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SPS flexible system control assessment analysisActive control of the Satellite Power System (SPS0, a large mechanically flexible aerospace structure is addressed. The control algorithm is the principle component in the feedback link from sensors to actuators. An analysis of the interaction of the SPS structure and its active control system is presented.
Document ID
19810016587
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Balas, M. J. (Rensselaer Polytechnic Inst. Troy, NY, United States)
Date Acquired
September 4, 2013
Publication Date
March 15, 1981
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-160962
Report Number: NASA-CR-160962
Accession Number
81N25122
Funding Number(s)
CONTRACT_GRANT: NAS9-16053
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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