Title :
The adaptive fuzzy PID control study of active vibration isolation system
Author :
Lin Yan ; Liu Wen Ding
Author_Institution :
Dept. of Educ., Beijing Forestry Univ., Beijing, China
Abstract :
With the development of space technology, the adverse effects to the spacecraft payload caused by the inevitable vibration from electromechanical system become increasingly prominent. To effectively reduce low frequency vibration, this paper presents a design scheme which takes voice coil motor servo system as active actuator of vibration isolation platform, and for the actual vibration isolation system, it is not possible to establish a precise mathematical model, so the combination of adaptive fuzzy control and PID control are applied to the active vibration isolation system based on voice coil motor. Simulation results show that the self-adaptive fuzzy PID control system has a good stability and anti-jamming capabilities, could isolate external vibration interference in a very wide frequency range, provides new and reasonable control ideas for the complex conditions and high index of control systems.
Keywords :
actuators; adaptive control; aerospace control; fuzzy control; self-adjusting systems; three-term control; vibration isolation; active actuator; active vibration isolation system; adverse effect; antijamming capability; design scheme; electromechanical system; external vibration interference isolation; self-adaptive fuzzy PID control system; spacecraft payload; stability; voice coil motor servo system; Decision support systems; Hafnium; Active actuator; Active vibration isolation system; Adaptive fuzzy PID control; Voice coil motor;
Conference_Titel :
Intelligent Control and Automation (WCICA), 2012 10th World Congress on
Conference_Location :
Beijing
Print_ISBN :
978-1-4673-1397-1
DOI :
10.1109/WCICA.2012.6358048