NASA NTRS · 19900051305
Experimental implementation of the modified independent modal space control method
Abstract
An experimental realization of a modified independent modal space control (MIMSC) method to control the vibration of a flexible cantilevered beam is presented. In its operation the method relies on the use of one piezoelectric actuator to control several vibration modes through a time-sharing strategy. The effectiveness of the MIMSC method in damping out the beam vibration is demonstrated by comparing the results with those obtained by other modal control methods. Two methods are considered, the independent modal space control method and the pseudo-inverse method. The feasibility of the MIMSC method as a viable alternative for controlling large flexible structures with a very small number of actuators is emphasized.
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Baz, A., Poh, S.. 1990-05-22. Experimental implementation of the modified independent modal space control method. https://ntrs.nasa.gov/citations/19900051305
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