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Use of guidance and control test cases to verify spacecraft attitude control system designA simulation and analysis approach is introduced for verification of attitude control flight software performance in a deep space mission.
Document ID
20210001796
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/8094
Authors
Lee, A. Y.
Barltrop, K. J.
Chang, L.
Brown, J. M.
Date Acquired
January 27, 2002
Publication Date
January 27, 2002
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Cassini
attitude
control
subsystem
AACS
G&C
testing
guidance
and
controls

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