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A steering law for a roof-type configuration for a single-gimbal control moment gyro systemSingle-Gimbal Control Moment Gyro (SGCMG) systems have been investigated for attitude control of the Large Space Telescope (LST) and the High Energy Astronomy Observatory (HEAO). However, various proposed steering laws for the SGCMG systems thus far have some defects because of singular states of the system. In this report, a steering law for a roof-type SGCMG system is proposed which is based on a new momentum distribution scheme that makes all the singular states unstable. This momentum distribution scheme is formulated by a treatment of the system as a sampled-data system. From analytical considerations, it is shown that this steering law gives control performance which is satisfactory for practical applications. Results of the preliminary computer simulation entirely support this premise.
Document ID
19750008780
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Yoshikawa, T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
December 12, 1974
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-TM-X-64907
Report Number: NASA-TM-X-64907
Accession Number
75N16852
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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