public class MultiplexedMeasurement extends AbstractMeasurement<MultiplexedMeasurement>
Date comes from the first measurement, observed and estimated values result from gathering all underlying measurements values.
| Constructor and Description |
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MultiplexedMeasurement(List<ObservedMeasurement<?>> measurements)
Simple constructor.
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| Modifier and Type | Method and Description |
|---|---|
List<EstimatedMeasurement<?>> |
getEstimatedMeasurements()
Get the underlying estimated measurements.
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List<ObservedMeasurement<?>> |
getMeasurements()
Get the underlying measurements.
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protected EstimatedMeasurement<MultiplexedMeasurement> |
theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
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addModifier, addParameterDriver, estimate, getBaseWeight, getCoordinates, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getSatellites, getTheoreticalStandardDeviation, isEnabled, setEnabled, signalTimeOfFlight, signalTimeOfFlightclone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, waitcompareTopublic MultiplexedMeasurement(List<ObservedMeasurement<?>> measurements)
measurements - measurements to multiplexpublic List<ObservedMeasurement<?>> getMeasurements()
public List<EstimatedMeasurement<?>> getEstimatedMeasurements()
protected EstimatedMeasurement<MultiplexedMeasurement> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
The theoretical value does not have any modifiers applied.
theoreticalEvaluation in class AbstractMeasurement<MultiplexedMeasurement>iteration - iteration numberevaluation - evaluation numberstates - orbital states at measurement dateAbstractMeasurement.estimate(int, int, SpacecraftState[])Copyright © 2002-2020 CS GROUP. All rights reserved.