This article presents the application of the fuzzy logic (FL) concept
to the active control of a multiple degree of freedom reaction compens
ating platform system that is designed and used for isolation vibrator
y disturbances of space-based devices. the physical model used is a sc
aled down two-plate platform system. In this work, simulation is perfo
rmed and presented. According to the desired performance specification
s, a full range of investigation regarding the development of an FL st
abilization controller for the system is conduced. Specifically, the s
tudy includes four stages: comprehensive dynamic modeling of the react
ion compensating system; analysis of the dynamic responses of the plat
form system when it is subjected to various disturbances; dynamic resp
onses of the platform system when it is subjected to various disturban
ces; design of an FL controller capable of filtering the vibratory dis
turbances transmitted to the bottom plate of the platform system; perf
ormance evaluation of the developed FL controller through computer sim
ulations. To simplify the simulation work, the system model is lineari
zed and the system component parameter variations are not considered.
The performance of the FL controller is tested by exciting the system
with an impulsive force applied at an arbitrarily chosen point on the
top plate. It is shown that the proposed FL controller is robust in th
at the resultant active system is well stabilized when subjected to a
random external disturbance. The comparative study of the performances
of the FL controlled active reaction and passive reaction compensatin
g systems also reveals that the FL controlled system achieves signific
ant improvements in reducing vibratory accelerations over passive syst
ems. (C) 1995 John Wiley & Sons, Inc.