A C D E F G I J K L M N O P R S T U V W Y
All Classes All Packages
All Classes All Packages
All Classes All Packages
A
- AbstractOrbitDetermination<T extends org.orekit.propagation.conversion.PropagatorBuilder> - Class in org.orekit.tutorials.estimation.common
-
Base class for Orekit orbit determination tutorials.
- AbstractOrbitDetermination() - Constructor for class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
- AbstractOrbitDeterminationEngine<T extends org.orekit.propagation.conversion.PropagatorBuilder> - Class in org.orekit.tutorials.estimation.common
-
Base class for Orekit orbit determination tutorials.
- AbstractOrbitDeterminationEngine() - Constructor for class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
- ApogeeManeuver - Class in org.orekit.tutorials.maneuvers
-
Orekit tutorial for an apogee maneuver.
- AttitudeMode - Enum in org.orekit.tutorials.estimation.common
-
Attitude modes.
C
- CENTER_POINTING_WITH_YAW_STEERING - org.orekit.tutorials.estimation.common.AttitudeMode
-
Body center pointing with yaw compensation.
- compareWithReference(Orbit) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Compare the estimated orbit with a reference orbit.
- compareWithReference(Orbit) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Compare the estimated orbit with a reference orbit.
- compareWithReference(Orbit) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Compare the estimated orbit with a reference orbit.
- compareWithReference(Orbit) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Compare the estimated orbit with a reference orbit.
- compareWithReference(Orbit) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Compare the estimated orbit with a reference orbit.
- compareWithReference(Orbit) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Compare the estimated orbit with a reference orbit.
- compareWithReference(Orbit) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Compare the estimated orbit with a reference orbit.
- compareWithReference(Orbit) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Compare the estimated orbit with a reference orbit.
- compareWithReference(Orbit) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Compare the estimated orbit with a reference orbit.
- containsKey(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Check if a key is contained in the map.
- Context - Class in org.orekit.tutorials.data
-
Orekit tutorial for data contexts.
- Context() - Constructor for class org.orekit.tutorials.data.Context
- CovariancePropagation - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for covariance matrix propagation.
- CR3BPSphereCrossingDetector - Class in org.orekit.tutorials.propagation.cr3bp
-
Detector for YZ Planes crossing.
- CR3BPSphereCrossingDetector(double, double, CR3BPSystem, double, double) - Constructor for class org.orekit.tutorials.propagation.cr3bp.CR3BPSphereCrossingDetector
-
Simple Constructor.
- create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.tutorials.propagation.cr3bp.CR3BPSphereCrossingDetector
- create(AdaptableInterval, double, int, EventHandler) - Method in class org.orekit.tutorials.propagation.cr3bp.YZPlaneCrossingDetector
- createBody(TutorialBody) - Static method in class org.orekit.tutorials.utils.OrekitBuilder
-
Create a central body.
- createCartesianCovariance(AbsoluteDate, Frame, RealMatrix) - Static method in class org.orekit.tutorials.utils.NdmUtils
-
Creates a CartesianCovariance data block.
- createCommonMetadata(CenterName, String, String, Frame) - Static method in class org.orekit.tutorials.utils.NdmUtils
-
Creates the common meta data.
- createGravityField(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Create a gravity field from input parameters.
- createGravityField(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Create a gravity field from input parameters.
- createGravityField(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Create a gravity field from input parameters.
- createGravityField(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Create a gravity field from input parameters.
- createGravityField(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Create a gravity field from input parameters.
- createGravityField(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Create a gravity field from input parameters.
- createGravityField(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Create a gravity field from input parameters.
- createGravityField(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Create a gravity field from input parameters.
- createGravityField(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Create a gravity field from input parameters.
- createHeader() - Static method in class org.orekit.tutorials.utils.NdmUtils
-
Creates a header for a NDM.
- createKeplerianElements(Orbit) - Static method in class org.orekit.tutorials.utils.NdmUtils
-
Creates a KeplerianElements data block from a orbit.
- createOpmSegments(OdmCommonMetadata, OpmData) - Static method in class org.orekit.tutorials.utils.NdmUtils
-
Creates the segments for an OPM.
- createOrbit(TutorialOrbit, double) - Static method in class org.orekit.tutorials.utils.OrekitBuilder
-
Create an orbit from input parameters.
- createPropagatorBuilder(Orbit, ODEIntegratorBuilder, double) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Create a propagator builder from input parameters.
- createPropagatorBuilder(Orbit, ODEIntegratorBuilder, double) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Create a propagator builder from input parameters.
- createPropagatorBuilder(Orbit, ODEIntegratorBuilder, double) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Create a propagator builder from input parameters.
- createPropagatorBuilder(Orbit, ODEIntegratorBuilder, double) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Create a propagator builder from input parameters.
- createPropagatorBuilder(Orbit, ODEIntegratorBuilder, double) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Create a propagator builder from input parameters.
- createPropagatorBuilder(Orbit, ODEIntegratorBuilder, double) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Create a propagator builder from input parameters.
- createPropagatorBuilder(Orbit, ODEIntegratorBuilder, double) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Create a propagator builder from input parameters.
- createPropagatorBuilder(Orbit, ODEIntegratorBuilder, double) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Create a propagator builder from input parameters.
- createPropagatorBuilder(Orbit, ODEIntegratorBuilder, double) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Create a propagator builder from input parameters.
- createStateVector(TimeStampedPVCoordinates) - Static method in class org.orekit.tutorials.utils.NdmUtils
-
Creates a StateVector data block from PV coordinates.
- CustomHarmonicAccelerationModel - Class in org.orekit.tutorials.estimation.common
-
Harmonic acceleration model based on sine and cosine.
- CustomHarmonicAccelerationModel(String, AbsoluteDate, double, int) - Constructor for class org.orekit.tutorials.estimation.common.CustomHarmonicAccelerationModel
-
Simple constructor.
D
- DEFAULT_LAW - org.orekit.tutorials.estimation.common.AttitudeMode
-
Default law.
- DEFAULT_ORIGINATOR - Static variable in class org.orekit.tutorials.utils.NdmUtils
-
Default file originator.
- DEFAULT_VERSION - Static variable in class org.orekit.tutorials.utils.NdmUtils
-
Default version for CCSDS files.
- DEFile - Class in org.orekit.tutorials.bodies
-
This tutorial reads a DEXXX binary file (JPL or IMCCE inpop ephemeris file) and writes a new one containing only the data asked by the user.
- DOPComputation - Class in org.orekit.tutorials.gnss
-
Orekit tutorial for DOP computation.
- DSSTOrbitDetermination - Class in org.orekit.tutorials.estimation
-
Orekit tutorial for orbit determination using DSST theory.
- DSSTOrbitDetermination() - Constructor for class org.orekit.tutorials.estimation.DSSTOrbitDetermination
- DSSTPropagation - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for semi-analytical extrapolation using the DSST.
- DSSTPropagation.TutorialDSSTPropagation - Class in org.orekit.tutorials.propagation
-
Input data for the DSST propagation tutorial.
E
- EarthMoonHaloOrbit - Class in org.orekit.tutorials.propagation.cr3bp
-
Orekit tutorial for the computation of a northern Halo Orbit around Earth-Moon L1.
- EarthObservation - Class in org.orekit.tutorials.attitude
-
Orekit tutorial for Earth observation attitude sequence.
- EphemerisMode - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for ephemeris mode propagation.
- evaluationPerformed(int, int, Orbit[], ParameterDriversList, ParameterDriversList, ParameterDriversList, EstimationsProvider, LeastSquaresProblem.Evaluation) - Method in class org.orekit.tutorials.estimation.common.OrbitDeterminationObserver
- evaluationPerformed(KalmanEstimation) - Method in class org.orekit.tutorials.estimation.common.KalmanOrbitDeterminationObserver
- evaluationPerformed(KalmanEstimation) - Method in class org.orekit.tutorials.estimation.ExtendedSemianalyticalKalmanFilter.Observer
- ExtendedSemianalyticalKalmanFilter - Class in org.orekit.tutorials.estimation
-
Tutorial to present the Extended Semi-analytical Kalman Filter.
- ExtendedSemianalyticalKalmanFilter() - Constructor for class org.orekit.tutorials.estimation.ExtendedSemianalyticalKalmanFilter
- ExtendedSemianalyticalKalmanFilter.Observer - Class in org.orekit.tutorials.estimation
-
Observer for Kalman estimation.
F
- FieldPropagation - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for field mode propagation.
- finish(Propagator[]) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Initialization just after orekit-data setting.
- finish(Propagator[]) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Initialization just after orekit-data setting.
- Frames1 - Class in org.orekit.tutorials.frames
-
Orekit tutorial for basic frames support.
- Frames2 - Class in org.orekit.tutorials.frames
-
Orekit tutorial for advanced frames support.
- Frames3 - Class in org.orekit.tutorials.frames
-
Orekit tutorial for computing spacecraft related data.
G
- g(SpacecraftState) - Method in class org.orekit.tutorials.propagation.cr3bp.CR3BPSphereCrossingDetector
-
Compute the value of the detection function.
- g(SpacecraftState) - Method in class org.orekit.tutorials.propagation.cr3bp.YZPlaneCrossingDetector
-
Compute the value of the detection function.
- generateMeasurements() - Method in class org.orekit.tutorials.estimation.performance.PerformanceTesting.TutorialPerformanceTesting
-
Get the flag for measurement generation.
- getA() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Get the semi major axis.
- getA() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Get the semi major axis.
- getA() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Get the semi major axis.
- getAccelerationDirection() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Get the acceleration direction in defining frame.
- getAlphaV() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Get the true latitude argument.
- getAltitude() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the station altitude as read in the YAML file.
- getAngle(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get an angle value from a parameters map.
- getAngleArray(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get an angle values array from a parameters map.
- getAngularOffset() - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Get the angular offset.
- getAntennaOffset() - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Get the coordinates of the on-board antenna phase center in spacecraft frame.
- getArea() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialDrag
-
Get the cross section.
- getArea() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialSolarRadiationPressure
-
Get the cross section.
- getAttitudeMode() - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Get the name of the attitude mode.
- getAzEl() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the azimuth/elevation measurement data.
- getAzElBias() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the estimated azimuth/elevation measurement bias.
- getBias() - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Get the estimated On-board range bias.
- getBody() - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Get the body data.
- getBody() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Get the body data.
- getBody() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the body data.
- getBoolean(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a raw boolean value from a parameters map.
- getBooleanArray(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a raw boolean values array from a parameters map.
- getCartesian() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Get the cartesian elements.
- getCartesianOrbitalP() - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Get the initial diagonal elements of the cartesian covariance matrix.
- getCartesianOrbitalQ() - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Get the initial diagonal elements of the cartesian process noise matrix.
- getCd() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialDrag
-
Get the estimated drag coefficient.
