Spacecraft.AttitudeMatrix Property

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Description

The Direction-Cosine-Matrix (DCM) that defines the rotation from the specified Attitude Reference Frame to the Spacecraft Body Coordinate System.

 

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond timing precision mode.

 

Attributes

Type:

Matrix of number (size = 3 x 3)

Access:

read/write

Default Value:

[1.0,0.0,0.0;0.0,1.0,0.0;0.0,0.0,1.0]

 

Syntax

myMatrix1 = mySpacecraft1.AttitudeMatrix;

 

mySpacecraft1.AttitudeMatrix = myMatrix1;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide