Modal Cost Analysis for Linear Matrix-Second-Order Systems

[+] Author and Article Information
R. E. Skelton, P. C. Hughes

School of Aeronautics & Astronautics, Purdue University, West Lafayette, Ind. 47907

J. Dyn. Sys., Meas., Control 102(3), 151-158 (Sep 01, 1980) (8 pages) doi:10.1115/1.3139625 History: Received July 07, 1980; Online July 21, 2009


Reduced models and reduced controllers for systems governed by matrix-second-order differential equations are obtained by retaining those modes which make the largest contributions to quadratic control objectives. Such contributions, expressed in terms of modal data, are called “modal costs” and when used as mode truncation criteria, allow the statement of the specific control objectives to influence the early model reduction from very high order models which are available, for example, from finite element methods. The relative importance of damping, frequency and eigenvector in the mode truncation decisions are made explicit for each of these control objectives: attitude control, vibration suppression and figure control. The paper also shows that using Modal Cost Analysis (MCA) on the closed loop modes of the optimally controlled system allows the construction of reduced control policies which feedback only those closed loop modal coordinates which are most critical to the quadratic control performance criterion. In this way, the modes which should be controlled (and hence the modes which must be observable by choice of measurements), are deduced from truncations of the optimal controller.

Copyright © 1980 by ASME
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