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The dual-momentum control device for large space systemsThe dual-momentum control device being studied for large spacecraft consists of two counter-rotating rings, each designated as an annular momentum control device (AMCD). For large rings, flexibility is appreciable and it becomes necessary to account for the distributed nature of the rings in the design of the magnetic bearing controllers. Also, ring behavior is unpredictably sensitive to ring temperature, spin rate, manufacturing imperfections, and other variables. For that reason, an adaptive control system is being sought for ring stabilization and maneuvering. This paper details an original adaptive control methodology for distributed parameter systems and illustrates this technique by application to AMCD stabilization.
Document ID
19790050731
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Montgomery, R. C.
(NASA Langley Research Center Flight Dynamics and Control Div., Hampton, Va., United States)
Johnson, C. R., Jr.
(NASA Langley Research Center Hampton; Virginia Polytechnic Institute and State University, Blacksburg, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 79-0923
Report Number: AIAA PAPER 79-0923
Meeting Information
Meeting: Conference on Advanced Technology for Future Space Systems
Location: Hampton, VA
Start Date: May 8, 1979
End Date: May 10, 1979
Accession Number
79A34744
Distribution Limits
Public
Copyright
Other

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