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Robust design of distributed controllers for large flexible space structuresIndependent Modal Space Control (IMSC) method avoids control spillover generated by conventional control schemes such as Coupled Modal Control by decoupling the large flexible space structure into independent subsystems of second order and controlling each mode independently. The IMSC implementation requires that the number of actuators be equal to that of modeled modes, which is in general very huge. Consequently the number of required actuators is unrealizable. Two methods are proposed for the implementation of IMSC with reduced number of actuators. In the first method, the first m modes are optimized, leaving the last (n-m) modes unchanged. In the second method, generalized inverse matrices are employed to design the feedback controller so that the control scheme is suboptimal with respect to IMSC. The performance of the proposed methods is tested by performing computer simulation on a simply support beam. Simulation results are presented and discussed.
Document ID
19880020750
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nguyen, Charles C.
(Catholic Univ. of America, Washington, DC, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1988
Subject Category
Mechanical Engineering
Report/Patent Number
NAS 1.26:183202
NASA-CR-183202
Report Number: NAS 1.26:183202
Report Number: NASA-CR-183202
Accession Number
88N30134
Funding Number(s)
CONTRACT_GRANT: NAG5-949
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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