Title :
On active acceleration control of vibration isolation systems
Author :
Zhu, Wen-Hong ; Tryggvason, Bjarni
Author_Institution :
Canadian Space Agency, Saint-Hubert, Que., Canada
Abstract :
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.
Keywords :
acceleration control; aerospace control; feedback; feedforward; frequency response; vibration isolation; 22.2 Hz; active acceleration control; double integral type flotor acceleration feedback control; feedforward compensation; frequency selective filter; ground environment; ground vehicle suspensions; integral type flotor acceleration feedback control; isolation frequency; microgravity isolation mount; peak frequency responses; space shuttle; umbilical dynamics; umbilical resonant modes; vibration isolation systems; Acceleration; Control systems; Feedback control; Frequency; Land vehicles; Space shuttles; State feedback; Suspensions; Vehicle dynamics; Vibration control;
Conference_Titel :
Decision and Control, 2004. CDC. 43rd IEEE Conference on
Print_ISBN :
0-7803-8682-5
DOI :
10.1109/CDC.2004.1429437