Package | Description |
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org.orekit.estimation.measurements |
The measurements package defines everything that is related to orbit
determination measurements.
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org.orekit.estimation.measurements.filtering |
This package provides measurement pre-processing filters.
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org.orekit.estimation.measurements.generation |
This package provides Orbit Determination measurements generation.
|
org.orekit.estimation.measurements.gnss |
This package provides methods to handle GNSS measurements.
|
org.orekit.estimation.measurements.modifiers |
This package provides measurement modifier.
|
Modifier and Type | Method and Description |
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GroundStation |
TurnAroundRange.getMasterStation()
Get the master ground station from which measurement is performed.
|
GroundStation |
TurnAroundRange.getSlaveStation()
Get the slave ground station reflecting the signal.
|
GroundStation |
Range.getStation()
Get the ground station from which measurement is performed.
|
GroundStation |
AngularAzEl.getStation()
Get the ground station from which measurement is performed.
|
GroundStation |
RangeRate.getStation()
Get the ground station from which measurement is performed.
|
GroundStation |
AngularRaDec.getStation()
Get the ground station from which measurement is performed.
|
Constructor and Description |
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AngularAzEl(GroundStation station,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
AngularRaDec(GroundStation station,
Frame referenceFrame,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
Range(GroundStation station,
boolean twoWay,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
RangeRate(GroundStation station,
AbsoluteDate date,
double rangeRate,
double sigma,
double baseWeight,
boolean twoway,
ObservableSatellite satellite)
Simple constructor.
|
TurnAroundRange(GroundStation masterStation,
GroundStation slaveStation,
AbsoluteDate date,
double turnAroundRange,
double sigma,
double baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
Constructor and Description |
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ElevationFilter(GroundStation station,
double threshold)
Constructor.
|
Constructor and Description |
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AngularAzElBuilder(CorrelatedRandomVectorGenerator noiseSource,
GroundStation station,
double[] sigma,
double[] baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
AngularRaDecBuilder(CorrelatedRandomVectorGenerator noiseSource,
GroundStation station,
Frame referenceFrame,
double[] sigma,
double[] baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
RangeBuilder(CorrelatedRandomVectorGenerator noiseSource,
GroundStation station,
boolean twoWay,
double sigma,
double baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
RangeRateBuilder(CorrelatedRandomVectorGenerator noiseSource,
GroundStation station,
boolean twoWay,
double sigma,
double baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
TurnAroundRangeBuilder(CorrelatedRandomVectorGenerator noiseSource,
GroundStation masterStation,
GroundStation slaveStation,
double sigma,
double baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
Modifier and Type | Method and Description |
---|---|
GroundStation |
Phase.getStation()
Get the ground station from which measurement is performed.
|
Constructor and Description |
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Phase(GroundStation station,
AbsoluteDate date,
double phase,
double wavelength,
double sigma,
double baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
PhaseBuilder(CorrelatedRandomVectorGenerator noiseSource,
GroundStation station,
double wavelength,
double sigma,
double baseWeight,
ObservableSatellite satellite)
Simple constructor.
|
Modifier and Type | Method and Description |
---|---|
<T extends RealFieldElement<T>> |
RangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(GroundStation station,
FieldSpacecraftState<T> state,
T[] parameters)
Compute the measurement error due to Troposphere.
|
double |
RangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(GroundStation station,
SpacecraftState state)
Compute the measurement error due to Troposphere.
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