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Modular design attitude control systemApplication of modular control techniques to the attitude control of a prototype flexible spacecraft and a prototype flexible space platform was further developed by determining numerical values for the physical parameters of a four body approximation of the MSFC/hybrid deployable truss incorporated in the space platform model, generating sensitivity coefficients for the model of the flexible spacecraft, evaluating the changes in the digital computer simulation of the flexible spacecraft resulting from the addition of another rigid body to the model and comparing attitude control effectiveness with actuators on more than one rigid body of the model with that for the case in which the actuators were restricted to one body.
Document ID
19830016270
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chichester, F. D. (Bendix Corp. Teterboro, NJ, United States)
Date Acquired
September 4, 2013
Publication Date
March 18, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-170736
NAS 1.26:170736
Accession Number
83N24541
Funding Number(s)
CONTRACT_GRANT: NAS8-33979
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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