General Design and Control Law of BackLaunched AirtoAir Missile
-
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,实现空空导弹后射是可能的.Abstract: 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.
-
Key words:
- air-to-air missiles /
- air-combat simulation /
- control law /
- back-launched
-
[1] 高劲松,佟明安,孙隆和.越肩发射和其它攻击方式[J].电光与控制,2000(3):52~55. [2]付盛杰.F-22"猛禽"——典型第四代战斗机[M].北京:空军第八研究所,1998.
点击查看大图
计量
- 文章访问数: 2782
- HTML全文浏览量: 257
- PDF下载量: 777
- 被引次数: 0