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Simultaneous structural and control optimization via linear quadratic regulator eigenstructure assignment

Authors :
Becus, G. A
Lui, C. Y
Venkayya, V. B
Tischler, V. A
Source :
NASA-Marshall Space Flight Center, The 58th Shock and Vibration Symposium, Volume 1
Publication Year :
1987
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1987.

Abstract

A method for simultaneous structural and control design of large flexible space structures (LFSS) to reduce vibration generated by disturbances is presented. Desired natural frequencies and damping ratios for the closed loop system are achieved by using a combination of linear quadratic regulator (LQR) synthesis and numerical optimization techniques. The state and control weighing matrices (Q and R) are expressed in terms of structural parameters such as mass and stiffness. The design parameters are selected by numerical optimization so as to minimize the weight of the structure and to achieve the desired closed-loop eigenvalues. An illustrative example of the design of a two bar truss is presented.

Subjects

Subjects :
Structural Mechanics

Details

Language :
English
Database :
NASA Technical Reports
Journal :
NASA-Marshall Space Flight Center, The 58th Shock and Vibration Symposium, Volume 1
Publication Type :
Report
Accession number :
edsnas.19880004240
Document Type :
Report