org.orekit.files.ccsds.ndm.adm.aem

Class AemSatelliteEphemeris

java.lang.Object

org.orekit.files.ccsds.ndm.adm.aem.AemSatelliteEphemeris

All Implemented Interfaces:

AttitudeEphemerisFile.SatelliteAttitudeEphemeris<TimeStampedAngularCoordinates,AemSegment>

public class AemSatelliteEphemeris
extends Object
implements AttitudeEphemerisFile.SatelliteAttitudeEphemeris<TimeStampedAngularCoordinates,AemSegment>

AEM ephemeris blocks for a single satellite.

Author:

Bryan Cazabonne

Constructor Summary

Constructors

Constructor and Description
AemSatelliteEphemeris(String id, List<AemSegment> blocks) Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.

Method Summary

Modifier and Type	Method and Description
String	getId() Get the satellite ID.
List<AemSegment>	getSegments() Get the segments of the attitude ephemeris.
AbsoluteDate	getStart() Get the start date of the ephemeris.
AbsoluteDate	getStop() Get the end date of the ephemeris.

Methods inherited from class java.lang.Object

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

Methods inherited from interface org.orekit.files.general.AttitudeEphemerisFile.SatelliteAttitudeEphemeris

getAttitudeProvider

Constructor Detail

AemSatelliteEphemeris

public AemSatelliteEphemeris(String id,
                             List<AemSegment> blocks)

Create a container for the set of ephemeris blocks in the file that pertain to a single satellite.

Parameters:

id - of the satellite.

blocks - containing ephemeris data for the satellite.

Since:

10.3

Method Detail

getId

public String getId()

Get the satellite ID. The satellite ID is unique only within the same ephemeris file.

Specified by:

getId in interface AttitudeEphemerisFile.SatelliteAttitudeEphemeris<TimeStampedAngularCoordinates,AemSegment>

Returns:

the satellite's ID, never null.

getSegments

public List<AemSegment> getSegments()

Get the segments of the attitude ephemeris.

Attitude ephemeris segments are typically used to split an ephemeris around discontinuous events.

Specified by:

getSegments in interface AttitudeEphemerisFile.SatelliteAttitudeEphemeris<TimeStampedAngularCoordinates,AemSegment>

Returns:

the segments contained in the attitude ephemeris file for this satellite.

getStart

public AbsoluteDate getStart()

Get the start date of the ephemeris.

Specified by:

getStart in interface AttitudeEphemerisFile.SatelliteAttitudeEphemeris<TimeStampedAngularCoordinates,AemSegment>

Returns:

ephemeris start date.

getStop

public AbsoluteDate getStop()

Get the end date of the ephemeris.

Specified by:

getStop in interface AttitudeEphemerisFile.SatelliteAttitudeEphemeris<TimeStampedAngularCoordinates,AemSegment>

Returns:

ephemeris end date.