computeSpinDerivatives) throws PatriusException
setSpinDerivativesComputation
in interface AttitudeProvider
computeSpinDerivatives
- true if spin derivatives should be computedPatriusException
- if spin derivatives can not be computedCopyright © 2018 CNES. All Rights Reserved.