Overview

A new method was developed to design an active vibration isolation system for microgravity space experiments. This method yields the required controller transfer functions for a specified transmissibility ratio. Hence, it is a straightforward task to guarantee that the desired vibration isolation performance is achieved at each frequency. The theory for such a controller design was presented by considering a single degree of freedom system. In addition, the magnitude of the input required by the new method has been found to be less than that used by a standard phase lead/lag compensator. Sinha, Alok and Kao, Chikuan K. and Grodsinsky, Carlos M. Glenn Research Center NASA-TM-102470, E-5257, NAS 1.15:102470 NAG3-949; RTOP 694-03-03...

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