fr.cnes.sirius.patrius.events.sensor

Class SecondarySpacecraft

java.lang.Object

fr.cnes.sirius.patrius.events.sensor.SecondarySpacecraft

All Implemented Interfaces:

Serializable

public class SecondarySpacecraft
extends Object
implements Serializable

Secondary spacecraft to be used in events detections. It is described by its assembly of parts and a propagator.

Since:

1.2 HISTORY VERSION:4.3:DM:DM-2097:15/05/2019:[PATRIUS et COLOSUS] Mise en conformite du code avec le nouveau standard de codage DYNVOL VERSION::FA:231:03/04/2014:bad updating of the assembly's tree of frames END-HISTORY

Version:

$Id$

Author:

Thomas Trapier

See Also:

Serialized Form

Concurrency :

not thread-safe

Concurrency comment :

the direct use of a not thread-safe Assembly makes this class not thread-safe itself

Constructor Summary

Constructors

Constructor and Description
SecondarySpacecraft(Assembly assembly, Propagator propagator, String name) Constructor for a secondary spacecraft to be used in events detections.

Method Summary

Modifier and Type	Method and Description
Assembly	getAssembly()
String	getName()
void	updateSpacecraftState(AbsoluteDate date) Updates the assembly frames at a given date from the orbit and attitude information provided by the propagator.

Methods inherited from class java.lang.Object

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

Constructor Detail

SecondarySpacecraft

public SecondarySpacecraft(Assembly assembly,
                           Propagator propagator,
                           String name)

Constructor for a secondary spacecraft to be used in events detections.

Parameters:

assembly - the spacecraft's assembly

propagator - the spacecraft's propagator

name - the spacecraft's name

Method Detail

getAssembly

public Assembly getAssembly()

Returns:

the spacecraft's assembly

getName

public String getName()

Returns:

the spacecraft's name

updateSpacecraftState

public void updateSpacecraftState(AbsoluteDate date)
                           throws PatriusException

Updates the assembly frames at a given date from the orbit and attitude information provided by the propagator.

Parameters:

date - the date

Throws:

PatriusException - if some frames problem occurs