Simulation of target image tracking when thrust and velocity change abruptly

Hai Lin*, Xiaofang Wang

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

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
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 20026 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
Shanghai
时期3/11/026/11/02

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