Comparable<AngularAzEl>
, ComparableMeasurement
, ObservedMeasurement<AngularAzEl>
, TimeStamped
public class AngularAzEl extends AbstractMeasurement<AngularAzEl>
Constructor | Description |
---|---|
AngularAzEl(GroundStation station,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight) |
Deprecated.
since 9.3, replaced by
AngularAzEl(GroundStation, AbsoluteDate,
double[], double[], double[], ObservableSatellite) |
AngularAzEl(GroundStation station,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight,
int propagatorIndex) |
Deprecated.
since 9.3, replaced by
AngularAzEl(GroundStation, AbsoluteDate,
double[], double[], double[], ObservableSatellite) |
AngularAzEl(GroundStation station,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
Modifier and Type | Method | Description |
---|---|---|
GroundStation |
getStation() |
Get the ground station from which measurement is performed.
|
protected EstimatedMeasurement<AngularAzEl> |
theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states) |
Estimate the theoretical value.
|
addModifier, addParameterDriver, estimate, getBaseWeight, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getPropagatorsIndices, getSatellites, getTheoreticalStandardDeviation, isEnabled, setEnabled, signalTimeOfFlight, signalTimeOfFlight
compareTo
@Deprecated public AngularAzEl(GroundStation station, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight)
AngularAzEl(GroundStation, AbsoluteDate,
double[], double[], double[], ObservableSatellite)
This constructor uses 0 as the index of the propagator related to this measurement, thus being well suited for mono-satellite orbit determination.
station
- ground station from which measurement is performeddate
- date of the measurementangular
- observed valuesigma
- theoretical standard deviationbaseWeight
- base weight@Deprecated public AngularAzEl(GroundStation station, AbsoluteDate date, double[] angular, double[] sigma, double[] baseWeight, int propagatorIndex)
AngularAzEl(GroundStation, AbsoluteDate,
double[], double[], double[], ObservableSatellite)
station
- ground station from which measurement is performeddate
- date of the measurementangular
- observed valuesigma
- theoretical standard deviationbaseWeight
- base weightpropagatorIndex
- index of the propagator related to this measurementpublic 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 measurementpublic GroundStation getStation()
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[])
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