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| 导弹迎击时飞机的最佳逃逸策略研究 | |
| 引用本文： | 王斯财,南英,刘经纬.导弹迎击时飞机的最佳逃逸策略研究[J].航空兵器,2009(4):28-32. |
| 作者姓名： | 王斯财 南英 刘经纬 |
| 作者单位： | 1. 南昌航空大学航机学院,江西,南昌,330063 2. 南京航空航天大学航天学院,南京,210016 3. 上海飞机设计研究所,上海,200232 |
| 基金项目： | 南昌航空大学学校创新基金 |
| 摘 要： | 研究了飞机在被导弹迎面攻击时的最佳逃逸策略。首先建立了弹-机追逃对抗飞行数学模型,提出了几种突防方案,即机动变轨技术、抛射诱饵以及综合这两种突防方案,通过大量飞行数值仿真直观地比较了各种突防策略,得出了飞机躲避导弹袭击的最佳策略——作非常规机动并且同时发射诱饵弹。 |
| 关 键 词： | 最佳逃逸策略 追逃对抗飞行 非常规机动 数值仿真 |
Optimal Escape Strategy of Fighter against Oncoming Missiles |
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| WANG Si-cai,NAN Ying,LIU Jing-wei.Optimal Escape Strategy of Fighter against Oncoming Missiles[J].Aero Weaponry,2009(4):28-32. | |
| Authors: | WANG Si-cai NAN Ying LIU Jing-wei |
| Affiliation: | 1.The Department of Aeronautical and Mechanical Engineering;Nanchang Hangkong University;Nanchang 330063;China;2.The College of Astronautics;Nanjing University of Aeronautics and Astronautics;Nanjing 210016;3.The Aircraft Institute of Shanghai;Shanghai 200232;China |
| Abstract: | The optimal escape strategy of the fighter vehicle against oncoming missile is studied.Firstly,the escape-intercept mathematic model of fighter vehicle and missile is built,and several escape strategies are presented,such as trajectory maneuver,bait technology and integration of both the two penetration strategies.Based on a great deal of flight numerical simulation,all kinds of penetration maneuver strategies are compared,and the optimal escape strategy is gotten for fighter escaping from the intercept of ... |
| Keywords: | optimal escape strategy escape-intercept counter-flight unconventional maneuver nu-merical simulation |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ | |
