Design and Simulation of Controller for Hyper Velocity Kinetic Energy Missile

作     者：康长赓 雷成 刘藻珍 KANG Chang-geng;LEI Cheng;LIU Zao-zhen

作者机构：北京理工大学机电控制工程系北京100081 中国科学院自动化所北京100080 

出 版 物：《Journal of Beijing Institute of Technology》 (北京理工大学学报（英文版）)

年 卷 期：2000年第9卷第1期

页      码：107-112页

摘      要：The controller design and digital simulation for the hyper velocity kinetic energy missile is investigated. A mathematical model of the trajectory deviation from the line of sight was established, the guidance closed loop was compensated with a phase advance lag corrective network, a selecting algorithm of the attitude control motors used to steer the missile s attitude was presented. In the presence of a wide variety of disturbances the results of digital simulation are satisfactory to circular error probability(CEP) being less than 0 5?m. The steering scheme utilizing attitude control motors as actuators to control the attitude of the missile is feasible.

主 题 词：hyper velocity missile guidance missile control attitude control motor simulation 

学科分类：0810[工学-土木类] 08[工学] 082601[082601] 082501[082501] 0826[工学-生物医学工程类] 0805[工学-能源动力学] 082602[082602] 0825[工学-环境科学与工程类] 0812[工学-测绘类] 

核心收录：

D　O　I：10.3969/j.issn.1004-0579.2000.01.019

馆 藏 号：203211045...