Package org.orekit.tutorials.yaml
This package provides classes to read the data
contained inside a YAML file.
- Author:
- Bryan Cazabonne
-
Class Summary Class Description TutorialBatchLSEstimator Initial data for the batch least squares orbit determination estimator.TutorialBody Initial data for the central body.TutorialEstimatedDateParameter Utility class for estimated date parameters during a maneuver estimation process.TutorialEstimatedParameter Utility class for estimated parameters during an orbit determination process.TutorialForceModel Initial data to initialize the main Orekit force models.TutorialForceModel.TutorialDrag Atmospheric drag.TutorialForceModel.TutorialGravity Central body gravity.TutorialForceModel.TutorialManeuver Maneuver.TutorialForceModel.TutorialOceanTides Ocean tides.TutorialForceModel.TutorialPolynomialAcceleration Polynomial acceleration.TutorialForceModel.TutorialRelativity Post-Newtonian correction force due to general relativity.TutorialForceModel.TutorialSolarRadiationPressure Solar radiation pressure.TutorialForceModel.TutorialThirdBody Third body attraction.TutorialIntegrator Initial data to initialize a numerical integrator.TutorialIonosphere Initial data to initialize an ionospheric delay model.TutorialKalman Initial data for the kalman filter estimator.TutorialMeasurements Initial data to initialize the measurements used during the orbit determination process.TutorialMeasurements.TutorialAzEl Azimuth/Elevation measurement.TutorialMeasurements.TutorialPhase Phase measurement.TutorialMeasurements.TutorialPosition Position only measurement.TutorialMeasurements.TutorialPV Position/Velocity measurement.TutorialMeasurements.TutorialRange Range measurement.TutorialMeasurements.TutorialRangeRate Range rate measurement.TutorialOptimizationEngine Optimization engine used by the estimator.TutorialOptimizationEngine.TutorialGaussNewton Gauss-Newton optimizer.TutorialOptimizationEngine.TutorialLevenbergMarquardt Levenberg-Marquardt optimizer.TutorialOrbit Initial data for the orbit determination orbit.TutorialOrbitType Input data for tutorial orbit type.TutorialOrbitType.TutorialCartesianOrbit Cartesian orbit.TutorialOrbitType.TutorialCircularOrbit Circular orbit.TutorialOrbitType.TutorialEquinoctialOrbit Equinoctial orbit.TutorialOrbitType.TutorialKeplerianOrbit Keplerian orbit.TutorialOrbitType.TutorialTLE TLE data.TutorialPropagator Initial data to initialize an orbit propagator.TutorialSinex Container for SINEX data.TutorialSpacecraft Initial data to initialize the spacecraft state.TutorialStation Initial data used to initialize station data (name, coordinates, observation types and measurement data).TutorialStation.TutorialObservationType Observation types for the measurements.TutorialStationDisplacement Initial data to initialize the station displacement.TutorialTroposphere Initial data to initialize a tropospheric delay model.