- getCelestialBodies() - Method in class org.orekit.tutorials.data.Context
- getCircular() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Get the circular elements.
- getClockOffset() - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Get the estimated On-board clock offset.
- getClockOffset() - Method in class org.orekit.tutorials.yaml.TutorialStation.TutorialObservationType
-
Get the estimated station clock offset.
- getCoefficients() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Get the array of acceleration coefficients.
- getConvergenceThreshold() - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Get the convergence threshold.
- getCoordinates() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the array containing the station coordinates.
- getCorrectionDate() - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Get the medium date used to initialize the time span tropospheric model.
- getCr() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialSolarRadiationPressure
-
Get the estimated reflection coefficient.
- getCycleDuration() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the SK cycle duration.
- getCyclesNumber() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the number of SK cycles to simulate.
- getDate() - Method in class org.orekit.tutorials.yaml.TutorialOrbit
-
Get the String representation of the orbit date.
- getDate(Key, TimeScale) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a date value from a parameters map.
- getDateArray(Key, TimeScale) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a date values array from a parameters map.
- getDegree() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialGravity
-
Get the maximal degree.
- getDegree() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialOceanTides
-
Get the maximal degree.
- getDeltaVMax() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the DV max.
- getDirection() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Get the thust direction.
- getDirections() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Get the acceleration direction in defining frame.
- getDouble(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a raw double value from a parameters map.
- getDoubleArray(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a raw double values array from a parameters map.
- getDrag() - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Get the drag force model.
- getDuration() - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Get the simulation duration.
- getDuration() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Get the estimated duration.
- getDurationInDays() - Method in class org.orekit.tutorials.estimation.SequentialBatchLeastSquares.TutorialSequentialBatch
-
Get the simulation duration.
- getDurationInDays() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the simulation duration.
- getE() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Get the orbit eccentricity.
- getEarthFrame() - Method in class org.orekit.tutorials.yaml.TutorialBody
-
Get the Earth frame.
- getEarthFrame(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get an Earth frame from a parameters map.
- getEasternBoundary() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the eastern boundary for longitude window.
- getEndDate() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Get the end date for measurement generation.
- getEquatorialRadius() - Method in class org.orekit.tutorials.yaml.TutorialBody
-
Get the equatorial radius of the body.
- getEquinoctial() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Get the equinoctial elements.
- getEstimator() - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Get the batch least square estimator data.
- getEx() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEx() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Get the first component of the equinoctial eccentricity vector.
- getEy() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getEy() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Get the second component of the equinoctial eccentricity vector.
- getFixedNumberOfInterpolationPoints() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the interpolation grid specification.
- getFixedStep() - Method in class org.orekit.tutorials.yaml.TutorialIntegrator
-
Get the fixed step size.
- getFlowRate() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Get the estimated flow rate.
- getForceModels() - Method in class org.orekit.tutorials.yaml.TutorialPropagator
-
Get the force model data.
- getFrameName() - Method in class org.orekit.tutorials.yaml.TutorialBody
-
Get the name of the body frame related to body shape.
- getFrameName() - Method in class org.orekit.tutorials.yaml.TutorialOrbit
-
Get the name of the inertial orbit frame.
- getFrames() - Method in class org.orekit.tutorials.data.Context
- getGaussNewton() - Method in class org.orekit.tutorials.yaml.TutorialOptimizationEngine
-
Get the Gauss-Newton optimization engine.
- getGeoMagneticFields() - Method in class org.orekit.tutorials.data.Context
- getGravity() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the gravity data.
- getGravity() - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Get the central body gravity force model.
- getGravityFields() - Method in class org.orekit.tutorials.data.Context
- getGrids() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the list of grid data.
- getHx() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Get the first component of the inclination vector.
- getHy() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Get the second component of the inclination vector.
- getI() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Get the orbit inclination.
- getI() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Get the orbit inclination.
- getId() - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Get the satellite ID.
- getIersConventionYear() - Method in class org.orekit.tutorials.yaml.TutorialBody
-
Get the year of the IERS Convention (1996, 2003 or 2010).
- getInertialFrame() - Method in class org.orekit.tutorials.yaml.TutorialOrbit
-
Get the inertial frame.
- getInertialFrame(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get an inertial frame from a parameters map.
- getInitialMass() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the initial mass of the spacecraft.
- getInitialStep() - Method in class org.orekit.tutorials.yaml.TutorialOptimizationEngine.TutorialLevenbergMarquardt
-
Get the optimizer's initial step.
- getInitialValue() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedDateParameter
-
Get the initial value for the estimated date parameter.
- getInitialValue() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedParameter
-
Get the initial value for the estimated parameter.
- getInt(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a raw int value from a parameters map.
- getIntArray(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a raw int values array from a parameters map.
- getIntegrator() - Method in class org.orekit.tutorials.yaml.TutorialPropagator
-
Get the numerical integrator used by the orbit propagator.
- getInverseFlattening() - Method in class org.orekit.tutorials.yaml.TutorialBody
-
Get the inverse flattening of the body.
- getIonosphere() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the ionospheric model.
- getIonosphericLayer() - Method in class org.orekit.tutorials.yaml.TutorialIonosphere
-
Get the height of the ionospheric layer.
- getIsp() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the ISP.
- getIsp() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Get the Isp.
- getKalman() - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Get the kalman filter data.
- getKeplerian() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Get the keplerian elements.
- getLatitude() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialGrid
-
Get the point latitude.
- getLatitude() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the station latitude as read in the YAML file.
- getLevenbergMarquardt() - Method in class org.orekit.tutorials.yaml.TutorialOptimizationEngine
-
Get the Levenberg-Marquardt optimization engine.
- getLine1() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialTLE
-
Get the TLE first line.
- getLine2() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialTLE
-
Get the TLE second line.
- getLongitude() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the station longitude as read in the YAML file.
- getLv() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Get the mean anomaly.
- getManeuvers() - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Get the list of maneuvers.
- getMappingFunction() - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Get the name of the tropospheric mapping function.
- getMass() - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Get the spacecraft mass.
- getMaxEvaluations() - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Get the maximum number of evaluations before an exception is thrown.
- getMaxIterations() - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Get the maximum number of iterations before an exception is thrown.
- getMaxMDaily() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the maximum order of m-daily terms for eccentricity fitting.
- getMaxStep() - Method in class org.orekit.tutorials.yaml.TutorialIntegrator
-
Get the maximum step size.
- getMaxTimeGapBetweenInterpolationPoints() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the interpolation grid specification.
- getMaxValue() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedDateParameter
-
Get the maximum allowed value for the date parameter.
- getMaxValue() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedParameter
-
Get the maximum allowed value for the parameter.
- getMeanLongitude(Orbit) - Method in class org.orekit.tutorials.maneuvers.StationKeeping
-
Get Earth based mean longitude.
- getMeanSolarTime() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the string representation of the mean solar time.
- getMeasurementFiles() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the list of measurement files.
- getMeasurementGenerationInputFile() - Method in class org.orekit.tutorials.estimation.performance.PerformanceTesting.TutorialPerformanceTesting
-
Get the name of the input YAML file for measurement generation.
- getMeasurementP() - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Get the initial diagonal elements of the measurement covariance matrix.
- getMeasurementQ() - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Get the initial diagonal elements of the measurement process noise matrix.
- getMeasurements() - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Get the measurements data.
- getMeasurements() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Get the measurement data.
- getMedianDate() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Get the estimated median date.
- getMinElevation() - Method in class org.orekit.tutorials.propagation.VisibilityCircle.TutorialVisibilityCircle
-
Get the minimum elevation for defining visibility above ground.
- getMinStep() - Method in class org.orekit.tutorials.yaml.TutorialIntegrator
-
Get the minimum step size.
- getMinValue() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedDateParameter
-
Get the minimum allowed value for the date parameter.
- getMinValue() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedParameter
-
Get the minimum allowed value for the parameter.
- getMu() - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Get the central attraction coefficient.
- getMu() - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Get the central attraction coefficient.
- getMu() - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Get the central attraction coefficient.
- getMu() - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Get the central attraction coefficient.
- getMu() - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Get the central attraction coefficient.
- getMu() - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Get the central attraction coefficient.
- getMu() - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Get the central attraction coefficient.
- getMu() - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Get the central attraction coefficient.
- getMu() - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Get the central attraction coefficient.
- getName() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Get the name.
- getName() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Get the prefix to use for parameter drivers.
- getName() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialThirdBody
-
Get the name of the celestial body.
- getName() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Get the name of the orbit type.
- getName() - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Get the satellite name.
- getName() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the station name.
- getName() - Method in class org.orekit.tutorials.yaml.TutorialStation.TutorialObservationType
-
Get the name of the observation type.
- getNbMaxManeuvers() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the max number of maneuvers per cycle.
- getObjectId() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the id of the object.
- getObjectName() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the name of the object.
- getObservationTypes() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the list of observation types.
- getOceanTides() - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Get the ocean tides force model.
- getOemDuration() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the OEM duration.
- getOemStep() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the OEM step size.
- getOptimizationEngine() - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Get the optimization engine.
- getOrbit() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the orbit data.
- getOrbit() - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Get the orbit data.
- getOrbit() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Get the orbit data.
- getOrbit() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the orbit data.
- getOrbit() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the orbit data.
- getOrbit() - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Get the orbit data (circular orbit).
- getOrbitalParametersPositionScale() - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Get the scaling factor for orbital parameters normalization.
- getOrbitDetermination() - Method in class org.orekit.tutorials.estimation.SequentialBatchLeastSquares.TutorialSequentialBatch
-
Get the orbit determination data.
- getOrbitDeterminationInputFile() - Method in class org.orekit.tutorials.estimation.performance.PerformanceTesting.TutorialPerformanceTesting
-
Get the name of the input YAML file for orbit determination.
- getOrbitsSeparation() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the number of orbits between maneuvers.
- getOrbitType() - Method in class org.orekit.tutorials.yaml.TutorialOrbit
-
Get the orbit type (name and orbital elements).
- getOrbitType() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Get the orbit type.
- getOrder() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialGravity
-
Get the maximal order.
- getOrder() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialOceanTides
-
Get the maximal order.
- getOutlierRejectionMultiplier() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the detection limit for outliers.
- getOutlierRejectionStartingIteration() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the number of iterations before with filter is not applied.
- getOutputBaseName() - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Get the base name of the output files (log and residuals).
- getOutputBaseName() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Get the name of the output measurement file.
- getOutputShortPeriodCoefficients() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the list of short period coefficients to output.
- getOutputStep() - Method in class org.orekit.tutorials.estimation.SequentialBatchLeastSquares.TutorialSequentialBatch
-
Get the time step for OEM generation.
- getOutputStep() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the time step between printed elements.
- getOutputStep() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the time step between printed elements.
- getPa() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Get the perigee argument.
