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Reduction of Model Complexity by Active ControlThe mathematical models of many dynamic systems of interest in the aerospace industry are inherently complex and of high order. Rather than grapple with the full-complexity models for such systems, the control designers often elect to derive low-order, reduced-complexity models for which a control system can be designed. The subject of model-order reduction has received a significant amount of attention in control engineering literature. This paper describes and demonstrates a novel active-control methodology that can be used to design a control system that automatically forces the original system to behave like a chosen reduced-complexity model by treating the effects of the original complexity-related terms as disturbances acting on the reduced-complexity system. The method is demonstrated by several worked examples involving both linear and nonlinear systems, supported by simulation results.
Document ID
19980011876
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Bukley, Angelia P.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Johnson, C. D.
(Alabama Univ. Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Cybernetics
Report/Patent Number
NAS 1.15:112810
NASA-TM-112810
Report Number: NAS 1.15:112810
Report Number: NASA-TM-112810
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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