Spacecraft.AngularAcceleration Property

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Description

The angular acceleration vector that is associated with the quaternion attitude system. When using a Spinner attitude system the angular acceleration is populated with values; which will be non-zero if you have a non-zero nutation angle, and the Spacecraft moment of inertia Ixx != Iyy != Izz.

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:	Array of number (size = 3)
Access:	read
Units:	deg/s2

Syntax

myVariable1 = mySpacecraft1.AngularAcceleration[0];