- getParametersDrivers() - Method in class org.orekit.tutorials.estimation.common.CustomHarmonicAccelerationModel
- getPhase() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the phase measurement data.
- getPhaseBias() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the estimated phase measurement bias.
- getPhasingDaysNumer() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the number of days in the phasing cycle.
- getPhasingOrbitsNumber() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the number of orbits in the phasing cycle.
- getPointsNumber() - Method in class org.orekit.tutorials.propagation.VisibilityCircle.TutorialVisibilityCircle
-
Get the number of points to compute.
- getPolynomialAcceleration() - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Get the list of polynomial acceleration force models.
- getPosition() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the position only measurement data.
- getPositionAngle() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Get the name of the position angle.
- getPositionAngle() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Get the name of the position angle.
- getPositionAngle() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Get the name of the position angle.
- getPositionError() - Method in class org.orekit.tutorials.yaml.TutorialIntegrator
-
Get the position error.
- getPropagationP() - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Get the initial diagonal elements of the propagation covariance matrix.
- getPropagationQ() - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Get the initial diagonal elements of the propagation process noise matrix.
- getPropagator() - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Get the propagator data.
- getPropagator() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Get the propagator data.
- getPropagator() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the orbit propagator data.
- getProvider(Frame, OneAxisEllipsoid) - Method in enum org.orekit.tutorials.estimation.common.AttitudeMode
-
Get attitude provider.
- getPv() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the position/velocity measurement data.
- getPvBias() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the estimated position/velocity measurement bias.
- getRaan() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Get the right ascension of the ascending node.
- getRaan() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Get the right ascension of the ascending node.
- getRange() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the range measurement data.
- getRangeBias() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the estimated range measurement bias.
- getRangeRate() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the range rate measurement data.
- getRangeRateBias() - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Get the estimated range rate measurement bias.
- getReferenceLatitude() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the reference latitude for Sun synchronous orbit.
- getRelativity() - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Get the relativity force model.
- getSigma() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialAzEl
-
Get the theoretical standard deviation of the measurement.
- getSigma() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPhase
-
Get the theoretical standard deviation of the measurement.
- getSigma() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRange
-
Get the theoretical standard deviation of the measurement.
- getSigma() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRangeRate
-
Get the theoretical standard deviation of the measurement.
- getSigmaPos() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPosition
-
Get the theoretical standard deviation for position data.
- getSigmaPos() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPV
-
Get the theoretical standard deviation for position data.
- getSigmaVel() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPV
-
Get the theoretical standard deviation for velocity data.
- getSinex() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the sinex files containing station positions and eccentricities.
- getSolarRadiationPressure() - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Get the solar radiation pressure force model.
- getSpacecraft() - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Get the spacecraft data.
- getSpacecraft() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Get the spacecraft data.
- getSpacecraft() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the spacecraft data.
- getSpacecraftAltitude() - Method in class org.orekit.tutorials.propagation.VisibilityCircle.TutorialVisibilityCircle
-
Get the satellite altitude.
- getStartDate() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Get the start date for measurement generation.
- getStartDate() - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Get the simulation start date.
- getStartDate() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Get the estimated start date.
- getStation() - Method in class org.orekit.tutorials.propagation.VisibilityCircle.TutorialVisibilityCircle
-
Get the ground station.
- getStationDisplacement() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the station displacement data.
- getStationEccentricities() - Method in class org.orekit.tutorials.yaml.TutorialSinex
-
Get the path for sinex station eccentricities file.
- getStationPositions() - Method in class org.orekit.tutorials.yaml.TutorialSinex
-
Get the path for sinex station positions file.
- getStations() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the list of used stations.
- getStep() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Get the step for the measurement generation.
- getStep() - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Get the time step between each points.
- getStopDate() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Get the estimated stop date.
- getString(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a raw string value from a parameters map.
- getStringArray(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a raw string values array from a parameters map.
- getStringsList(Key, char) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a strings list from a parameters map.
- getStringsListArray(Key, char) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a strings list array from a parameters map.
- getThirdBody() - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Get the list of third body attraction force models.
- getThrust() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Get the estimated thrust.
- getTime(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a time value from a parameters map.
- getTimeArray(Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a time values array from a parameters map.
- getTimeScales() - Method in class org.orekit.tutorials.data.Context
- getTle() - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Get the TLE data.
- getTle() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Get the TLE data.
- getTroposphere() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the tropospheric model.
- getV() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Get the true anomaly.
- getValues() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedDateParameter
-
Get the initial, minimum and maximum dates for the parameter.
- getValues() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedParameter
-
Get the initial, minimum and maximum value of the parameter.
- getVector(Key, Key, Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a vector value from a parameters map.
- getVectorArray(Key, Key, Key) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Get a vector values array from a parameters map.
- getVtec() - Method in class org.orekit.tutorials.yaml.TutorialIonosphere
-
Get the estimated ionospheric parameter.
- getVx() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Get the first coordinate of the satellite velocity.
- getVy() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Get the second coordinate of the satellite velocity.
- getVz() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Get the third coordinate of the satellite velocity.
- getWeight() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialAzEl
-
Get the measurement base weight.
- getWeight() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPhase
-
Get the measurement base weight.
- getWeight() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPosition
-
Get the measurement base weight.
- getWeight() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPV
-
Get the measurement base weight.
- getWeight() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRange
-
Get the measurement base weight.
- getWeight() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRangeRate
-
Get the measurement base weight.
- getWesternBoundary() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the western boundary for longitude window.
- getX() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Get the first coordinate of position vector.
- getY() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Get the second coordinate of position vector.
- getZ() - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Get the third coordinate of the satellite position.
- getZenithDelay() - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Get the estimated troposheric parameter.
- GNSSOrbitDetermination - Class in org.orekit.tutorials.estimation
-
Orekit tutorial for Global Navigation Satellite System (GNSS) orbit determination.
- GNSSOrbitDetermination() - Constructor for class org.orekit.tutorials.estimation.GNSSOrbitDetermination
- GNSSPropagation - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for GNSS orbit propagation based on navigation messages.
- GradientComputation - Class in org.orekit.tutorials.propagation
-
Gradient Computation.
- GroundTrack - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for graphical display of ground tracks.
I
- ImpulseAtNode - Class in org.orekit.tutorials.maneuvers
-
Orekit tutorial for simple impulsive maneuver.
- init(SpacecraftState, AbsoluteDate) - Method in class org.orekit.tutorials.estimation.common.CustomHarmonicAccelerationModel
- init(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Initialization just after orekit-data setting.
- init(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Initialization just after orekit-data setting.
- isAnalytical() - Method in class org.orekit.tutorials.yaml.TutorialPropagator
-
Get the flag for the propagator type.
- isAscending() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialGrid
-
Get the indicator for latitude crossing direction.
- isEstimated() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedDateParameter
-
Get the flag for the date parameter estimation.
- isEstimated() - Method in class org.orekit.tutorials.yaml.TutorialEstimatedParameter
-
Get the flag for the parameter estimation.
- isEstimated() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Get the flag for acceleration coefficients estimation.
- isEstimatedModel() - Method in class org.orekit.tutorials.yaml.TutorialIonosphere
-
Get the flag to know if the ionospheric model is estimated of not.
- isEstimatedModel() - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Get the flag to know if tropospheric model is estimated of not.
- isFinished() - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator
-
Get the flag for measurement generation processing.
- isInitialOrbitIsOsculating() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the flag for initial orbit type.
- isKalman() - Method in class org.orekit.tutorials.estimation.performance.PerformanceTesting.TutorialPerformanceTesting
-
Get the flag for orbit determination engine.
- isNumericalComparison() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the flag for the comparison with the numerical orbit propagator.
- isOpmGenerated() - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Get the flag for the estimated OPM generation.
- isOutputOrbitIsOsculating() - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Get the flag for output orbit type.
- isPrintToFile() - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Get the flag for printing results to a file.
- isReferenceAscending() - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Get the reference indicator for latitude crossing direction.
- isUsed() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialRelativity
-
Get the flag to use the relativity force model.
- isWithOceanLoadingCorrection() - Method in class org.orekit.tutorials.yaml.TutorialStationDisplacement
-
Get the flag for the computation of ocean loading correction.
- isWithRefractionCorrection() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialAzEl
-
Get the flag for the computation of the refraction correction.
- isWithShapiro() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the flag for the computation of the Shapiro effect.
- isWithSolidTides() - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialThirdBody
-
Get the flag for the computation of the body's solid tides.
- isWithStationPositionEstimated() - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Get the flag for station position estimation.
- isWithTidalCorrection() - Method in class org.orekit.tutorials.yaml.TutorialStationDisplacement
-
Get the flag for the computation of the tidal displacement.
- isWithWeatherModel() - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Get the flag to know if an empirical model is used to compute station Temperature and Pressure.
J
- JupiterSwingBy - Class in org.orekit.tutorials.propagation
-
Swing-by trajectory about Jupiter compared in EME2000, ICRF and Jupiter-centered inertial reference frame.
K
- KalmanNumericalOrbitDetermination - Class in org.orekit.tutorials.estimation
-
Orekit tutorial for Kalman orbit determination.
- KalmanNumericalOrbitDetermination() - Constructor for class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
- KalmanOrbitDeterminationObserver - Class in org.orekit.tutorials.estimation.common
-
Observer for the KalmanNumericalOrbitDetermination scheme.
- KalmanOrbitDeterminationObserver(PrintStream, RangeLog, RangeRateLog, AzimuthLog, ElevationLog, PositionLog, VelocityLog) - Constructor for class org.orekit.tutorials.estimation.common.KalmanOrbitDeterminationObserver
-
Constructor.
- KeplerianPropagation - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for analytical propagation using the keplerian propagator.
- KeyValueFileParser<Key extends Enum<Key>> - Class in org.orekit.tutorials
-
Simple parser for key/value files.
- KeyValueFileParser(Class<Key>) - Constructor for class org.orekit.tutorials.KeyValueFileParser
-
Simple constructor.
L
- LaserRangingOrbitDetermination - Class in org.orekit.tutorials.estimation
-
Orekit tutorial for orbit determination based on laser ranging data.
- LaserRangingOrbitDetermination() - Constructor for class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
- LOF_ALIGNED_LVLH - org.orekit.tutorials.estimation.common.AttitudeMode
-
Aligned with Local Vertical, Local Horizontal frame.
- LOF_ALIGNED_QSW - org.orekit.tutorials.estimation.common.AttitudeMode
-
Aligned with QSW frame.
- LOF_ALIGNED_TNW - org.orekit.tutorials.estimation.common.AttitudeMode
-
Aligned with TNW frame.
- LOF_ALIGNED_VNC - org.orekit.tutorials.estimation.common.AttitudeMode
-
aligned with Velocity - Normal - Co-normal frame.
