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ATM-CMG control system stabilityStability analyses and simulation data and results are presented for an initial Control Moment Gyroscope system proposed for the Apollo Telescope Mount cluster (later named Skylab) using momentum vector feedback. A compensation filtering technique is presented which significantly improved analytical and simulation performance of the system. This technique is quite similar to the complementary filtering technique and represents an early NASA application.
Document ID
19800017878
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Anderson, W. W.
(NASA Langley Research Center Hampton, VA, United States)
Avis, L. M.
(NASA Langley Research Center Hampton, VA, United States)
Jacobs, K. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81827
Report Number: NASA-TM-81827
Accession Number
80N26377
Funding Number(s)
PROJECT: RTOP 506-54-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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