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
Link To Document :
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