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A survey of decentralized control techniques for large space structuresPreliminary results on the design of decentralized controllers for the COFS I Mast are reported. A nine mode finite element model is used along with second order model of the actuators. It is shown that without actuator dynamics, the system is stable with collocated rate feedback and has acceptable performace. However, when actuator dynamics are included, the system is unstable.
Document ID
19880040132
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lindner, D. K.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Reichard, K.
(Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 1987 American Control Conference
Location: Minneapolis, MN
Country: United States
Start Date: June 10, 1987
End Date: June 12, 1987
Sponsors: American Automatic Control Council
Accession Number
88A27359
Funding Number(s)
CONTRACT_GRANT: NAS1-18106
Distribution Limits
Public
Copyright
Other

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