Vibration isolation systems (VIS) have appeared in applications ranging from space shuttle applications to ground vehicle suspensions. In this paper, the significant advantage of using I (integral) and II (double integral) type flotor acceleration feedback control together with feedforward compensation of the umbilical dynamics is analyzed theoretically and is also demonstrated experimentally with respect to a typical system, namely a microgravity isolation mount (MIM) operated in the ground environment. The lowest isolation frequency is reduced by about 40 times with a sufficiently improved vibration isolation performance up to 10 Hz, compared to a conventional PID controller. A unique frequency selective filter (FSF) is proposed to suppress the peak frequency responses caused by umbilical resonant modes. The effectiveness of the FSF is demonstrated experimentally with a 20 dB attenuation at 22.2 Hz.
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