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Model reduction in integrated controls-structures designIt is the objective of this paper to present a model reduction technique developed for the integrated controls-structures design of flexible structures. Integrated controls-structures design problems are typically posed as nonlinear mathematical programming problems, where the design variables consist of both structural and control parameters. In the solution process, both structural and control design variables are constantly changing; therefore, the dynamic characteristics of the structure are also changing. This presents a problem in obtaining a reduced-order model for active control design and analysis which will be valid for all design points within the design space. In other words, the frequency and number of the significant modes of the structure (modes that should be included) may vary considerably throughout the design process. This is also true as the locations and/or masses of the sensors and actuators change. Moreover, since the number of design evaluations in the integrated design process could easily run into thousands, any feasible order-reduction method should not require model reduction analysis at every design iteration. In this paper a novel and efficient technique for model reduction in the integrated controls-structures design process, which addresses these issues, is presented.
Document ID
19930009746
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Maghami, Peiman G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: The Fifth NASA(DOD Controls-Structures Interaction Technology Conference, Part 2
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93N18935
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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