- LOF_ALIGNED_VVLH - org.orekit.tutorials.estimation.common.AttitudeMode
-
Aligned with Vehicle Velocity, Local Horizontal frame.
M
- main(String[]) - Static method in class org.orekit.tutorials.attitude.EarthObservation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.bodies.DEFile
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.bodies.Phasing
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.conversion.PropagatorConversion
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.conversion.TLEConversion
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.data.Context
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.ExtendedSemianalyticalKalmanFilter
-
Main method.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.ManeuverEstimation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.performance.PerformanceTesting
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.SequentialBatchLeastSquares
-
Main method.
- main(String[]) - Static method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.frames.Frames1
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.frames.Frames2
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.frames.Frames3
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.gnss.DOPComputation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.gnss.RinexObservationFile
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.maneuvers.ApogeeManeuver
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.maneuvers.ImpulseAtNode
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.maneuvers.StationKeeping
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.models.TidalDisplacements
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.CovariancePropagation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.cr3bp.EarthMoonHaloOrbit
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.cr3bp.ManifoldTransfer
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.cr3bp.PropagationInCR3BP
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.cr3bp.SunEarthMultipleShooter
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.DSSTPropagation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.EphemerisMode
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.FieldPropagation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.GNSSPropagation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.GradientComputation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.GroundTrack
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.JupiterSwingBy
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.KeplerianPropagation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.NumericalPropagation
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.PropagationInNonInertialFrame
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.PropagationInRotatingFrame
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.TrackCorridor
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.VisibilityCheck
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.propagation.VisibilityCircle
-
Program entry point.
- main(String[]) - Static method in class org.orekit.tutorials.time.Time1
-
Program entry point.
- ManeuverEstimation - Class in org.orekit.tutorials.estimation
-
Orekit tutorial for maneuver estimation.
- ManeuverEstimation() - Constructor for class org.orekit.tutorials.estimation.ManeuverEstimation
- ManifoldTransfer - Class in org.orekit.tutorials.propagation.cr3bp
-
Orekit tutorial for the computation of a transfer from Earth-Moon L2 Halo Orbit to High Lunar Orbit using unstable manifolds.
- MeasurementGenerator - Class in org.orekit.tutorials.estimation.performance
-
Class for measurement generation.
- MeasurementGenerator() - Constructor for class org.orekit.tutorials.estimation.performance.MeasurementGenerator
-
Constructor.
- MeasurementGenerator.TutorialMeasurementGeneration - Class in org.orekit.tutorials.estimation.performance
-
Tutorial input data.
N
- NADIR_POINTING_WITH_YAW_COMPENSATION - org.orekit.tutorials.estimation.common.AttitudeMode
-
Nadir pointing with yaw compensation.
- NdmUtils - Class in org.orekit.tutorials.utils
-
Utility class for parsing and generating CCSDS NDM files.
- NOT_EARTH_FRAME - Static variable in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Error message for not Earth frame.
- NumericalOrbitDetermination - Class in org.orekit.tutorials.estimation
-
Orekit tutorial for orbit determination.
- NumericalOrbitDetermination() - Constructor for class org.orekit.tutorials.estimation.NumericalOrbitDetermination
- NumericalPropagation - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for numerical orbit propagation
O
- Observer(PrintStream) - Constructor for class org.orekit.tutorials.estimation.ExtendedSemianalyticalKalmanFilter.Observer
-
Constructor.
- OrbitDeterminationEngine - Class in org.orekit.tutorials.estimation.performance
-
Orbit determination engine for performance testing.
- OrbitDeterminationEngine(boolean) - Constructor for class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Constructor.
- OrbitDeterminationObserver - Class in org.orekit.tutorials.estimation.common
-
Observer for the OrbitDetermination scheme.
- OrbitDeterminationObserver(Orbit, PrintStream) - Constructor for class org.orekit.tutorials.estimation.common.OrbitDeterminationObserver
-
Constructor.
- OrekitBuilder - Class in org.orekit.tutorials.utils
-
Utility class for building Orekit objects from parsed YAML files.
- org.orekit.tutorials - package org.orekit.tutorials
- org.orekit.tutorials.attitude - package org.orekit.tutorials.attitude
- org.orekit.tutorials.bodies - package org.orekit.tutorials.bodies
- org.orekit.tutorials.conversion - package org.orekit.tutorials.conversion
- org.orekit.tutorials.data - package org.orekit.tutorials.data
- org.orekit.tutorials.estimation - package org.orekit.tutorials.estimation
- org.orekit.tutorials.estimation.common - package org.orekit.tutorials.estimation.common
- org.orekit.tutorials.estimation.performance - package org.orekit.tutorials.estimation.performance
-
This package provides elements for testing performance of Orekit Orbit Determination features.
- org.orekit.tutorials.frames - package org.orekit.tutorials.frames
- org.orekit.tutorials.gnss - package org.orekit.tutorials.gnss
- org.orekit.tutorials.maneuvers - package org.orekit.tutorials.maneuvers
- org.orekit.tutorials.models - package org.orekit.tutorials.models
- org.orekit.tutorials.propagation - package org.orekit.tutorials.propagation
- org.orekit.tutorials.propagation.cr3bp - package org.orekit.tutorials.propagation.cr3bp
- org.orekit.tutorials.time - package org.orekit.tutorials.time
- org.orekit.tutorials.utils - package org.orekit.tutorials.utils
- org.orekit.tutorials.yaml - package org.orekit.tutorials.yaml
-
This package provides classes to read the data contained inside a YAML file.
P
- parseInput(String, InputStream) - Method in class org.orekit.tutorials.KeyValueFileParser
-
Parse an input file.
- parseOPM(double, double, File) - Static method in class org.orekit.tutorials.utils.NdmUtils
-
Parses an OPM to a file.
- PerformanceTesting - Class in org.orekit.tutorials.estimation.performance
-
Main class for Orbit Determination performance testing.
- PerformanceTesting.TutorialPerformanceTesting - Class in org.orekit.tutorials.estimation.performance
-
Input data for orbit determination performance testing.
- Phasing - Class in org.orekit.tutorials.bodies
-
Orekit tutorial for setting up a Sun-synchronous Earth-phased Low Earth Orbit.
- Phasing() - Constructor for class org.orekit.tutorials.bodies.Phasing
-
Simple constructor.
- Phasing.TutorialGrid - Class in org.orekit.tutorials.bodies
-
Input data for the grid parameter.
- Phasing.TutorialPhasing - Class in org.orekit.tutorials.bodies
-
Input data for the Phasing tutorial.
- printCovarianceMatrix() - Method in class org.orekit.tutorials.estimation.ExtendedSemianalyticalKalmanFilter.Observer
-
Print the physical estimated covariance matrix.
- printXStatistics() - Method in class org.orekit.tutorials.estimation.ExtendedSemianalyticalKalmanFilter.Observer
-
Print the statistics on the X coordinate residuals.
- printYStatistics() - Method in class org.orekit.tutorials.estimation.ExtendedSemianalyticalKalmanFilter.Observer
-
Print the statistics on the Y coordinate residuals.
- printZStatistics() - Method in class org.orekit.tutorials.estimation.ExtendedSemianalyticalKalmanFilter.Observer
-
Print the statistics on the Z coordinate residuals.
- PropagationInCR3BP - Class in org.orekit.tutorials.propagation.cr3bp
-
Simple tutorial giving an example of propagation in the Circular Restricted 3 Body problem with Orekit.
- PropagationInNonInertialFrame - Class in org.orekit.tutorials.propagation
-
The goal of this tutorial is to introduce users to orbital integration using SingleBodyAttraction.
- PropagationInRotatingFrame - Class in org.orekit.tutorials.propagation
-
Compared propagation of a LEO in Earth-centered inertial and non-inertial frames: EME2000 and ITRF.
- PropagatorConversion - Class in org.orekit.tutorials.conversion
-
Orekit tutorial for propagator conversion.
R
- removePermanentDeformation() - Method in class org.orekit.tutorials.yaml.TutorialStationDisplacement
-
Get the flag for permanent deformation.
- RinexObservationFile - Class in org.orekit.tutorials.gnss
-
Orekit tutorial for the reading of Rinex observation file.
- run(File) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Run the program.
- run(File) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Run the program.
- run(File) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator
-
Run the program.
- run(SpacecraftState, double) - Method in class org.orekit.tutorials.maneuvers.StationKeeping
-
Run the SK simulation for a single cycle.
- runKalman(File) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Run the program.
- runKalman(File) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Run the program.
- runOrbitDetermination(File) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Run the orbit determination.
- runReference(File, Vector3D, Vector3D, ParameterDriversList, AbsoluteDate) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Use the physical models in the input file.
- runReference(File, Vector3D, Vector3D, ParameterDriversList, AbsoluteDate) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Use the physical models in the input file.
S
- SequentialBatchLeastSquares - Class in org.orekit.tutorials.estimation
-
The purpose of the tutorial is to presents the Sequential-Batch Least Squares estimation.
- SequentialBatchLeastSquares() - Constructor for class org.orekit.tutorials.estimation.SequentialBatchLeastSquares
- SequentialBatchLeastSquares.TutorialSequentialBatch - Class in org.orekit.tutorials.estimation
-
Input data for the sequential-batch orbit determination tutorial.
- setA(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Set the semi major axis.
- setA(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Set the semi major axis.
- setA(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Set the semi major axis.
- setAlphaV(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Set the true latitude argument.
- setAngularOffset(double) - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Set the angular offset.
- setAntennaOffset(double[]) - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Set the coordinates of the on-board antenna phase center in spacecraft frame.
- setArea(double) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialDrag
-
Set the cross section.
- setArea(double) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialSolarRadiationPressure
-
Set the cross section.
- setAscending(boolean) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialGrid
-
Set the indicator for latitude crossing direction.
- setAttitudeMode(String) - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Set the name of the attitude mode.
- setAttitudeProvider(DSSTPropagatorBuilder, AttitudeProvider) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set attitude provider.
- setAttitudeProvider(NumericalPropagatorBuilder, AttitudeProvider) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set attitude provider.
- setAttitudeProvider(NumericalPropagatorBuilder, AttitudeProvider) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set attitude provider.
- setAttitudeProvider(NumericalPropagatorBuilder, AttitudeProvider) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set attitude provider.
- setAttitudeProvider(NumericalPropagatorBuilder, AttitudeProvider) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set attitude provider.
- setAttitudeProvider(NumericalPropagatorBuilder, AttitudeProvider) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set attitude provider.
- setAttitudeProvider(TLEPropagatorBuilder, AttitudeProvider) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set attitude provider.
- setAttitudeProvider(T, AttitudeProvider) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set attitude provider.
- setAttitudeProvider(T, AttitudeProvider) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set attitude provider.
- setAzEl(TutorialMeasurements.TutorialAzEl) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the azimuth/elevation measurement data.
