Uses of Class
org.orekit.files.ccsds.ndm.odm.ocm.TrajectoryStateHistory

Packages that use TrajectoryStateHistory

Package	Description
org.orekit.files.ccsds.ndm.odm.ocm	This package contains class managing CCSDS Orbit Comprehensive Message.

Uses of TrajectoryStateHistory in org.orekit.files.ccsds.ndm.odm.ocm

Methods in org.orekit.files.ccsds.ndm.odm.ocm that return types with arguments of type TrajectoryStateHistory

Modifier and Type	Method	Description
List<TrajectoryStateHistory>	OcmSatelliteEphemeris.getSegments()	Get the segments of the ephemeris.
List<TrajectoryStateHistory>	OcmData.getTrajectoryBlocks()	Get trajectory state histories logical blocks.

Constructor parameters in org.orekit.files.ccsds.ndm.odm.ocm with type arguments of type TrajectoryStateHistory

Modifier	Constructor	Description
	OcmData(List<TrajectoryStateHistory> trajectoryBlocks, OrbitPhysicalProperties physicBlock, List<OrbitCovarianceHistory> covarianceBlocks, List<OrbitManeuverHistory> maneuverBlocks, Perturbations perturbationsBlock, OrbitDetermination orbitDeterminationBlock, UserDefined userDefinedBlock)	Simple constructor.
	OcmSatelliteEphemeris(String name, double mu, List<TrajectoryStateHistory> blocks)	Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.