public class AngularAzEl extends GroundReceiverMeasurement<AngularAzEl>
Modifier and Type | Field and Description |
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static String |
MEASUREMENT_TYPE
Type of the measurement.
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Constructor and Description |
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AngularAzEl(GroundStation station,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight,
ObservableSatellite satellite)
Simple constructor.
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Modifier and Type | Method and Description |
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org.hipparchus.geometry.euclidean.threed.Vector3D |
getObservedLineOfSight(Frame outputFrame)
Calculate the Line Of Sight of the given measurement.
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protected EstimatedMeasurement<AngularAzEl> |
theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
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protected EstimatedMeasurementBase<AngularAzEl> |
theoreticalEvaluationWithoutDerivatives(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value without derivatives.
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computeCommonParametersWithDerivatives, computeCommonParametersWithout, getGroundStationCoordinates, getGroundStationPosition, getStation, isTwoWay
addModifier, addParameterDriver, estimate, estimateWithoutDerivatives, getBaseWeight, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getSatellites, getTheoreticalStandardDeviation, isEnabled, setEnabled, signalTimeOfFlight, signalTimeOfFlight
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
getMeasurementType
compareTo
durationFrom
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported
public static final String MEASUREMENT_TYPE
public AngularAzEl(GroundStation station, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, ObservableSatellite satellite)
station
- ground station from which measurement is performeddate
- date of the measurementangular
- observed valuesigma
- theoretical standard deviationbaseWeight
- base weightsatellite
- satellite related to this measurementprotected EstimatedMeasurementBase<AngularAzEl> theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
The theoretical value does not have any modifiers applied.
theoreticalEvaluationWithoutDerivatives
in class AbstractMeasurement<AngularAzEl>
iteration
- iteration numberevaluation
- evaluation numberstates
- orbital states at measurement dateAbstractMeasurement.estimate(int, int, SpacecraftState[])
protected EstimatedMeasurement<AngularAzEl> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
The theoretical value does not have any modifiers applied.
theoreticalEvaluation
in class AbstractMeasurement<AngularAzEl>
iteration
- iteration numberevaluation
- evaluation numberstates
- orbital states at measurement dateAbstractMeasurement.estimate(int, int, SpacecraftState[])
public org.hipparchus.geometry.euclidean.threed.Vector3D getObservedLineOfSight(Frame outputFrame)
outputFrame
- output frame of the line of sight vectorCopyright © 2002-2023 CS GROUP. All rights reserved.