火力与指挥控制2011，Vol.8Issue(8)：122-125,4.
逆系统空空导弹控制器设计
Design of Controller Based on Inverse System for Air-to-Air Missile
摘要
Abstract
Using the inverse system method in nonlinear control,a controller is designed for a missile dynamics system of the centroid motion.In order to realize the attack of the target,the output information of the control system including velocity,trajectory inclination and declination can track the guidance command through the control of the tangential and normal overloading of the missile in the trajectory coordinate.Simulation results show that the centroid motion parameters can quickly track the guidance command with rather high precision.关键词
逆系统/空空导弹/动力学系统/渐近无差跟踪Key words
inverse system/air-to-air missile/dynamics system/no error progressive tracking分类
武器工业引用本文复制引用
何素娟,周凤岐..逆系统空空导弹控制器设计[J].火力与指挥控制,2011,8(8):122-125,4.基金项目
国家自然科学基金 （）
教育部新世纪人才支持计划基金资助项目 （）
