Package | Description |
---|---|
org.orekit.estimation.measurements |
The measurements package defines everything that is related to orbit
determination measurements.
|
org.orekit.estimation.measurements.generation |
This package provides Orbit Determination measurements generation.
|
org.orekit.estimation.measurements.modifiers |
Modifier and Type | Method | Description |
---|---|---|
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 |
AngularAzEl.getStation() |
Get the ground station from which measurement is performed.
|
GroundStation |
AngularRaDec.getStation() |
Get the ground station from which measurement is performed.
|
GroundStation |
Phase.getStation() |
Get the ground station from which measurement is performed.
|
GroundStation |
Range.getStation() |
Get the ground station from which measurement is performed.
|
GroundStation |
RangeRate.getStation() |
Get the ground station from which measurement is performed.
|
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.
|
AngularRaDec(GroundStation station,
Frame referenceFrame,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight) |
Deprecated.
|
AngularRaDec(GroundStation station,
Frame referenceFrame,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight,
int propagatorIndex) |
Deprecated.
|
AngularRaDec(GroundStation station,
Frame referenceFrame,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
Phase(GroundStation station,
AbsoluteDate date,
double phase,
double wavelength,
double sigma,
double baseWeight) |
Deprecated.
|
Phase(GroundStation station,
AbsoluteDate date,
double phase,
double wavelength,
double sigma,
double baseWeight,
int propagatorIndex) |
Deprecated.
|
Phase(GroundStation station,
AbsoluteDate date,
double phase,
double wavelength,
double sigma,
double baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
Range(GroundStation station,
boolean twoWay,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
int propagatorIndex) |
Deprecated.
as of 9.3, replaced by
Range(GroundStation, boolean, AbsoluteDate,
double, double, double, ObservableSatellite) |
Range(GroundStation station,
boolean twoWay,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
Range(GroundStation station,
AbsoluteDate date,
double range,
double sigma,
double baseWeight) |
Deprecated.
as of 9.3, replaced by
Range(GroundStation, boolean, AbsoluteDate,
double, double, double, ObservableSatellite) |
Range(GroundStation station,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
boolean twoWay) |
Deprecated.
as of 9.3, replaced by
Range(GroundStation, boolean, AbsoluteDate,
double, double, double, ObservableSatellite) |
Range(GroundStation station,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
int propagatorIndex) |
Deprecated.
as of 9.3, replaced by
Range(GroundStation, boolean, AbsoluteDate,
double, double, double, ObservableSatellite) |
RangeRate(GroundStation station,
AbsoluteDate date,
double rangeRate,
double sigma,
double baseWeight,
boolean twoway) |
Deprecated.
|
RangeRate(GroundStation station,
AbsoluteDate date,
double rangeRate,
double sigma,
double baseWeight,
boolean twoway,
int propagatorIndex) |
Deprecated.
|
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) |
Deprecated.
|
TurnAroundRange(GroundStation masterStation,
GroundStation slaveStation,
AbsoluteDate date,
double turnAroundRange,
double sigma,
double baseWeight,
int propagatorIndex) |
Deprecated.
|
TurnAroundRange(GroundStation masterStation,
GroundStation slaveStation,
AbsoluteDate date,
double turnAroundRange,
double sigma,
double baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
Constructor | Description |
---|---|
AngularAzElBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource,
GroundStation station,
double[] sigma,
double[] baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
AngularRaDecBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource,
GroundStation station,
Frame referenceFrame,
double[] sigma,
double[] baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
RangeBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource,
GroundStation station,
boolean twoWay,
double sigma,
double baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
RangeRateBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource,
GroundStation station,
boolean twoWay,
double sigma,
double baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
TurnAroundRangeBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource,
GroundStation masterStation,
GroundStation slaveStation,
double sigma,
double baseWeight,
ObservableSatellite satellite) |
Simple constructor.
|
Modifier and Type | Method | Description |
---|---|---|
<T extends org.hipparchus.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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