Spacecraft.AttitudeSystem Property

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Description

Specifies which attitude system set defines the Spacecraft state.

 

Timing Precision Mode

This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

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

 

Attributes

Type:

string

Access:

read/write

Default Value:

"EulerAngles" ( Euler Angles )

Valid Values:

Value

Label

"EulerAngles"

Euler Angles

"Quaternion"

Quaternion

"AttitudeMatrix"

Attitude Matrix

"Spinner"

Spinner

 

Syntax

myString1 = mySpacecraft1.AttitudeSystem;

 

mySpacecraft1.AttitudeSystem = myString1;

 

See also

Spacecraft Object

Spacecraft Propagation Guide

Coverage and Contact Analysis Guide