DocumentCode
488246
Title
Optimization of Linear, Controlled Structures
Author
Hunziker, K.Scott ; Kraft, Raymond H. ; Kosut, Robert T. ; Armstrong, Ernest S.
Author_Institution
Boeing Aerospace and Electronics, Seattle, Washington
fYear
1990
fDate
23-25 May 1990
Firstpage
854
Lastpage
859
Abstract
This paper describes an approach for the integrated design of linear controlled structures which is being investigated as part of NASA´s Control-Structures Interaction (CSI) methodology development program. The approach is integrated in the sense that the structure and its controller are simmultaneously designed. The design methodology employs 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 stabilizing 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.
Keywords
Actuators; Aerospace electronics; Assembly; Control systems; Damping; Design methodology; Design optimization; Equations; Open loop systems; Wheels;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1990
Conference_Location
San Diego, CA, USA
Type
conf
Filename
4790851
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