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The Galileo Attitude and Articulation Control System - A radiation-hard, high precision, state-of-the-art control systemThe Galileo Mission and Spacecraft design impose tight requirements on the Attitude and Articulation Control System (AACS). These requirements, coupled with the flexible spacecraft, the need for autonomy, and a severe radiation environment, pose a great challenge for the AACS designer. The resulting design and implementation are described, along with the discovery and solution of the Single-Event Upset problem. The status of the testing of the AACS in the Integration and Test Laboratory as well as at the spacecraft level is summarized.
Document ID
19880029060
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Rhoads Stephenson, R.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
88A16287
Distribution Limits
Public
Copyright
Other

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