| 后射空空弹的总体构想与控制律研究 |
| |
| 引用本文： | 王义宁,姜玉宪.后射空空弹的总体构想与控制律研究[J].北京航空航天大学学报,2002,28(4):462-464. |
| |
| 作者姓名： | 王义宁 姜玉宪 |
| |
| 作者单位： | 北京航空航天大学自动化科学与电气工程学院 |
| |
| 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.
|
| 关 键 词： | 空对空导弹 空战模拟 控制定律 向后发射 |
| 文章编号： | 1001-5965(2002)04-0462-03 |
| 收稿时间： | 2000-12-25 |
| 修稿时间： | 2000年12月25日 |
General Design and Control Law of Back-Launched Air-to-Air Missile |
| |
| WANG Yi-ning,JIANG Yu-xian.General Design and Control Law of Back-Launched Air-to-Air Missile[J].Journal of Beijing University of Aeronautics and Astronautics,2002,28(4):462-464. |
| |
| Authors: | WANG Yi-ning JIANG Yu-xian |
| |
| Institution: | Beijing University of Aeronautics and Astronautics, School of Automation Science and Electrical Engineering |
| |
| 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. |
| |
| Keywords: | air-to-air missiles air-combat simulation control law back-launched |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《北京航空航天大学学报》浏览原始摘要信息 |
| 点击此处可从《北京航空航天大学学报》下载免费的PDF全文 |
