Package org.orekit.files.ccsds

Class OEMParser

java.lang.Object

org.orekit.files.ccsds.ODMParser

org.orekit.files.ccsds.OEMParser

All Implemented Interfaces:

EphemerisFileParser

public class OEMParser
extends ODMParser
implements EphemerisFileParser

A parser for the CCSDS OEM (Orbit Ephemeris Message).

Since:

6.1

Author:

sports

Constructor Summary

Constructors

Constructor	Description
OEMParser()	Simple constructor.

Method Summary

Modifier and Type	Method	Description
OEMFile	parse(BufferedReader reader, String fileName)	Parse an ephemeris file from a stream.
OEMFile	parse(InputStream stream)	Parse a CCSDS Orbit Data Message.
OEMFile	parse(InputStream stream, String fileName)	Parse a CCSDS Orbit Data Message.
OEMFile	parse(String fileName)	Parse a CCSDS Orbit Data Message.
OEMParser	withConventions(IERSConventions newConventions)	Set IERS conventions.
OEMParser	withInternationalDesignator(int newLaunchYear, int newLaunchNumber, String newLaunchPiece)	Set international designator.
OEMParser	withMissionReferenceDate(AbsoluteDate newMissionReferenceDate)	Set initial date.
OEMParser	withMu(double newMu)	Set gravitational coefficient.
OEMParser	withSimpleEOP(boolean newSimpleEOP)	Set EOP interpolation method.

Methods inherited from class java.lang.Object

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

Methods inherited from class org.orekit.files.ccsds.ODMParser

getConventions, getLaunchNumber, getLaunchPiece, getLaunchYear, getMissionReferenceDate, getMu, isSimpleEOP, parseCCSDSFrame, parseComment, parseDate, parseGeneralStateDataEntry, parseHeaderEntry, parseMetaDataEntry

Constructor Detail

OEMParser

public OEMParser()

Simple constructor.

This class is immutable, and hence thread safe. When parts must be changed, such as reference date for Mission Elapsed Time or Mission Relative Time time systems, or the gravitational coefficient or the IERS conventions, the various withXxx methods must be called, which create a new immutable instance with the new parameters. This is a combination of the builder design pattern and a fluent interface.

The initial date for Mission Elapsed Time and Mission Relative Time time systems is not set here. If such time systems are used, it must be initialized before parsing by calling withMissionReferenceDate(AbsoluteDate).

The gravitational coefficient is not set here. If it is needed in order to parse Cartesian orbits where the value is not set in the CCSDS file, it must be initialized before parsing by calling withMu(double).

The IERS conventions to use is not set here. If it is needed in order to parse some reference frames or UT1 time scale, it must be initialized before parsing by calling withConventions(IERSConventions).

Method Detail

withMissionReferenceDate

public OEMParser withMissionReferenceDate(AbsoluteDate newMissionReferenceDate)

Set initial date.

Specified by:

withMissionReferenceDate in class ODMParser

Parameters:

newMissionReferenceDate - mission reference date to use while parsing

Returns:

a new instance, with mission reference date replaced

See Also:

ODMParser.getMissionReferenceDate()

withMu

public OEMParser withMu(double newMu)

Set gravitational coefficient.

Specified by:

withMu in class ODMParser

Parameters:

newMu - gravitational coefficient to use while parsing

Returns:

a new instance, with gravitational coefficient date replaced

See Also:

ODMParser.getMu()

withConventions

public OEMParser withConventions(IERSConventions newConventions)

Set IERS conventions.

Specified by:

withConventions in class ODMParser

Parameters:

newConventions - IERS conventions to use while parsing

Returns:

a new instance, with IERS conventions replaced

See Also:

ODMParser.getConventions()

withSimpleEOP

public OEMParser withSimpleEOP(boolean newSimpleEOP)

Set EOP interpolation method.

Specified by:

withSimpleEOP in class ODMParser

Parameters:

newSimpleEOP - if true, tidal effects are ignored when interpolating EOP

Returns:

a new instance, with EOP interpolation method replaced

See Also:

ODMParser.isSimpleEOP()

withInternationalDesignator

public OEMParser withInternationalDesignator(int newLaunchYear,
                                             int newLaunchNumber,
                                             String newLaunchPiece)

Set international designator.

This method may be used to ensure the launch year number and pieces are correctly set if they are not present in the CCSDS file header in the OBJECT_ID in the form YYYY-NNN-P{PP}. If they are already in the header, they will be parsed automatically regardless of this method being called or not (i.e. header information override information set here).

Specified by:

withInternationalDesignator in class ODMParser

Parameters:

newLaunchYear - launch year

newLaunchNumber - launch number

newLaunchPiece - piece of launch (from "A" to "ZZZ")

Returns:

a new instance, with TLE settings replaced

parse

public OEMFile parse(String fileName)

Parse a CCSDS Orbit Data Message.

Specified by:

parse in interface EphemerisFileParser

Overrides:

parse in class ODMParser

Parameters:

fileName - name of the file containing the message

Returns:

parsed orbit

parse

public OEMFile parse(InputStream stream)

Parse a CCSDS Orbit Data Message.

Overrides:

parse in class ODMParser

Parameters:

stream - stream containing message

Returns:

parsed orbit

parse

public OEMFile parse(InputStream stream,
                     String fileName)

Parse a CCSDS Orbit Data Message.

Specified by:

parse in class ODMParser

Parameters:

stream - stream containing message

fileName - name of the file containing the message (for error messages)

Returns:

parsed orbit

parse

public OEMFile parse(BufferedReader reader,
                     String fileName)

Description copied from interface: EphemerisFileParser

Parse an ephemeris file from a stream.

Specified by:

parse in interface EphemerisFileParser

Parameters:

reader - containing the ephemeris file.

fileName - to use in error messages.

Returns:

a parsed ephemeris file.