Package org.orekit.estimation.measurements

Class SignalTravelTimeAdjustableReceiver

java.lang.Object

org.orekit.estimation.measurements.SignalTravelTimeAdjustableReceiver

public class SignalTravelTimeAdjustableReceiver
extends Object

Class for computing signal time of flight with an adjustable receiver and fixed emitter's position.

Since:

14.0

Author:

Romain Serra

Field Summary

Fields

Modifier and Type	Field	Description
protected static double	C_RECIPROCAL	Reciprocal for light speed.

Constructor Summary

Constructors

Constructor	Description
SignalTravelTimeAdjustableReceiver(PVCoordinatesProvider adjustableReceiverPVProvider)

Method Summary

Modifier and Type	Method	Description
double	compute(Vector3D emitterPosition, AbsoluteDate emissionDate, Frame frame)	Compute propagation delay on a link leg (typically downlink or uplink) without a guess.
double	compute(Vector3D emitterPosition, AbsoluteDate emissionDate, AbsoluteDate approxReceptionDate, Frame frame)	Compute propagation delay on a link leg (typically downlink or uplink).
protected double	compute(PVCoordinatesProvider pvCoordinatesProvider, double initialOffset, Vector3D fixedPosition, AbsoluteDate guessDate, Frame frame)	Compute propagation delay on a link leg (typically downlink or uplink).
protected double	computeShift(double offset, double delay)	Computes the time shift.
static SignalTravelTimeAdjustableReceiver	of(SpacecraftState state)	Build instance from spacecraft state.

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Field Detail

C_RECIPROCAL

protected static final double C_RECIPROCAL

Reciprocal for light speed.

See Also:

Constant Field Values

Constructor Detail

SignalTravelTimeAdjustableReceiver

public SignalTravelTimeAdjustableReceiver(PVCoordinatesProvider adjustableReceiverPVProvider)

Method Detail

of

public static SignalTravelTimeAdjustableReceiver of(SpacecraftState state)

Build instance from spacecraft state.

Parameters:

state - spacecraft state

Returns:

signal time computer

compute

public double compute(Vector3D emitterPosition,
                      AbsoluteDate emissionDate,
                      Frame frame)

Compute propagation delay on a link leg (typically downlink or uplink) without a guess.

Parameters:

emitterPosition - fixed position of emitter

emissionDate - emission date

frame - inertial frame in which emitter is defined

Returns:

positive delay between signal emission and signal reception dates

compute

public double compute(Vector3D emitterPosition,
                      AbsoluteDate emissionDate,
                      AbsoluteDate approxReceptionDate,
                      Frame frame)

Compute propagation delay on a link leg (typically downlink or uplink).

Parameters:

emitterPosition - fixed position of emitter

emissionDate - emission date

approxReceptionDate - approximate reception date

frame - inertial frame in which emitter is defined

Returns:

positive delay between signal emission and signal reception dates

computeShift

protected double computeShift(double offset,
                              double delay)

Computes the time shift.

Parameters:

offset - time offset

delay - time delay

Returns:

time shift to use in computation

compute

protected double compute(PVCoordinatesProvider pvCoordinatesProvider,
                         double initialOffset,
                         Vector3D fixedPosition,
                         AbsoluteDate guessDate,
                         Frame frame)

Compute propagation delay on a link leg (typically downlink or uplink).

Parameters:

pvCoordinatesProvider - adjustable emitter/receiver

initialOffset - guess for the time off set

fixedPosition - fixed receiver/emitter position

guessDate - guess for emission/reception date

frame - Inertial frame in which receiver/emitter is defined.

Returns:

positive delay between signal emission and signal reception dates