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

Syntax

myVariable1 = mySpacecraft1.AngularAcceleration[0];