Package org.orekit.files.ccsds.ndm.odm.opm

Class Opm

java.lang.Object

org.orekit.files.ccsds.ndm.NdmConstituent<OdmHeader,Segment<OdmCommonMetadata,OpmData>>

org.orekit.files.ccsds.ndm.odm.opm.Opm

All Implemented Interfaces:

TimeStamped

public class Opm
extends NdmConstituent<OdmHeader,Segment<OdmCommonMetadata,OpmData>>
implements TimeStamped

This class gathers the informations present in the Orbital Parameter Message (OPM).

Since:

6.1

Author:

sports

Field Summary

Fields

Modifier and Type	Field	Description
static String	FORMAT_VERSION_KEY	Key for format version.
static String	ROOT	Root element for XML files.

Constructor Summary

Constructors

Constructor	Description
Opm(OdmHeader header, List<Segment<OdmCommonMetadata,OpmData>> segments, IERSConventions conventions, DataContext dataContext, double mu)	Simple constructor.

Method Summary

Modifier and Type	Method	Description
CartesianOrbit	generateCartesianOrbit()	Generate a Cartesian orbit.
KeplerianOrbit	generateKeplerianOrbit()	Generate a keplerian orbit.
SpacecraftState	generateSpacecraftState()	Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.
OpmData	getData()	Get the file data.
AbsoluteDate	getDate()	Get the date.
Maneuver	getManeuver(int index)	Get a maneuver.
List<Maneuver>	getManeuvers()	Get a list of all maneuvers.
OdmCommonMetadata	getMetadata()	Get the file metadata.
int	getNbManeuvers()	Get the number of maneuvers present in the OPM.
TimeStampedPVCoordinates	getPVCoordinates()	Get the position/velocity coordinates contained in the OPM.
boolean	hasManeuvers()	check whether the OPM contains at least one maneuver.

Methods inherited from class org.orekit.files.ccsds.ndm.NdmConstituent

getConventions, getDataContext, getHeader, getSegments, setHeader, setSegments, validate

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Methods inherited from interface org.orekit.time.TimeStamped

durationFrom

Field Detail

ROOT

public static final String ROOT

Root element for XML files.

See Also:

Constant Field Values

FORMAT_VERSION_KEY

public static final String FORMAT_VERSION_KEY

Key for format version.

See Also:

Constant Field Values

Constructor Detail

Opm

public Opm(OdmHeader header,
           List<Segment<OdmCommonMetadata,OpmData>> segments,
           IERSConventions conventions,
           DataContext dataContext,
           double mu)

Simple constructor.

Parameters:

header - file header

segments - file segments

conventions - IERS conventions

dataContext - used for creating frames, time scales, etc.

mu - gravitational coefficient to use for building Cartesian/Keplerian orbits

Method Detail

getMetadata

public OdmCommonMetadata getMetadata()

Get the file metadata.

Returns:

file metadata

getData

public OpmData getData()

Get the file data.

Returns:

file data

getDate

public AbsoluteDate getDate()

Get the date.

Specified by:

getDate in interface TimeStamped

Returns:

date attached to the object

getNbManeuvers

public int getNbManeuvers()

Get the number of maneuvers present in the OPM.

Returns:

the number of maneuvers

getManeuvers

public List<Maneuver> getManeuvers()

Get a list of all maneuvers.

Returns:

unmodifiable list of all maneuvers.

getManeuver

public Maneuver getManeuver(int index)

Get a maneuver.

Parameters:

index - maneuver index, counting from 0

Returns:

maneuver

hasManeuvers

public boolean hasManeuvers()

check whether the OPM contains at least one maneuver.

Returns:

true if OPM contains at least one maneuver false otherwise

getPVCoordinates

public TimeStampedPVCoordinates getPVCoordinates()

Get the position/velocity coordinates contained in the OPM.

Returns:

the position/velocity coordinates contained in the OPM

generateCartesianOrbit

public CartesianOrbit generateCartesianOrbit()

Generate a Cartesian orbit.

Returns:

generated orbit

generateKeplerianOrbit

public KeplerianOrbit generateKeplerianOrbit()

Generate a keplerian orbit.

Returns:

generated orbit

generateSpacecraftState

public SpacecraftState generateSpacecraftState()

Generate spacecraft state from the CartesianOrbit generated by generateCartesianOrbit.

Returns:

the spacecraft state of the OPM