Application of self-adaptive fuzzy PID technology in launch site gas supply system

被引:0
作者
Yang Yiqi [1 ]
Liu Haoyang [2 ]
Yue Longhua [3 ]
Wang Tianhang [4 ]
机构
[1] Air Force Engn Univ, Sch Air & Missile Def, Xian 710051, Shaanxi, Peoples R China
[2] Air Force Engn Univ, Sch Informat & Nav, Xian 710000, Shaanxi, Peoples R China
[3] Unit 93658 PLA, Beijing 100144, Peoples R China
[4] Unit 63723 PLA, Xinzhou 036304, Peoples R China
关键词
injection gas supply; fuzzy control; PID; data fitting; system modeling; simulation;
D O I
10.16708/j.cnki.1000-758X.2019.0022
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Aiming at the problems of nonlinear pressure control, large time-lag and variable parameters, a closed loop pressure control system is designed based on self-adaption fuzzy PID technology. By online adjusting of the proportional coefficient K-p, the integral coefficient K-i and the differential coefficient K-d of the controller, high precision control of the pressure is realized. Based on the test data, a second-order lag inertia model is established by curve fitting and simulation. The simulation verifies the validity of the model. The conclusion shows that this control effect is better than the conventional PID control, and can effectively improve performance and steady-state accuracy of the system. It can be widely used in the automatic control system of the launch site where PLC control is a core method.
引用
收藏
页码:81 / 87
页数:7
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