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Decentralized control of large flexible structures by joint decouplingA decentralized control design method is presented for large complex flexible structures by using the idea of joint decoupling. The derivation is based on a coupled substructure state-space model, which is obtained from enforcing conditions of interface compatibility and equilibrium to the substructure state-space models. It is shown that by restricting the control law to be localized state feedback and by setting the joint actuator input commands to decouple joint 'degrees of freedom' (dof) from interior dof, the global structure control design problem can be decomposed into several substructure control design problems. The substructure control gains and substructure observers are designed based on modified substructure state-space models. The controllers produced by the proposed method can operate successfully at the individual substructure level as well as at the global structure level. Therefore, not only control design but also control implementation is decentralized. Stability and performance requirement of the closed-loop system can be achieved by using any existing state feedback control design method. A two-component mass-spring damper system and a three-truss structure are used as examples to demonstrate the proposed method.
Document ID
19930002832
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Su, Tzu-Jeng
(NASA Langley Research Center Hampton, VA, United States)
Juang, Jer-Nan
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:107694
NASA-TM-107694
Report Number: NAS 1.15:107694
Report Number: NASA-TM-107694
Accession Number
93N12020
Funding Number(s)
PROJECT: RTOP 469-01-11-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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