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The dynamics of spin stabilized spacecraft with movable appendages, part 2Research efforts on various methods that employ moving external parts for spacecraft control are presented. Two basic types of appendages were considered: (1) a hinged type, and (2) a telescoping type. Procedures for evaluating each type of appendage are listed, and control laws and equations of motion for each type are also discussed. Illustrations of the different types of appendages are shown.
Document ID
19760004128
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bainum, P. M.
(Howard Univ. Washington, DC, United States)
Sellappan, R.
(Howard Univ. Washington, DC, United States)
Date Acquired
September 3, 2013
Publication Date
November 15, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-145605
Report Number: NASA-CR-145605
Accession Number
76N11216
Funding Number(s)
CONTRACT_GRANT: NSG-1181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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