- setAzElBias(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Set the estimated azimuth/elevation measurement bias.
- setBias(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Set the estimated On-board range bias.
- setBody(TutorialBody) - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Set the body data.
- setBody(TutorialBody) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Set the body data.
- setBody(TutorialBody) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the body data.
- setCartesian(TutorialOrbitType.TutorialCartesianOrbit) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Set the cartesian elements.
- setCartesianOrbitalP(double[]) - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Set the initial diagonal elements of the cartesian covariance matrix.
- setCartesianOrbitalQ(double[]) - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Set the initial diagonal elements of the cartesian process noise matrix.
- setCd(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialDrag
-
Set the estimated drag coefficient.
- setCircular(TutorialOrbitType.TutorialCircularOrbit) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Set the circular elements.
- setClockOffset(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Set the estimated On-board clock offset.
- setClockOffset(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialStation.TutorialObservationType
-
Set the estimated clock offset.
- setCoefficients(double[]) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Set the array of acceleration coefficients.
- setConvergenceThreshold(double) - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Set the convergence threshold.
- setCoordinates(double[]) - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Set the array containing the station coordinates.
- setCorrectionDate(String) - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Set the medium date used to initialize the time span tropospheric model.
- setCr(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialSolarRadiationPressure
-
Set the estimated reflection coefficient.
- setCycleDuration(double) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the SK cycle duration.
- setCyclesNumber(int) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the number of SK cycles to simulate.
- setDate(String) - Method in class org.orekit.tutorials.yaml.TutorialOrbit
-
Set the String representation of the orbit date.
- setDegree(int) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialGravity
-
Set the maximal degree.
- setDegree(int) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialOceanTides
-
Set the maximal degree.
- setDeltaVMax(double) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the DV max.
- setDirection(double[]) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Set the thust direction.
- setDirections(double[]) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Set the acceleration direction in defining frame.
- setDrag(DSSTPropagatorBuilder, Atmosphere, DragSensitive) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set drag force model.
- setDrag(NumericalPropagatorBuilder, Atmosphere, DragSensitive) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set drag force model.
- setDrag(NumericalPropagatorBuilder, Atmosphere, DragSensitive) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set drag force model.
- setDrag(NumericalPropagatorBuilder, Atmosphere, DragSensitive) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set drag force model.
- setDrag(NumericalPropagatorBuilder, Atmosphere, DragSensitive) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set drag force model.
- setDrag(NumericalPropagatorBuilder, Atmosphere, DragSensitive) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set drag force model.
- setDrag(TLEPropagatorBuilder, Atmosphere, DragSensitive) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set drag force model.
- setDrag(TutorialForceModel.TutorialDrag) - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Set the drag force model.
- setDrag(T, Atmosphere, DragSensitive) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set drag force model.
- setDrag(T, Atmosphere, DragSensitive) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set drag force model.
- setDuration(double) - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Set the simulation duration.
- setDuration(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Set the estimated duration.
- setDurationInDays(double) - Method in class org.orekit.tutorials.estimation.SequentialBatchLeastSquares.TutorialSequentialBatch
-
Set the simulation duration.
- setDurationInDays(double) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the simulation duration.
- setE(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Set the orbit eccentricity.
- setEasternBoundary(double) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the eastern boundary for longitude window.
- setEndDate(String) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Set the end date for measurement generation.
- setEquatorialRadius(double) - Method in class org.orekit.tutorials.yaml.TutorialBody
-
Set the equatorial radius of the body.
- setEquinoctial(TutorialOrbitType.TutorialEquinoctialOrbit) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Set the equinoctial elements.
- setEstimator(TutorialBatchLSEstimator) - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Set the batch least square estimator data.
- setEx(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Set the first component of the equinoctial eccentricity vector.
- setEx(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Set the first component of the equinoctial eccentricity vector.
- setEy(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Set the second component of the equinoctial eccentricity vector.
- setEy(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Set the second component of the equinoctial eccentricity vector.
- setFixedNumberOfInterpolationPoints(int) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the interpolation grid specification.
- setFixedStep(double) - Method in class org.orekit.tutorials.yaml.TutorialIntegrator
-
Set the fixed step size.
- setFlowRate(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Set the estimated flow rate.
- setForceModels(TutorialForceModel) - Method in class org.orekit.tutorials.yaml.TutorialPropagator
-
Set the force model data.
- setFrameName(String) - Method in class org.orekit.tutorials.yaml.TutorialBody
-
Set the name of the body frame related to body shape.
- setFrameName(String) - Method in class org.orekit.tutorials.yaml.TutorialOrbit
-
Set the name of the inertial orbit frame.
- setGaussNewton(TutorialOptimizationEngine.TutorialGaussNewton) - Method in class org.orekit.tutorials.yaml.TutorialOptimizationEngine
-
Set the Gauss-Newton optimization engine.
- setGenerateMeasurements(boolean) - Method in class org.orekit.tutorials.estimation.performance.PerformanceTesting.TutorialPerformanceTesting
-
Set the flag for measurements generation.
- setGravity(DSSTPropagatorBuilder, OneAxisEllipsoid) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set gravity force model.
- setGravity(NumericalPropagatorBuilder, OneAxisEllipsoid) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set gravity force model.
- setGravity(NumericalPropagatorBuilder, OneAxisEllipsoid) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set gravity force model.
- setGravity(NumericalPropagatorBuilder, OneAxisEllipsoid) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set gravity force model.
- setGravity(NumericalPropagatorBuilder, OneAxisEllipsoid) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set gravity force model.
- setGravity(NumericalPropagatorBuilder, OneAxisEllipsoid) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set gravity force model.
- setGravity(TLEPropagatorBuilder, OneAxisEllipsoid) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set gravity force model.
- setGravity(TutorialForceModel.TutorialGravity) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the gravity data.
- setGravity(TutorialForceModel.TutorialGravity) - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Set the central body gravity force model.
- setGravity(T, OneAxisEllipsoid) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set gravity force model.
- setGravity(T, OneAxisEllipsoid) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set gravity force model.
- setGrids(List<Phasing.TutorialGrid>) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the list of grid data.
- setHx(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Set the first component of the inclination vector.
- setHy(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Set the second component of the inclination vector.
- setI(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Set the orbit inclination.
- setI(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Set the orbit inclination.
- setId(String) - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Set the satellite ID.
- setIersConventionYear(int) - Method in class org.orekit.tutorials.yaml.TutorialBody
-
Set the year of the IERS Convention (1996, 2003 or 2010).
- setInitialMass(double) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the initial mass of the spacecraft.
- setInitialOrbitIsOsculating(boolean) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the flag for initial orbit type.
- setInitialStep(double) - Method in class org.orekit.tutorials.yaml.TutorialOptimizationEngine.TutorialLevenbergMarquardt
-
Set the optimizer's initial step.
- setIntegrator(TutorialIntegrator) - Method in class org.orekit.tutorials.yaml.TutorialPropagator
-
Set the numerical integrator used by the orbit propagator.
- setInverseFlattening(double) - Method in class org.orekit.tutorials.yaml.TutorialBody
-
Set the inverse flattening of the body.
- setIonosphere(TutorialIonosphere) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the ionospheric model.
- setIonosphericLayer(double) - Method in class org.orekit.tutorials.yaml.TutorialIonosphere
-
Set the height of the ionospheric layer.
- setIsAnalytical(boolean) - Method in class org.orekit.tutorials.yaml.TutorialPropagator
-
Set the flag for the propagator type.
- setIsEstimated(boolean) - Method in class org.orekit.tutorials.yaml.TutorialEstimatedDateParameter
-
Set the flag for the date parameter estimation.
- setIsEstimated(boolean) - Method in class org.orekit.tutorials.yaml.TutorialEstimatedParameter
-
Set the flag for the parameter estimation.
- setIsEstimated(boolean) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Set the flag for acceleration coefficients estimation.
- setIsEstimatedModel(boolean) - Method in class org.orekit.tutorials.yaml.TutorialIonosphere
-
Set the flag to know if the ionospheric model is estimated of not.
- setIsEstimatedModel(boolean) - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Set the flag to know if tropospheric model is estimated of not.
- setIsKalman(boolean) - Method in class org.orekit.tutorials.estimation.performance.PerformanceTesting.TutorialPerformanceTesting
-
Set the flag for orbit determination engine.
- setIsOpmGenerated(boolean) - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Set the flag for the estimated OPM generation.
- setIsp(double) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the ISP.
- setIsp(double) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Set the Isp.
- setIsUsed(boolean) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialRelativity
-
Set the flag to use the relativity force model.
- setKalman(TutorialKalman) - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Set the kalman filter data.
- setKeplerian(TutorialOrbitType.TutorialKeplerianOrbit) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Set the keplerian elements.
- setLatitude(double) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialGrid
-
Set the point latitude.
- setLevenbergMarquardt(TutorialOptimizationEngine.TutorialLevenbergMarquardt) - Method in class org.orekit.tutorials.yaml.TutorialOptimizationEngine
-
Set the Levenberg-Marquardt optimization engine.
- setLine1(String) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialTLE
-
Set the TLE first line.
- setLine2(String) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialTLE
-
Set the TLE second line.
- setLv(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Set the mean anomaly.
- setManeuver(DSSTPropagatorBuilder, AbsoluteDate, double, double, double, Vector3D, String) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
- setManeuver(NumericalPropagatorBuilder, AbsoluteDate, double, double, double, Vector3D, String) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
- setManeuver(NumericalPropagatorBuilder, AbsoluteDate, double, double, double, Vector3D, String) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
- setManeuver(NumericalPropagatorBuilder, AbsoluteDate, double, double, double, Vector3D, String) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
- setManeuver(NumericalPropagatorBuilder, AbsoluteDate, double, double, double, Vector3D, String) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set maneuver model.
- setManeuver(TLEPropagatorBuilder, AbsoluteDate, double, double, double, Vector3D, String) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
- setManeuver(T, AbsoluteDate, double, double, double, Vector3D, String) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set maneuver model.
- setManeuvers(List<TutorialForceModel.TutorialManeuver>) - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Set the list of maneuvers.
- setMappingFunction(String) - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Set the name of the tropospheric mapping function.
- setMass(double) - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Set the spacecraft mass.
- setMass(DSSTPropagatorBuilder, double) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set satellite mass.
- setMass(NumericalPropagatorBuilder, double) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set satellite mass.
- setMass(NumericalPropagatorBuilder, double) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set satellite mass.
- setMass(NumericalPropagatorBuilder, double) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set satellite mass.
- setMass(NumericalPropagatorBuilder, double) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set satellite mass.
- setMass(NumericalPropagatorBuilder, double) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set satellite mass.
- setMass(TLEPropagatorBuilder, double) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set satellite mass.
- setMass(T, double) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set satellite mass.
- setMass(T, double) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set satellite mass.
