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基于PID控制的垂直发射控制技术
引用本文:黄剑华,耿宝亮,胡云安.基于PID控制的垂直发射控制技术[J].海军航空工程学院学报,2008,23(5):513-516, 520.
作者姓名:黄剑华  耿宝亮  胡云安
作者单位:1. 海军航空工程学院控制工程系,山东烟台,264001;江西师范大学物理与通信电子学院,南昌,330000
2. 海军航空工程学院控制工程系,山东烟台,264001
摘    要:基于对PID控制的垂直发射控制技术的研究,针对导弹的垂直发射问题,文章阐述了:①建立了气动舵,推力矢量复合控制的模型;②提出了一种能够实现垂直发射快速转弯的程序弹道指令设计方法,并设计了导弹3个通道的PID控制器;③通过对弹道进行6DOF仿真分析,验证了指令和控制器设计的正确性和有效性。

关 键 词:垂直发射  气动舵/推力矢量复合控制  程序弹道  PID控制器

Vertically Launched Technology Based on PID Control
HUANG Jian-hu,GENG Bao-liang and HU Yun-an.Vertically Launched Technology Based on PID Control[J].Journal of Naval Aeronautical Engineering Institute,2008,23(5):513-516, 520.
Authors:HUANG Jian-hu  GENG Bao-liang and HU Yun-an
Institution:HUANG Jian-hua1,2,GENG Bao-liang1,HU Yun-an1 (1.Department of Control Engineering,NAAU,Yantai Sh,ong 264001,China,2.College of Physics , Communication Electronics of Jiangxi Normal University,Nanchang 330000,China)
Abstract:Based on the study of vertically launched technology using PID control, in this paper, the problems of vertical launch were solved. First, the model of integrated aerofin/thrust vector control missile was built. Second, a kind of arc trajectory design method which could achieve the quick turning of vertically launched missiles was introduced, and PID controller of three channels was designed respectively. Finally, a 6-degree trajectory simulation analysis of missile was made to validate the correctness and ...
Keywords:vertical launch  integrated aerofin/thrust vector control  procedural trajectory  PID controller  
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