飞机拦阻系统电液比例控制研究

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2005, Vol. 26 ›› Issue (4): 520-523.

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Study on the Electro-Hydraulic Proportional Controlled Aircraft Arresting System

SONG Jin-chun¹, WANG Yan¹, ZHANG Zhi-wei¹, ZHANG Fu-bo²

1. Institute of Mechanical Engineering and Automation, Northeastern University, Shenyang 110004, China;2. The State Key Laboratory of Rolling and Automation, Northeastern University, Shenyang 110004, China

Received:2004-04-29 Revised:2005-04-21 Online:2005-08-25 Published:2005-08-25

Abstract

Abstract: On the basis of analyzing certain aircraft arresting system which is a pure mechanical and hydraulic system, an new type electro-hydraulic proportional controlled aircraft arresting system is designed. And the pressure-displacement curve is also deduced. This paper designs the pole configuration self-tuning PID controller. Simulation results indicate that the PID controller designed is able to satisfy the need of the aircraft arresting system, the dynamic and static characteristics of the system can be improved to a certain extent.

Key words: aircraft arrestment, electro-hydraulic proportional control, self-tuning PID control, pole configuration

CLC Number:

V249

SONG Jin-chun;WANG Yan;ZHANG Zhi-wei;ZHANG Fu-bo. Study on the Electro-Hydraulic Proportional Controlled Aircraft Arresting System[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2005, 26(4): 520-523.

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Study on the Electro-Hydraulic Proportional Controlled Aircraft Arresting System

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