- setMaxEvaluations(int) - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Set the maximum number of evaluations before an exception is thrown.
- setMaxIterations(int) - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Set the maximum number of iterations before an exception is thrown.
- setMaxMDaily(int) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the maximum order of m-daily terms for eccentricity fitting.
- setMaxStep(double) - Method in class org.orekit.tutorials.yaml.TutorialIntegrator
-
Set the maximum step size.
- setMaxTimeGapBetweenInterpolationPoints(double) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the interpolation grid specification.
- setMeanSolarTime(String) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the string representation of the mean solar time.
- setMeasurementFiles(List<String>) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the list of measurement files.
- setMeasurementGenerationInputFile(String) - Method in class org.orekit.tutorials.estimation.performance.PerformanceTesting.TutorialPerformanceTesting
-
Set the name of the input YAML file for measurement generation.
- setMeasurementP(double[]) - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Set the initial diagonal elements of the measurement covariance matrix.
- setMeasurementQ(double[]) - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Set the initial diagonal elements of the measurement process noise matrix.
- setMeasurements(TutorialMeasurements) - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Set the measurement data.
- setMeasurements(TutorialMeasurements) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Set the measurement data.
- setMedianDate(TutorialEstimatedDateParameter) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Set the estimated median date.
- setMinElevation(double) - Method in class org.orekit.tutorials.propagation.VisibilityCircle.TutorialVisibilityCircle
-
Set the minimum elevation for defining visibility above ground.
- setMinStep(double) - Method in class org.orekit.tutorials.yaml.TutorialIntegrator
-
Set the minimum step size.
- setName(String) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Set the name.
- setName(String) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Set the prefix to use for parameter drivers.
- setName(String) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialThirdBody
-
Set the name of the celestial body.
- setName(String) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Set the name of the orbit type.
- setName(String) - Method in class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Set the satellite name.
- setName(String) - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Set the station name.
- setName(String) - Method in class org.orekit.tutorials.yaml.TutorialStation.TutorialObservationType
-
Set the name of the observation type.
- setNbMaxManeuvers(int) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the max number of maneuvers per cycle.
- setNumericalComparison(boolean) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the flag for the comparison with the numerical orbit propagator.
- setObjectId(String) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the id of the object.
- setObjectName(String) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the name of the object.
- setObservationTypes(List<TutorialStation.TutorialObservationType>) - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Set the list of observation types.
- setOceanTides(DSSTPropagatorBuilder, IERSConventions, OneAxisEllipsoid, int, int) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set third body attraction force model.
- setOceanTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, int, int) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set third body attraction force model.
- setOceanTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, int, int) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set third body attraction force model.
- setOceanTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, int, int) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set third body attraction force model.
- setOceanTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, int, int) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set third body attraction force model.
- setOceanTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, int, int) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set third body attraction force model.
- setOceanTides(TLEPropagatorBuilder, IERSConventions, OneAxisEllipsoid, int, int) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set third body attraction force model.
- setOceanTides(TutorialForceModel.TutorialOceanTides) - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Set the ocean tides force model.
- setOceanTides(T, IERSConventions, OneAxisEllipsoid, int, int) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set third body attraction force model.
- setOceanTides(T, IERSConventions, OneAxisEllipsoid, int, int) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set third body attraction force model.
- setOemDuration(double) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the OEM duration.
- setOemStep(double) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the OEM step size.
- setOptimizationEngine(TutorialOptimizationEngine) - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Set the optimization engine.
- setOrbit(TutorialOrbit) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the orbit data.
- setOrbit(TutorialOrbit) - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Set the orbit data.
- setOrbit(TutorialOrbit) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Set the orbit data.
- setOrbit(TutorialOrbit) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the orbit data.
- setOrbit(TutorialOrbit) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the orbit data.
- setOrbit(TutorialOrbit) - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Set the orbit data (circular orbit).
- setOrbitalParametersPositionScale(double) - Method in class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
-
Set the scaling factor for orbital parameters normalization.
- setOrbitDetermination(TutorialOrbitDetermination) - Method in class org.orekit.tutorials.estimation.SequentialBatchLeastSquares.TutorialSequentialBatch
-
Set the orbit determination data.
- setOrbitDeterminationInputFile(String) - Method in class org.orekit.tutorials.estimation.performance.PerformanceTesting.TutorialPerformanceTesting
-
Set the name of the input YAML file for orbit determination.
- setOrbitsSeparation(int) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the number of orbits between maneuvers.
- setOrbitType(TutorialOrbitType) - Method in class org.orekit.tutorials.yaml.TutorialOrbit
-
Set the orbit type (name and orbital elements).
- setOrder(int) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialGravity
-
Set the maximal order.
- setOrder(int) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialOceanTides
-
Set the maximal order.
- setOutlierRejectionMultiplier(int) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the detection limit for outliers.
- setOutlierRejectionStartingIteration(int) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the number of iterations before with filter is not applied.
- setOutputBaseName(String) - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Set the base name of the output files (log and residuals).
- setOutputBaseName(String) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Set the name of the output measurement file.
- setOutputOrbitIsOsculating(boolean) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the flag for output orbit type.
- setOutputShortPeriodCoefficients(List<String>) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the list of short period coefficients to output.
- setOutputStep(double) - Method in class org.orekit.tutorials.estimation.SequentialBatchLeastSquares.TutorialSequentialBatch
-
Set the time step for OEM generation.
- setOutputStep(double) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the time step between printed elements.
- setOutputStep(double) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the time step between printed elements.
- setPa(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Set the perigee argument.
- setPhase(TutorialMeasurements.TutorialPhase) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the phase measurement data.
- setPhaseBias(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Set the estimated phase measurement bias.
- setPhasingDaysNumer(int) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the number of days in the phasing cycle.
- setPhasingOrbitsNumber(int) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the number of orbits in the phasing cycle.
- setPointsNumber(int) - Method in class org.orekit.tutorials.propagation.VisibilityCircle.TutorialVisibilityCircle
-
Set the number of points to compute.
- setPolynomialAcceleration(List<TutorialForceModel.TutorialPolynomialAcceleration>) - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Set the list of polynomial acceleration force models.
- setPolynomialAcceleration(DSSTPropagatorBuilder, String, Vector3D, int) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set polynomial acceleration force model.
- setPolynomialAcceleration(NumericalPropagatorBuilder, String, Vector3D, int) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set polynomial acceleration force model.
- setPolynomialAcceleration(NumericalPropagatorBuilder, String, Vector3D, int) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set polynomial acceleration force model.
- setPolynomialAcceleration(NumericalPropagatorBuilder, String, Vector3D, int) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set polynomial acceleration force model.
- setPolynomialAcceleration(NumericalPropagatorBuilder, String, Vector3D, int) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set polynomial acceleration force model.
- setPolynomialAcceleration(NumericalPropagatorBuilder, String, Vector3D, int) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set polynomial acceleration force model.
- setPolynomialAcceleration(TLEPropagatorBuilder, String, Vector3D, int) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set polynomial acceleration force model.
- setPolynomialAcceleration(T, String, Vector3D, int) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set polynomial acceleration force model.
- setPolynomialAcceleration(T, String, Vector3D, int) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set polynomial acceleration force model.
- setPosition(TutorialMeasurements.TutorialPosition) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the position only measurement data.
- setPositionAngle(String) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Set the name of the position angle.
- setPositionAngle(String) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
-
Set the name of the position angle.
- setPositionAngle(String) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Set the name of the position angle.
- setPositionError(double) - Method in class org.orekit.tutorials.yaml.TutorialIntegrator
-
Set the position error.
- setPrintToFile(boolean) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the flag for printing results to a file.
- setPropagationP(double[]) - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Set the initial diagonal elements of the propagation covariance matrix.
- setPropagationQ(double[]) - Method in class org.orekit.tutorials.yaml.TutorialKalman
-
Set the initial diagonal elements of the propagation process noise matrix.
- setPropagator(TutorialPropagator) - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Set the propagator data.
- setPropagator(TutorialPropagator) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Set the propagator data.
- setPropagator(TutorialPropagator) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the orbit propagator data.
- setPv(TutorialMeasurements.TutorialPV) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the position/velocity measurement data.
- setPvBias(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Set the estimated position/velocity measurement bias.
- setRaan(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
-
Set the right ascension of the ascending node.
- setRaan(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Set the right ascension of the ascending node.
- setRange(TutorialMeasurements.TutorialRange) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the range measurement data.
- setRangeBias(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Set the estimated range measurement bias.
- setRangeRate(TutorialMeasurements.TutorialRangeRate) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the range rate measurement data.
- setRangeRateBias(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialStation
-
Set the estimated range rate measurement bias.
- setReferenceAscending(boolean) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the reference indicator for latitude crossing direction.
- setReferenceLatitude(double) - Method in class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
-
Set the reference latitude for Sun synchronous orbit.
- setRelativity(DSSTPropagatorBuilder) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set relativity force model.
- setRelativity(NumericalPropagatorBuilder) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set relativity force model.
- setRelativity(NumericalPropagatorBuilder) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set relativity force model.
- setRelativity(NumericalPropagatorBuilder) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set relativity force model.
- setRelativity(NumericalPropagatorBuilder) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set relativity force model.
- setRelativity(NumericalPropagatorBuilder) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set relativity force model.
- setRelativity(TLEPropagatorBuilder) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set relativity force model.
- setRelativity(TutorialForceModel.TutorialRelativity) - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Set the relativity force model.
- setRelativity(T) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set relativity force model.
- setRelativity(T) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set relativity force model.
- setRemovePermanentDeformation(boolean) - Method in class org.orekit.tutorials.yaml.TutorialStationDisplacement
-
Set the flag for permanent deformation.
- setSigma(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialAzEl
-
Set the theoretical standard deviation of the measurement.
- setSigma(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPhase
-
Set the theoretical standard deviation of the measurement.
- setSigma(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRange
-
Set the theoretical standard deviation of the measurement.
- setSigma(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRangeRate
-
Set the theoretical standard deviation of the measurement.
- setSigmaPos(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPosition
-
Set the theoretical standard deviation for position data.
- setSigmaPos(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPV
-
Set the theoretical standard deviation for position data.
- setSigmaVel(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPV
-
Set the theoretical standard deviation for velocity data.
- setSinex(TutorialSinex) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the sinex files containing station positions and eccentricities.
- setSolarRadiationPressure(DSSTPropagatorBuilder, CelestialBody, OneAxisEllipsoid, RadiationSensitive) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set solar radiation pressure force model.
- setSolarRadiationPressure(NumericalPropagatorBuilder, CelestialBody, OneAxisEllipsoid, RadiationSensitive) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set solar radiation pressure force model.
- setSolarRadiationPressure(NumericalPropagatorBuilder, CelestialBody, OneAxisEllipsoid, RadiationSensitive) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set solar radiation pressure force model.
