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Optimization of linear, controlled structuresAn approach to the integrated design of linear controlled structures, which is being investigated as part of NASA's controlled structures interaction (CSI) methodology development program, is presented. The approach is integrated in the sense that the structure and its controller are simultaneously designed. The design methodology uses constrained nonlinear optimization procedures based on analytically obtained gradients of the structural responses. Design of the controller is based on the so-called Q-parameterization theory, which parameterizes all closed-loop input/output maps achievable with stabiizing linear controllers. Very general objective and constraint functions are possible, and structural shape can be included in the design variables. This method has been partially implemented and demonstrated; early findings are reported.
Document ID
19910045461
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hunziker, K. Scott
(Boeing Aerospace Co. Seattle, WA, United States)
Kraft, Raymond H.
(Boeing Aerospace and Electronics Seattle, WA, United States)
Kosut, Robert T.
(Integrated Systems, Inc. Santa Clara, CA, United States)
Armstrong, Ernest S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
91A30084
Distribution Limits
Public
Copyright
Other

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