Uses of Class
org.orekit.estimation.measurements.ObservableSatellite

Packages that use ObservableSatellite

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.

Uses of ObservableSatellite in org.orekit.estimation.measurements

Methods in org.orekit.estimation.measurements that return types with arguments of type ObservableSatellite

Modifier and Type	Method	Description
List<ObservableSatellite>	AbstractMeasurement.getSatellites()	Get the satellites related to this measurement.
default List<ObservableSatellite>	ObservedMeasurement.getSatellites()	Get the satellites related to this measurement.

Constructors in org.orekit.estimation.measurements with parameters of type ObservableSatellite

Constructor	Description
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.
InterSatellitesRange(ObservableSatellite local, ObservableSatellite remote, boolean twoWay, AbsoluteDate date, double range, double sigma, double baseWeight)	Simple constructor.
Phase(GroundStation station, AbsoluteDate date, double phase, double wavelength, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
Position(AbsoluteDate date, org.hipparchus.geometry.euclidean.threed.Vector3D position, double[][] covarianceMatrix, double baseWeight, ObservableSatellite satellite)	Constructor with full covariance matrix and all inputs.
Position(AbsoluteDate date, org.hipparchus.geometry.euclidean.threed.Vector3D position, double[] sigmaPosition, double baseWeight, ObservableSatellite satellite)	Constructor with one vector for the standard deviation.
Position(AbsoluteDate date, org.hipparchus.geometry.euclidean.threed.Vector3D position, double sigmaPosition, double baseWeight, ObservableSatellite satellite)	Constructor with one double for the standard deviation.
PV(AbsoluteDate date, org.hipparchus.geometry.euclidean.threed.Vector3D position, org.hipparchus.geometry.euclidean.threed.Vector3D velocity, double[][] positionCovarianceMatrix, double[][] velocityCovarianceMatrix, double baseWeight, ObservableSatellite satellite)	Constructor with 2 smaller covariance matrices.
PV(AbsoluteDate date, org.hipparchus.geometry.euclidean.threed.Vector3D position, org.hipparchus.geometry.euclidean.threed.Vector3D velocity, double[][] covarianceMatrix, double baseWeight, ObservableSatellite satellite)	Constructor with full covariance matrix and all inputs.
PV(AbsoluteDate date, org.hipparchus.geometry.euclidean.threed.Vector3D position, org.hipparchus.geometry.euclidean.threed.Vector3D velocity, double[] sigmaPosition, double[] sigmaVelocity, double baseWeight, ObservableSatellite satellite)	Constructor with two vectors for the standard deviations.
PV(AbsoluteDate date, org.hipparchus.geometry.euclidean.threed.Vector3D position, org.hipparchus.geometry.euclidean.threed.Vector3D velocity, double[] sigmaPV, double baseWeight, ObservableSatellite satellite)	Constructor with one vector for the standard deviations.
PV(AbsoluteDate date, org.hipparchus.geometry.euclidean.threed.Vector3D position, org.hipparchus.geometry.euclidean.threed.Vector3D velocity, double sigmaPosition, double sigmaVelocity, double baseWeight, ObservableSatellite satellite)	Constructor with two double for the standard deviations.
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 parameters in org.orekit.estimation.measurements with type arguments of type ObservableSatellite

Constructor	Description
AbstractMeasurement(AbsoluteDate date, double[] observed, double[] sigma, double[] baseWeight, List<ObservableSatellite> satellites)	Simple constructor, for multi-dimensional measurements.
AbstractMeasurement(AbsoluteDate date, double observed, double sigma, double baseWeight, List<ObservableSatellite> satellites)	Simple constructor for mono-dimensional measurements.

Uses of ObservableSatellite in org.orekit.estimation.measurements.generation

Methods in org.orekit.estimation.measurements.generation that return ObservableSatellite

Modifier and Type	Method	Description
ObservableSatellite	Generator.addPropagator(Propagator propagator)	Add a propagator.
protected ObservableSatellite[]	AbstractMeasurementBuilder.getSatellites()	Get the satellites related to this measurement.

Methods in org.orekit.estimation.measurements.generation with parameters of type ObservableSatellite

Modifier and Type	Method	Description
Propagator	Generator.getPropagator(ObservableSatellite satellite)	Get a registered propagator.

Constructors in org.orekit.estimation.measurements.generation with parameters of type ObservableSatellite

Constructor	Description
AbstractMeasurementBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource, double[] sigma, double[] baseWeight, ObservableSatellite... satellites)	Simple constructor.
AbstractMeasurementBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource, double sigma, double baseWeight, ObservableSatellite... satellites)	Simple constructor.
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.
InterSatellitesRangeBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource, ObservableSatellite local, ObservableSatellite remote, boolean twoWay, double sigma, double baseWeight)	Simple constructor.
PositionBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource, double sigma, double baseWeight, ObservableSatellite satellite)	Simple constructor.
PVBuilder(org.hipparchus.random.CorrelatedRandomVectorGenerator noiseSource, double sigmaPosition, double sigmaVelocity, 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.