- setSolarRadiationPressure(NumericalPropagatorBuilder, CelestialBody, OneAxisEllipsoid, RadiationSensitive) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set solar radiation pressure force model.
- setSolarRadiationPressure(NumericalPropagatorBuilder, CelestialBody, OneAxisEllipsoid, RadiationSensitive) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set solar radiation pressure force model.
- setSolarRadiationPressure(NumericalPropagatorBuilder, CelestialBody, OneAxisEllipsoid, RadiationSensitive) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set solar radiation pressure force model.
- setSolarRadiationPressure(TLEPropagatorBuilder, CelestialBody, OneAxisEllipsoid, RadiationSensitive) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set solar radiation pressure force model.
- setSolarRadiationPressure(TutorialForceModel.TutorialSolarRadiationPressure) - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Set the solar radiation pressure force model.
- setSolarRadiationPressure(T, CelestialBody, OneAxisEllipsoid, RadiationSensitive) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set solar radiation pressure force model.
- setSolarRadiationPressure(T, CelestialBody, OneAxisEllipsoid, RadiationSensitive) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set solar radiation pressure force model.
- setSolidTides(DSSTPropagatorBuilder, IERSConventions, OneAxisEllipsoid, CelestialBody[]) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set third body attraction force model.
- setSolidTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, CelestialBody[]) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set third body attraction force model.
- setSolidTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, CelestialBody[]) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set third body attraction force model.
- setSolidTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, CelestialBody[]) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set third body attraction force model.
- setSolidTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, CelestialBody[]) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set third body attraction force model.
- setSolidTides(NumericalPropagatorBuilder, IERSConventions, OneAxisEllipsoid, CelestialBody[]) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set third body attraction force model.
- setSolidTides(TLEPropagatorBuilder, IERSConventions, OneAxisEllipsoid, CelestialBody[]) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set third body attraction force model.
- setSolidTides(T, IERSConventions, OneAxisEllipsoid, CelestialBody[]) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set third body attraction force model.
- setSolidTides(T, IERSConventions, OneAxisEllipsoid, CelestialBody[]) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set third body attraction force model.
- setSpacecraft(TutorialSpacecraft) - Method in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Set the spacecraft data.
- setSpacecraft(TutorialSpacecraft) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Set the spacecraft data.
- setSpacecraft(TutorialSpacecraft) - Method in class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
-
Set the spacecraft data.
- setSpacecraftAltitude(double) - Method in class org.orekit.tutorials.propagation.VisibilityCircle.TutorialVisibilityCircle
-
Set the satellite altitude.
- setStartDate(String) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Set the start date for measurement generation.
- setStartDate(String) - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Set the simulation start date.
- setStartDate(TutorialEstimatedDateParameter) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Set the estimated start date.
- setStation(TutorialStation) - Method in class org.orekit.tutorials.propagation.VisibilityCircle.TutorialVisibilityCircle
-
Set the ground station.
- setStationDisplacement(TutorialStationDisplacement) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the station displacement data.
- setStationEccentricities(String) - Method in class org.orekit.tutorials.yaml.TutorialSinex
-
Set the path for sinex station eccentricities file.
- setStationPositions(String) - Method in class org.orekit.tutorials.yaml.TutorialSinex
-
Set the path for sinex station positions file.
- setStations(List<TutorialStation>) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the list of used stations.
- setStep(double) - Method in class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
-
Set the step for the measurement generation.
- setStep(double) - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Set the time step between each points.
- setStopDate(TutorialEstimatedDateParameter) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Set the estimated stop date.
- setThirdBody(List<TutorialForceModel.TutorialThirdBody>) - Method in class org.orekit.tutorials.yaml.TutorialForceModel
-
Set the list of third body attraction force models.
- setThirdBody(DSSTPropagatorBuilder, CelestialBody) - Method in class org.orekit.tutorials.estimation.DSSTOrbitDetermination
-
Set third body attraction force model.
- setThirdBody(NumericalPropagatorBuilder, CelestialBody) - Method in class org.orekit.tutorials.estimation.GNSSOrbitDetermination
-
Set third body attraction force model.
- setThirdBody(NumericalPropagatorBuilder, CelestialBody) - Method in class org.orekit.tutorials.estimation.KalmanNumericalOrbitDetermination
-
Set third body attraction force model.
- setThirdBody(NumericalPropagatorBuilder, CelestialBody) - Method in class org.orekit.tutorials.estimation.LaserRangingOrbitDetermination
-
Set third body attraction force model.
- setThirdBody(NumericalPropagatorBuilder, CelestialBody) - Method in class org.orekit.tutorials.estimation.NumericalOrbitDetermination
-
Set third body attraction force model.
- setThirdBody(NumericalPropagatorBuilder, CelestialBody) - Method in class org.orekit.tutorials.estimation.performance.OrbitDeterminationEngine
-
Set third body attraction force model.
- setThirdBody(TLEPropagatorBuilder, CelestialBody) - Method in class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
-
Set third body attraction force model.
- setThirdBody(T, CelestialBody) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDetermination
-
Set third body attraction force model.
- setThirdBody(T, CelestialBody) - Method in class org.orekit.tutorials.estimation.common.AbstractOrbitDeterminationEngine
-
Set third body attraction force model.
- setThrust(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
-
Set the estimated thrust.
- setTle(TutorialOrbitType.TutorialTLE) - Method in class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
-
Set the TLE data.
- setTle(TutorialOrbitType.TutorialTLE) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType
-
Set the TLE data.
- setTroposphere(TutorialTroposphere) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the tropospheric model.
- setV(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
-
Set the true anomaly.
- setValues(double[]) - Method in class org.orekit.tutorials.yaml.TutorialEstimatedParameter
-
Set the initial, minimum and maximum value of the parameter.
- setValues(String[]) - Method in class org.orekit.tutorials.yaml.TutorialEstimatedDateParameter
-
Set the initial, minimum and maximum dates for the parameter.
- setVtec(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialIonosphere
-
Set the estimated ionospheric parameter.
- setVx(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Set the first coordinate of the satellite velocity.
- setVy(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Set the second coordinate of the satellite velocity.
- setVz(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Set the third coordinate of the satellite velocity.
- setWeight(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialAzEl
-
Set the measurement base weight.
- setWeight(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPhase
-
Set the measurement base weight.
- setWeight(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPosition
-
Set the measurement base weight.
- setWeight(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPV
-
Set the measurement base weight.
- setWeight(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRange
-
Set the measurement base weight.
- setWeight(double) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRangeRate
-
Set the measurement base weight.
- setWesternBoundary(double) - Method in class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
-
Set the western boundary for longitude window.
- setWithOceanLoadingCorrection(boolean) - Method in class org.orekit.tutorials.yaml.TutorialStationDisplacement
-
Set the flag for the computation of ocean loading correction.
- setWithRefractionCorrection(boolean) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialAzEl
-
Set the flag for the computation of the refraction correction.
- setWithShapiro(boolean) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the flag for the computation of the Shapiro effect.
- setWithSolidTides(boolean) - Method in class org.orekit.tutorials.yaml.TutorialForceModel.TutorialThirdBody
-
Set the flag for the computation of the body's solid tides.
- setWithStationPositionEstimated(boolean) - Method in class org.orekit.tutorials.yaml.TutorialMeasurements
-
Set the flag for station position estimation.
- setWithTidalCorrection(boolean) - Method in class org.orekit.tutorials.yaml.TutorialStationDisplacement
-
Set the flag for the computation of the tidal displacement.
- setWithWeatherModel(boolean) - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Set the flag to know if an empirical model is used to compute station Temperature and Pressure.
- setX(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Set the first coordinate of position vector.
- setY(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Set the second coordinate of position vector.
- setZ(double) - Method in class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
-
Set the third coordinate of the satellite position.
- setZenithDelay(TutorialEstimatedParameter) - Method in class org.orekit.tutorials.yaml.TutorialTroposphere
-
Set the estimated troposheric parameter.
- signedAmplitude(FieldSpacecraftState<T>, T[]) - Method in class org.orekit.tutorials.estimation.common.CustomHarmonicAccelerationModel
- signedAmplitude(SpacecraftState, double[]) - Method in class org.orekit.tutorials.estimation.common.CustomHarmonicAccelerationModel
- StationKeeping - Class in org.orekit.tutorials.maneuvers
-
This tutorial shows the use of the FieldDSSTPropagator to calculate an East/West station-keeping strategy in GEO.
- StationKeeping(double, double, double, double, int, int) - Constructor for class org.orekit.tutorials.maneuvers.StationKeeping
-
Constructor.
- StationKeeping.TutorialStationKeeping - Class in org.orekit.tutorials.maneuvers
-
Input data for this station-keeping tutorial.
- SunEarthMultipleShooter - Class in org.orekit.tutorials.propagation.cr3bp
-
Correction of a trajectory using multiple shooting method.
T
- TidalDisplacements - Class in org.orekit.tutorials.models
-
Orekit tutorial for computing stations tidal displacements.
- Time1 - Class in org.orekit.tutorials.time
-
Orekit tutorial for dates support.
- TLEBasedOrbitDetermination - Class in org.orekit.tutorials.estimation
-
The purpose of the tutorial is to present a TLE based orbit determination.
- TLEBasedOrbitDetermination() - Constructor for class org.orekit.tutorials.estimation.TLEBasedOrbitDetermination
- TLEConversion - Class in org.orekit.tutorials.conversion
-
Orekit tutorial for TLE conversion.
- TrackCorridor - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for track corridor display.
- TrackCorridor.TutorialTrackCorridor - Class in org.orekit.tutorials.propagation
-
Input data for the TrackCorridor tutorial.
- TutorialAzEl() - Constructor for class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialAzEl
- TutorialBatchLSEstimator - Class in org.orekit.tutorials.yaml
-
Initial data for the batch least squares orbit determination estimator.
- TutorialBatchLSEstimator() - Constructor for class org.orekit.tutorials.yaml.TutorialBatchLSEstimator
- TutorialBody - Class in org.orekit.tutorials.yaml
-
Initial data for the central body.
- TutorialBody() - Constructor for class org.orekit.tutorials.yaml.TutorialBody
- TutorialCartesianOrbit() - Constructor for class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCartesianOrbit
- TutorialCircularOrbit() - Constructor for class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialCircularOrbit
- TutorialDrag() - Constructor for class org.orekit.tutorials.yaml.TutorialForceModel.TutorialDrag
- TutorialDSSTPropagation() - Constructor for class org.orekit.tutorials.propagation.DSSTPropagation.TutorialDSSTPropagation
- TutorialEquinoctialOrbit() - Constructor for class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialEquinoctialOrbit
- TutorialEstimatedDateParameter - Class in org.orekit.tutorials.yaml
-
Utility class for estimated date parameters during a maneuver estimation process.
