An asymptotically stable damping enhancement controller for large space structuresA secondary controller which uses a number of Annular Momentum Control Devices (AMCD's) for enhancement of structural damping in large flexible space structures is investigated. The closed-loop secondary controller is shown to be equivalent to a certain closed-loop optimal linear regulator, and the necessary and sufficient conditions for asymptotic stability are obtained. Sufficient conditions for asymptotic stability are also obtained which are much less restrictive than those obtained in an earlier paper. Design of a robust stable primary controller is also discussed.
Document ID
19810038362
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Joshi, S. M. (Vigyan Research Associates, Inc. Hampton, Va., United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1981
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 81-0455Report Number: AIAA PAPER 81-0455
Meeting Information
Meeting: Conference on Large Space Platforms: Toward Permanent Manned Occupancy of Space
Location: San Diego, CA
Start Date: February 2, 1981
End Date: February 4, 1981
Sponsors: American Institute of Aeronautics and Astronautics