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Two different approaches for a control law of single gimbal control moment gyrosIn the field of momentum exchange attitude control systems, single gimbal control moment gyros (SGCMG) are of increasing interest. A gimbal angle approach and a gimbal rate approach are presented for the SGCMG control law including the singularity avoidance. Both approaches are compared and some illustrative examples are given.
Document ID
19720024010
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Schiehlen, W. O. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
August 2, 1972
Subject Category
Navigation
Report/Patent Number
NASA-TM-X-64693
Report Number: NASA-TM-X-64693
Accession Number
72N31660
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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