- TutorialEstimatedDateParameter() - Constructor for class org.orekit.tutorials.yaml.TutorialEstimatedDateParameter
-
Constructor.
- TutorialEstimatedParameter - Class in org.orekit.tutorials.yaml
-
Utility class for estimated parameters during an orbit determination process.
- TutorialEstimatedParameter() - Constructor for class org.orekit.tutorials.yaml.TutorialEstimatedParameter
-
Constructor.
- TutorialForceModel - Class in org.orekit.tutorials.yaml
-
Initial data to initialize the main Orekit force models.
- TutorialForceModel() - Constructor for class org.orekit.tutorials.yaml.TutorialForceModel
- TutorialForceModel.TutorialDrag - Class in org.orekit.tutorials.yaml
-
Atmospheric drag.
- TutorialForceModel.TutorialGravity - Class in org.orekit.tutorials.yaml
-
Central body gravity.
- TutorialForceModel.TutorialManeuver - Class in org.orekit.tutorials.yaml
-
Maneuver.
- TutorialForceModel.TutorialOceanTides - Class in org.orekit.tutorials.yaml
-
Ocean tides.
- TutorialForceModel.TutorialPolynomialAcceleration - Class in org.orekit.tutorials.yaml
-
Polynomial acceleration.
- TutorialForceModel.TutorialRelativity - Class in org.orekit.tutorials.yaml
-
Post-Newtonian correction force due to general relativity.
- TutorialForceModel.TutorialSolarRadiationPressure - Class in org.orekit.tutorials.yaml
-
Solar radiation pressure.
- TutorialForceModel.TutorialThirdBody - Class in org.orekit.tutorials.yaml
-
Third body attraction.
- TutorialGaussNewton() - Constructor for class org.orekit.tutorials.yaml.TutorialOptimizationEngine.TutorialGaussNewton
- TutorialGravity() - Constructor for class org.orekit.tutorials.yaml.TutorialForceModel.TutorialGravity
- TutorialGrid() - Constructor for class org.orekit.tutorials.bodies.Phasing.TutorialGrid
- TutorialIntegrator - Class in org.orekit.tutorials.yaml
-
Initial data to initialize a numerical integrator.
- TutorialIntegrator() - Constructor for class org.orekit.tutorials.yaml.TutorialIntegrator
- TutorialIonosphere - Class in org.orekit.tutorials.yaml
-
Initial data to initialize an ionospheric delay model.
- TutorialIonosphere() - Constructor for class org.orekit.tutorials.yaml.TutorialIonosphere
- TutorialKalman - Class in org.orekit.tutorials.yaml
-
Initial data for the kalman filter estimator.
- TutorialKalman() - Constructor for class org.orekit.tutorials.yaml.TutorialKalman
-
Constructor.
- TutorialKeplerianOrbit() - Constructor for class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialKeplerianOrbit
- TutorialLevenbergMarquardt() - Constructor for class org.orekit.tutorials.yaml.TutorialOptimizationEngine.TutorialLevenbergMarquardt
- TutorialManeuver() - Constructor for class org.orekit.tutorials.yaml.TutorialForceModel.TutorialManeuver
- TutorialMeasurementGeneration() - Constructor for class org.orekit.tutorials.estimation.performance.MeasurementGenerator.TutorialMeasurementGeneration
- TutorialMeasurements - Class in org.orekit.tutorials.yaml
-
Initial data to initialize the measurements used during the orbit determination process.
- TutorialMeasurements() - Constructor for class org.orekit.tutorials.yaml.TutorialMeasurements
- TutorialMeasurements.TutorialAzEl - Class in org.orekit.tutorials.yaml
-
Azimuth/Elevation measurement.
- TutorialMeasurements.TutorialPhase - Class in org.orekit.tutorials.yaml
-
Phase measurement.
- TutorialMeasurements.TutorialPosition - Class in org.orekit.tutorials.yaml
-
Position only measurement.
- TutorialMeasurements.TutorialPV - Class in org.orekit.tutorials.yaml
-
Position/Velocity measurement.
- TutorialMeasurements.TutorialRange - Class in org.orekit.tutorials.yaml
-
Range measurement.
- TutorialMeasurements.TutorialRangeRate - Class in org.orekit.tutorials.yaml
-
Range rate measurement.
- TutorialObservationType() - Constructor for class org.orekit.tutorials.yaml.TutorialStation.TutorialObservationType
- TutorialOceanTides() - Constructor for class org.orekit.tutorials.yaml.TutorialForceModel.TutorialOceanTides
- TutorialOptimizationEngine - Class in org.orekit.tutorials.yaml
-
Optimization engine used by the estimator.
- TutorialOptimizationEngine() - Constructor for class org.orekit.tutorials.yaml.TutorialOptimizationEngine
- TutorialOptimizationEngine.TutorialGaussNewton - Class in org.orekit.tutorials.yaml
-
Gauss-Newton optimizer.
- TutorialOptimizationEngine.TutorialLevenbergMarquardt - Class in org.orekit.tutorials.yaml
-
Levenberg-Marquardt optimizer.
- TutorialOrbit - Class in org.orekit.tutorials.yaml
-
Initial data for the orbit determination orbit.
- TutorialOrbit() - Constructor for class org.orekit.tutorials.yaml.TutorialOrbit
- TutorialOrbitDetermination - Class in org.orekit.tutorials.estimation.common
-
Initial data to initialize an orbit determination tutorial.
- TutorialOrbitDetermination() - Constructor for class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
- TutorialOrbitType - Class in org.orekit.tutorials.yaml
-
Input data for tutorial orbit type.
- TutorialOrbitType() - Constructor for class org.orekit.tutorials.yaml.TutorialOrbitType
- TutorialOrbitType.TutorialCartesianOrbit - Class in org.orekit.tutorials.yaml
-
Cartesian orbit.
- TutorialOrbitType.TutorialCircularOrbit - Class in org.orekit.tutorials.yaml
-
Circular orbit.
- TutorialOrbitType.TutorialEquinoctialOrbit - Class in org.orekit.tutorials.yaml
-
Equinoctial orbit.
- TutorialOrbitType.TutorialKeplerianOrbit - Class in org.orekit.tutorials.yaml
-
Keplerian orbit.
- TutorialOrbitType.TutorialTLE - Class in org.orekit.tutorials.yaml
-
TLE data.
- TutorialPerformanceTesting() - Constructor for class org.orekit.tutorials.estimation.performance.PerformanceTesting.TutorialPerformanceTesting
- TutorialPhase() - Constructor for class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPhase
- TutorialPhasing() - Constructor for class org.orekit.tutorials.bodies.Phasing.TutorialPhasing
- TutorialPolynomialAcceleration() - Constructor for class org.orekit.tutorials.yaml.TutorialForceModel.TutorialPolynomialAcceleration
-
Constructor.
- TutorialPosition() - Constructor for class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPosition
- TutorialPropagator - Class in org.orekit.tutorials.yaml
-
Initial data to initialize an orbit propagator.
- TutorialPropagator() - Constructor for class org.orekit.tutorials.yaml.TutorialPropagator
- TutorialPV() - Constructor for class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialPV
- TutorialRange() - Constructor for class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRange
- TutorialRangeRate() - Constructor for class org.orekit.tutorials.yaml.TutorialMeasurements.TutorialRangeRate
- TutorialRelativity() - Constructor for class org.orekit.tutorials.yaml.TutorialForceModel.TutorialRelativity
- TutorialSequentialBatch() - Constructor for class org.orekit.tutorials.estimation.SequentialBatchLeastSquares.TutorialSequentialBatch
- TutorialSinex - Class in org.orekit.tutorials.yaml
-
Container for SINEX data.
- TutorialSinex() - Constructor for class org.orekit.tutorials.yaml.TutorialSinex
- TutorialSolarRadiationPressure() - Constructor for class org.orekit.tutorials.yaml.TutorialForceModel.TutorialSolarRadiationPressure
- TutorialSpacecraft - Class in org.orekit.tutorials.yaml
-
Initial data to initialize the spacecraft state.
- TutorialSpacecraft() - Constructor for class org.orekit.tutorials.yaml.TutorialSpacecraft
-
Constructor.
- TutorialStation - Class in org.orekit.tutorials.yaml
-
Initial data used to initialize station data (name, coordinates, observation types and measurement data).
- TutorialStation() - Constructor for class org.orekit.tutorials.yaml.TutorialStation
-
Constructor.
- TutorialStation.TutorialObservationType - Class in org.orekit.tutorials.yaml
-
Observation types for the measurements.
- TutorialStationDisplacement - Class in org.orekit.tutorials.yaml
-
Initial data to initialize the station displacement.
- TutorialStationDisplacement() - Constructor for class org.orekit.tutorials.yaml.TutorialStationDisplacement
- TutorialStationKeeping() - Constructor for class org.orekit.tutorials.maneuvers.StationKeeping.TutorialStationKeeping
- TutorialThirdBody() - Constructor for class org.orekit.tutorials.yaml.TutorialForceModel.TutorialThirdBody
- TutorialTLE() - Constructor for class org.orekit.tutorials.yaml.TutorialOrbitType.TutorialTLE
- TutorialTrackCorridor() - Constructor for class org.orekit.tutorials.propagation.TrackCorridor.TutorialTrackCorridor
- TutorialTroposphere - Class in org.orekit.tutorials.yaml
-
Initial data to initialize a tropospheric delay model.
- TutorialTroposphere() - Constructor for class org.orekit.tutorials.yaml.TutorialTroposphere
- TutorialVisibilityCircle() - Constructor for class org.orekit.tutorials.propagation.VisibilityCircle.TutorialVisibilityCircle
U
- UNKNOWN_FRAME - Static variable in class org.orekit.tutorials.estimation.common.TutorialOrbitDetermination
-
Error message for unknown frame.
V
- valueOf(String) - Static method in enum org.orekit.tutorials.estimation.common.AttitudeMode
-
Returns the enum constant of this type with the specified name.
- values() - Static method in enum org.orekit.tutorials.estimation.common.AttitudeMode
-
Returns an array containing the constants of this enum type, in the order they are declared.
- VisibilityCheck - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for special event detection.
- VisibilityCircle - Class in org.orekit.tutorials.propagation
-
Orekit tutorial for computing visibility circles.
- VisibilityCircle.TutorialVisibilityCircle - Class in org.orekit.tutorials.propagation
-
Input data for the visibility circle tutorial.
W
- writeOPM(OpmWriter, Opm, File) - Static method in class org.orekit.tutorials.utils.NdmUtils
-
Writes an OPM to a file.
Y
- YZPlaneCrossingDetector - Class in org.orekit.tutorials.propagation.cr3bp
-
Detector for YZ Planes crossing.
- YZPlaneCrossingDetector(double, double, double) - Constructor for class org.orekit.tutorials.propagation.cr3bp.YZPlaneCrossingDetector
-
Simple Constructor.
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