org.orekit.files.ccsds.ndm.adm.apm

Class Maneuver

java.lang.Object

org.orekit.files.ccsds.section.CommentsContainer

org.orekit.files.ccsds.ndm.adm.apm.Maneuver

All Implemented Interfaces:

Section

public class Maneuver
extends CommentsContainer

Maneuver in an APM file.

Since:

10.2

Author:

Bryan Cazabonne

Constructor Summary

Constructors

Constructor and Description
Maneuver() Simple constructor.

Method Summary

Modifier and Type	Method and Description
double	getDeltaMass() Get mass change during maneuver.
double	getDuration() Get duration (value is 0 for impulsive maneuver).
AbsoluteDate	getEpochStart() Get epoch start.
FrameFacade	getFrame() Get Coordinate system for the torque vector.
org.hipparchus.geometry.euclidean.threed.Vector3D	getTorque() Get the torque vector (N.m).
void	setDeltaMass(double deltaMass) Set mass change during maneuver.
void	setDuration(double duration) Set duration (value is 0 for impulsive maneuver).
void	setEpochStart(AbsoluteDate epochStart) Set epoch start.
void	setFrame(FrameFacade frame) Set Coordinate system for the torque vector.
void	setTorque(int index, double value) Set the torque vector (N.m).
void	validate(double version) Check is all mandatory entries have been initialized.

Methods inherited from class org.orekit.files.ccsds.section.CommentsContainer

acceptComments, addComment, checkAllowed, checkNotNaN, checkNotNegative, checkNotNull, getComments, refuseFurtherComments

Methods inherited from class java.lang.Object

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

Constructor Detail

Maneuver

public Maneuver()

Simple constructor.

Method Detail

validate

public void validate(double version)

Check is all mandatory entries have been initialized.

This method should throw an exception if some mandatory entries are missing or not compatible with version number.

Specified by:

validate in interface Section

Overrides:

validate in class CommentsContainer

Parameters:

version - format version

getEpochStart

public AbsoluteDate getEpochStart()

Get epoch start.

Returns:

epoch start

setEpochStart

public void setEpochStart(AbsoluteDate epochStart)

Set epoch start.

Parameters:

epochStart - epoch start

getFrame

public FrameFacade getFrame()

Get Coordinate system for the torque vector.

Returns:

coordinate system for the torque vector

setFrame

public void setFrame(FrameFacade frame)

Set Coordinate system for the torque vector.

Parameters:

frame - coordinate system for the torque vector

getDuration

public double getDuration()

Get duration (value is 0 for impulsive maneuver).

Returns:

duration (value is 0 for impulsive maneuver)

setDuration

public void setDuration(double duration)

Set duration (value is 0 for impulsive maneuver).

Parameters:

duration - duration (value is 0 for impulsive maneuver)

getTorque

public org.hipparchus.geometry.euclidean.threed.Vector3D getTorque()

Get the torque vector (N.m).

Returns:

torque vector

setTorque

public void setTorque(int index,
                      double value)

Set the torque vector (N.m).

Parameters:

index - vector component index (counting from 0)

value - component value

getDeltaMass

public double getDeltaMass()

Get mass change during maneuver.

Returns:

mass change during maneuver (kg, negative)

Since:

12.0

setDeltaMass

public void setDeltaMass(double deltaMass)

Set mass change during maneuver.

Parameters:

deltaMass - mass change during maneuver (kg)

Since:

12.0