DocumentCode
2729262
Title
Optimal control of large space structures via generalized inverse matrix
Author
Nguyen, Charles C. ; Fang, Xiaowen
Author_Institution
Dept. of Electr. Eng., Catholic Univ. of America, Washington, DC, USA
fYear
1988
fDate
0-0 1988
Firstpage
652
Lastpage
656
Abstract
Independent modal space control (IMSC) is a control scheme that decouples the space structure into n controlled modes and second-order subsystems according to n controlled modes and controls each mode independently. It is well known that IMSC eliminates control and observation spillover caused when the conventional coupled modal control scheme is used. The independent control of each mode requires that the number of actuators be equal to the number of modeled modes, which is very high for a faithful modelling of large space structures. The authors propose a control scheme that allows one to use a reduced number of actuators to control all modeled modes suboptimally. In particular, the method of generalized inverse matrices is used to implement the actuators so that the eigenvalues of the closed-loop system are as closed as possible to those specified by the optimal IMSC. Computer simulation of the proposed control scheme on a simply supported beam is given.<>
Keywords
aerospace control; closed loop systems; large-scale systems; matrix algebra; optimal control; aerospace control; closed-loop system; eigenvalues; independent modal space control; inverse matrix; large space structures; optimal control; Actuators; Attitude control; Eigenvalues and eigenfunctions; Filters; Optimal control; Shape control; Space exploration; Space shuttles; State estimation; State feedback;
fLanguage
English
Publisher
ieee
Conference_Titel
System Theory, 1988., Proceedings of the Twentieth Southeastern Symposium on
Conference_Location
Charlotte, NC, USA
ISSN
0094-2898
Print_ISBN
0-8186-0847-1
Type
conf
DOI
10.1109/SSST.1988.17129
Filename
17129
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