Class FieldSignalTravelTimeAdjustableReceiver<T extends CalculusFieldElement<T>>
- java.lang.Object
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- org.orekit.estimation.measurements.FieldSignalTravelTimeAdjustableReceiver<T>
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public class FieldSignalTravelTimeAdjustableReceiver<T extends CalculusFieldElement<T>> extends Object
Class for computing signal time of flight with an adjustable receiver and a fixed emitter's position and date.- Since:
- 14.0
- Author:
- Romain Serra, Luc Maisonnobe
- See Also:
SignalTravelTimeAdjustableReceiver
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Constructor Summary
Constructors Constructor Description FieldSignalTravelTimeAdjustableReceiver(FieldPVCoordinatesProvider<T> adjustableReceiverPVProvider)Constructor.
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Method Summary
All Methods Static Methods Instance Methods Concrete Methods Modifier and Type Method Description Tcompute(FieldVector3D<T> emitterPosition, FieldAbsoluteDate<T> emissionDate, Frame frame)Compute propagation delay on a link leg (typically downlink or uplink) without a guess.Tcompute(FieldVector3D<T> emitterPosition, FieldAbsoluteDate<T> emissionDate, FieldAbsoluteDate<T> approxReceptionDate, Frame frame)Compute propagation delay on a link leg (typically downlink or uplink).protected Tcompute(FieldPVCoordinatesProvider<T> pvCoordinatesProvider, T initialOffset, FieldVector3D<T> fixedPosition, FieldAbsoluteDate<T> guessDate, Frame frame)Compute propagation delay on a link leg (typically downlink or uplink).protected TcomputeShift(T offset, T delay)Computes the time shift.static <S extends CalculusFieldElement<S>>
FieldSignalTravelTimeAdjustableReceiver<S>of(FieldSpacecraftState<S> state)Build instance from spacecraft state.
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Field Detail
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C_RECIPROCAL
protected static final double C_RECIPROCAL
Reciprocal for light speed.- See Also:
- Constant Field Values
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Constructor Detail
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FieldSignalTravelTimeAdjustableReceiver
public FieldSignalTravelTimeAdjustableReceiver(FieldPVCoordinatesProvider<T> adjustableReceiverPVProvider)
Constructor.- Parameters:
adjustableReceiverPVProvider- adjustable receiver
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Method Detail
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of
public static <S extends CalculusFieldElement<S>> FieldSignalTravelTimeAdjustableReceiver<S> of(FieldSpacecraftState<S> state)
Build instance from spacecraft state.- Type Parameters:
S- field type- Parameters:
state- spacecraft state- Returns:
- signal travel time computer
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compute
public T compute(FieldVector3D<T> emitterPosition, FieldAbsoluteDate<T> emissionDate, Frame frame)
Compute propagation delay on a link leg (typically downlink or uplink) without a guess.- Parameters:
emitterPosition- fixed position of emitteremissionDate- emission dateframe- inertial frame in which emitter is defined- Returns:
- positive delay between signal emission and signal reception dates
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compute
public T compute(FieldVector3D<T> emitterPosition, FieldAbsoluteDate<T> emissionDate, FieldAbsoluteDate<T> approxReceptionDate, Frame frame)
Compute propagation delay on a link leg (typically downlink or uplink).- Parameters:
emitterPosition- fixed position of emitteremissionDate- emission dateapproxReceptionDate- approximate reception dateframe- inertial frame in which emitter is defined- Returns:
- positive delay between signal emission and signal reception dates
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computeShift
protected T computeShift(T offset, T delay)
Computes the time shift.- Parameters:
offset- time offsetdelay- time delay- Returns:
- time shift to use in computation
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compute
protected T compute(FieldPVCoordinatesProvider<T> pvCoordinatesProvider, T initialOffset, FieldVector3D<T> fixedPosition, FieldAbsoluteDate<T> guessDate, Frame frame)
Compute propagation delay on a link leg (typically downlink or uplink).- Parameters:
pvCoordinatesProvider- adjustable emitter/receiverinitialOffset- guess for the time off setfixedPosition- fixed receiver/emitter positionguessDate- guess for emission/reception dateframe- Inertial frame in which receiver/emitter is defined.- Returns:
- positive delay between signal emission and signal reception dates
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