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Control of the maneuvering SCOLE structureThis paper is concerned with the vibration control of the SCOLE structure while it undergoes a slewing maneuver. The control law is designed according to the linear quadratic regulator theory. In view of saturation limits on the actuators, the actual implementation is modified so as to observe these limits, resulting in suboptimal control. State estimation is carried out by means of a Kalman filter. The control and state estimation are carried out in discrete time. Numerical simulations for several cases of interest are presented.
Document ID
19930045382
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lim, S.
(NASA Langley Research Center Hampton, VA, United States)
Meirovitch, L.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: Dynamics and control of large structures; Proceedings of the 8th VPI&SU Symposium, Blacksburg, VA, May 6-8, 1991 (A93-29328 10-63)
Publisher: Virginia Polytechnic Institute and State University
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93A29379
Funding Number(s)
CONTRACT_GRANT: NAG1-225
Distribution Limits
Public
Copyright
Other

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