摘要
In terminal accelerating phase, abrupt changes of thrust and velocity of image guided missile will disturb image tracking and guidance loops in which the shooter is involved. A man-in-loop real-time simulation of tracking and guidance is taken to study this problem. The target, missile and image seeker in simulation system are expressed as mathematical models while the shooter and the controller are introduced into simulation system as hardware. Tracking error and guidance coefficient variety caused by abrupt thrust change is obtained and the stability of image tracking and trajectory is discussed.
| 源语言 | 英语 |
|---|---|
| 主期刊名 | Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai) |
| 编辑 | C. Zongij, F. Minrui, H. Guosen, P. Xiaoyuan, X. Guangleng, C. Zongji, F. Minrui, H. Guosen, P. Xiaoyuan, X. Guangleng |
| 页 | 444-447 |
| 页数 | 4 |
| 出版状态 | 已出版 - 2002 |
| 活动 | Proceedings of Asian Simulation Conference/the 5th International Conference on: System Simulation and Scientific Computing (Shanghai) - Shanghai, 中国 期限: 3 11月 2002 → 6 11月 2002 |
出版系列
| 姓名 | Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai) |
|---|
会议
| 会议 | Proceedings of Asian Simulation Conference/the 5th International Conference on: System Simulation and Scientific Computing (Shanghai) |
|---|---|
| 国家/地区 | 中国 |
| 市 | Shanghai |
| 时期 | 3/11/02 → 6/11/02 |
指纹
探究 'Simulation of target image tracking when thrust and velocity change abruptly' 的科研主题。它们共同构成独一无二的指纹。引用此
Lin, H., & Wang, X. (2002). Simulation of target image tracking when thrust and velocity change abruptly. 在 C. Zongij, F. Minrui, H. Guosen, P. Xiaoyuan, X. Guangleng, C. Zongji, F. Minrui, H. Guosen, P. Xiaoyuan, & X. Guangleng (编辑), Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai) (页码 444-447). (Proceedings of Asian Simulation Conference; System Simulation and Scientific Computing (Shanghai)).