<T extends CalculusFieldElement<T>> FieldAttitude<T> |
AttitudeBuilder.build(Frame frame,
FieldPVCoordinatesProvider<T> pvProv,
TimeStampedFieldAngularCoordinates<T> rawAttitude) |
Build a filtered attitude.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
FixedFrameBuilder.build(Frame frame,
FieldPVCoordinatesProvider<T> pvProv,
TimeStampedFieldAngularCoordinates<T> rawAttitude) |
Build a filtered attitude.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
AggregateBoundedAttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
AlignedAndConstrained.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
AttitudeProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
AttitudesSequence.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
CelestialBodyPointed.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
FixedRate.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
FrameAlignedProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
GroundPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
LofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
LofOffsetPointing.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
SpinStabilized.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
TabulatedLofOffset.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
TabulatedProvider.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
TorqueFree.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
YawCompensation.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
YawSteering.getAttitude(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the attitude corresponding to an orbital state.
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<T extends CalculusFieldElement<T>> FieldAttitude<T> |
GroundPointingAttitudeModifier.getBaseState(FieldPVCoordinatesProvider<T> pvProv,
FieldAbsoluteDate<T> date,
Frame frame) |
Compute the base system state at given date, without modifications.
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protected FieldAttitude<KK> |
FieldAttitudeInterpolator.interpolate(AbstractFieldTimeInterpolator.InterpolationData interpolationData) |
Interpolate instance from given interpolation data.
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FieldAttitude<T> |
FieldAttitude.shiftedBy(double dt) |
Get a time-shifted attitude.
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FieldAttitude<T> |
FieldAttitude.shiftedBy(T dt) |
Get a time-shifted attitude.
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FieldAttitude<T> |
FieldAttitude.withReferenceFrame(Frame newReferenceFrame) |
Get a similar attitude with a specific reference frame.
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