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

Class SpacecraftParameters

java.lang.Object

org.orekit.files.ccsds.section.CommentsContainer

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

All Implemented Interfaces:

Section

public class SpacecraftParameters
extends CommentsContainer

Container for spacecraft parameters data.

Since:

10.2

Author:

Bryan Cazabonne

Constructor Summary

Constructors

Constructor and Description
SpacecraftParameters() Simple constructor.

Method Summary

Modifier and Type	Method and Description
double	getI11() Get the moment of Inertia about the 1-axis (N.m²).
double	getI12() Get the moment of Inertia about the 1 and 2 axes (N.m²).
double	getI13() Get the moment of Inertia about the 1 and 3 axes (N.m²).
double	getI22() Get the moment of Inertia about the 2-axis (N.m²).
double	getI23() Get the moment of Inertia about the 2 and 3 axes (N.m²).
double	getI33() Get the moment of Inertia about the 3-axis (N.m²).
FrameFacade	getInertiaReferenceFrame() Get the coordinate system for the inertia tensor.
void	setI11(double i11) Set the moment of Inertia about the 1-axis (N.m²).
void	setI12(double i12) Set the moment of Inertia about the 1 and 2 axes (N.m²).
void	setI13(double i13) Set the moment of Inertia about the 1 and 3 axes (N.m²).
void	setI22(double i22) Set the moment of Inertia about the 2-axis (N.m²).
void	setI23(double i23) Set the moment of Inertia about the 2 and 3 axes (N.m²).
void	setI33(double i33) Set the moment of Inertia about the 3-axis (N.m²).
void	setInertiaReferenceFrame(FrameFacade inertiaReferenceFrame) Set the coordinate system for the inertia tensor.
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

SpacecraftParameters

public SpacecraftParameters()

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

getInertiaReferenceFrame

public FrameFacade getInertiaReferenceFrame()

Get the coordinate system for the inertia tensor.

Returns:

the coordinate system for the inertia tensor

setInertiaReferenceFrame

public void setInertiaReferenceFrame(FrameFacade inertiaReferenceFrame)

Set the coordinate system for the inertia tensor.

Parameters:

inertiaReferenceFrame - frame to be set

getI11

public double getI11()

Get the moment of Inertia about the 1-axis (N.m²).

Returns:

the moment of Inertia about the 1-axis.

setI11

public void setI11(double i11)

Set the moment of Inertia about the 1-axis (N.m²).

Parameters:

i11 - moment of Inertia about the 1-axis

getI22

public double getI22()

Get the moment of Inertia about the 2-axis (N.m²).

Returns:

the moment of Inertia about the 2-axis.

setI22

public void setI22(double i22)

Set the moment of Inertia about the 2-axis (N.m²).

Parameters:

i22 - moment of Inertia about the 2-axis

getI33

public double getI33()

Get the moment of Inertia about the 3-axis (N.m²).

Returns:

the moment of Inertia about the 3-axis.

setI33

public void setI33(double i33)

Set the moment of Inertia about the 3-axis (N.m²).

Parameters:

i33 - moment of Inertia about the 3-axis

getI12

public double getI12()

Get the moment of Inertia about the 1 and 2 axes (N.m²).

Returns:

the moment of Inertia about the 1 and 2 axes.

setI12

public void setI12(double i12)

Set the moment of Inertia about the 1 and 2 axes (N.m²).

Parameters:

i12 - moment of Inertia about the 1 and 2 axes

getI13

public double getI13()

Get the moment of Inertia about the 1 and 3 axes (N.m²).

Returns:

the moment of Inertia about the 1 and 3 axes.

setI13

public void setI13(double i13)

Set the moment of Inertia about the 1 and 3 axes (N.m²).

Parameters:

i13 - moment of Inertia about the 1 and 3 axes

getI23

public double getI23()

Get the moment of Inertia about the 2 and 3 axes (N.m²).

Returns:

the moment of Inertia about the 2 and 3 axes.

setI23

public void setI23(double i23)

Set the moment of Inertia about the 2 and 3 axes (N.m²).

Parameters:

i23 - moment of Inertia about the 2 and 3 axes