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PID Controller Optimization by GA an

時(shí)間:2023-04-28 13:46:31 航空航天論文 我要投稿
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PID Controller Optimization by GA and Its Performances on the Electro-hydraulic Servo Control System

A proportional integral derivative (PID) controller is designed and attached to electro-hydraulic servo actuator system (EHSAS) to control the angular position of the rotary actuator which control the movable surface of space vehicles. The PID gain parameters areoptimized by the genetic algorithm (GA). The controller is verified on the new state-space model of servo-valves attached to the physical rotary actuator by SIMULINK program. The controller and the state-space model are verified experimentally. Simulation and experimental results verify the effectiveness of the PID controller adaptive by GA to control the angular position of the rotary actuator as compared with the classical PID controller and the compensator controller.

作 者: Karam M. Eibayomy Jiao Zongxia Zhang Huaqing   作者單位: School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China  刊 名: 中國(guó)航空學(xué)報(bào)(英文版)  ISTIC 英文刊名: CHINESE JOURNAL OF AERONAUTICS  年,卷(期): 2008 21(4)  分類號(hào): V2  關(guān)鍵詞: PID controller   electro-hydraulic servo control system   genetic controller   GA  

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