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飞机拦阻系统PID控制及Matlab实现
引用本文:赵福新,宋锦春,张志伟. 飞机拦阻系统PID控制及Matlab实现[J]. 航空计算技术, 2004, 34(2): 95-97,100
作者姓名:赵福新  宋锦春  张志伟
作者单位:东北大学,机械工程与自动化学院,辽宁,沈阳,110004;东北大学,机械工程与自动化学院,辽宁,沈阳,110004;东北大学,机械工程与自动化学院,辽宁,沈阳,110004
摘    要:主要介绍了飞机拦阻器的控制原理,并以钢缆式液压飞机拦阻系统为对象,采用线性化的方法得出系统传递函数模型,以恒加速度为控制目标设计出了PID控制器。并将该控制器应用在飞机拦阻系统的控制中,仿真结果表明,采用此控制器的控制系统具有较好的拦阻效果,可应用于我国大多数型号军用飞机的拦阻。

关 键 词:飞机阻拦  PID控制  Matlab软件  仿真
文章编号:1671-654X(2004)02-0095-03
修稿时间:2004-03-08

PID Controller Design and Numeric Simulation on the Aircraft Arresting System
ZHAO Fu-xin,SONG Jin-chun,ZHANG Zhi-wei. PID Controller Design and Numeric Simulation on the Aircraft Arresting System[J]. Aeronautical Computer Technique, 2004, 34(2): 95-97,100
Authors:ZHAO Fu-xin  SONG Jin-chun  ZHANG Zhi-wei
Abstract:The control principle of aircraft arresting system was mainly introduced. and take the wire rope hydraulic aircraft system as research object, educed the transfer function model of the system by using the method of linearization. At the same time, designed the PID controller based on the control goal of constant acceleration. And apply the controller to the control of aircraft arresting system. The simulation result indicated that the control system applied this controller possessed all right arresting effect, can be applied to most type of aircraft of homeland.
Keywords:aircraft arresting system  PID control  Matlab software  simulation
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