org.orekit.files.ccsds

Class AEMFile.AemSatelliteEphemeris

java.lang.Object

org.orekit.files.ccsds.AEMFile.AemSatelliteEphemeris

Enclosing class:

AEMFile

public static class AEMFile.AemSatelliteEphemeris
extends Object

AEM ephemeris blocks for a single satellite.

Constructor Summary

Constructors

Constructor and Description
AemSatelliteEphemeris(List<AEMFile.AttitudeEphemeridesBlock> 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
List<AEMFile.AttitudeEphemeridesBlock>	getSegments() Get the segments of the attitude ephemeris.
AbsoluteDate	getStart() Get the start date of the attitude ephemeris.
AbsoluteDate	getStop() Get the end date of the attitude ephemeris.

Methods inherited from class java.lang.Object

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

Constructor Detail

AemSatelliteEphemeris

public AemSatelliteEphemeris(List<AEMFile.AttitudeEphemeridesBlock> blocks)

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

Parameters:

blocks - containing ephemeris data for the satellite.

Method Detail

getSegments

public List<AEMFile.AttitudeEphemeridesBlock> getSegments()

Get the segments of the attitude ephemeris.

Ephemeris segments are typically used to split an attitude ephemeris around discontinuous events, such as maneuvers.

Returns:

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

getStart

public AbsoluteDate getStart()

Get the start date of the attitude ephemeris.

Returns:

attitude ephemeris start date.

getStop

public AbsoluteDate getStop()

Get the end date of the attitude ephemeris.

Returns:

attitude ephemeris end date.