后射空空弹的总体构想与控制律研究  

General Design and Control Law of Back-Launched Air-to-Air Missile

作　　者：王义宁[1] 姜玉宪[1] 

机构地区：[1]北京航空航天大学自动化科学与电气工程学院

出　　处：《北京航空航天大学学报》2002年第4期462-464,共3页Journal of Beijing University of Aeronautics and Astronautics

摘　　要：讨论了空空导弹后射的工程实现问题 .阐明了后射的必要性和其现实技术基础 ;分析了后射弹工程实现存在的问题 (主动段的姿态静稳定性问题 ) ;提出了解决该问题的综合技术方案 ,依据该方案建立的系统模型 ,进行了系统设计及仿真 .结果阐明 。The realization to launch air-to-air missile backward is studied.The necessity and possibility on technology are clarified.Then the issues encluded in engineering practice are analysed,such as the still stability of missile's attitude motion. A synthetic scheme to solve the essues is presented. Based on the scheme, system model is developed. The design and simulation of this system are done. The result shows it is possible to launch air-to-air missile backward.

关 键 词：空对空导弹 空战模拟 控制定律 向后发射 

分 类 号：TJ762.23[兵器科学与技术—武器系统与运用工程]