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NASA NTRS · 19870046439

A comparison of active vibration control techniques - Output feedback vs optimal control

Abstract

The paper presents analytical and experimental comparison of two control laws for a laboratory structure designed to simulate large space structures. The first control law is the standard linear quadratic law, which is optimal but requires model reduction for practical implementation. The second control law is a new simple direct feedback control law designed to minimize control forces while guaranteeing stability. The optimal control law was found to be only slightly better than the direct feedback law even in terms of the quadratic performance index. Moreover, the optimal control law provided almost no margin of stability for the unmodeled modes while the direct feedback law provided significant stability margins to all modes. The above results were verified experimentally using a digital implementation of the control laws. Excellent agreement between the analytical prediction and experimental measurements was observed.

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BibTeXRIS

Martinovic, Zoran N., Haftka, Raphael T., Hallauer, William L., Jr., Schamel, George C., II. 1987-01-01. A comparison of active vibration control techniques - Output feedback vs optimal control. https://ntrs.nasa.gov/citations/19870046439

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