Package | Description |
---|---|
org.orekit.estimation.measurements |
The measurements package defines everything that is related to orbit
determination measurements.
|
org.orekit.estimation.measurements.modifiers |
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 |
AngularRaDec.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.
|
GroundStation |
AngularAzEl.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)
Simple constructor.
|
AngularAzEl(GroundStation station,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight,
int propagatorIndex)
Simple constructor.
|
AngularRaDec(GroundStation station,
Frame referenceFrame,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight)
Simple constructor.
|
AngularRaDec(GroundStation station,
Frame referenceFrame,
AbsoluteDate date,
double[] angular,
double[] sigma,
double[] baseWeight,
int propagatorIndex)
Simple constructor.
|
Range(GroundStation station,
AbsoluteDate date,
double range,
double sigma,
double baseWeight)
Simple constructor.
|
Range(GroundStation station,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
int propagatorIndex)
Simple constructor.
|
RangeRate(GroundStation station,
AbsoluteDate date,
double rangeRate,
double sigma,
double baseWeight,
boolean twoway)
Simple constructor.
|
RangeRate(GroundStation station,
AbsoluteDate date,
double rangeRate,
double sigma,
double baseWeight,
boolean twoway,
int propagatorIndex)
Simple constructor.
|
TurnAroundRange(GroundStation masterStation,
GroundStation slaveStation,
AbsoluteDate date,
double turnAroundRange,
double sigma,
double baseWeight)
Simple constructor.
|
TurnAroundRange(GroundStation masterStation,
GroundStation slaveStation,
AbsoluteDate date,
double turnAroundRange,
double sigma,
double baseWeight,
int propagatorIndex)
Simple constructor.
|
Modifier and Type | Method and Description |
---|---|
double |
RangeRateTroposphericDelayModifier.rangeRateErrorTroposphericModel(GroundStation station,
SpacecraftState state)
Compute the measurement error due to Troposphere.
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