首页 | 本学科首页   官方微博 | 高级检索  
     检索      

拦截机动目标的模糊导引律研究
引用本文:萧昌美,张福恩,尔联结.拦截机动目标的模糊导引律研究[J].航空学报,1998,19(3):299-304.
作者姓名:萧昌美  张福恩  尔联结
作者单位:1. 哈尔滨工业大学控制工程系,哈尔滨,150001
2. 北京航空航天大学自动控制系,北京,100080
摘    要: 使用模糊方法研究了三维实际追逃问题的最小能量导引律问题。首先,通过对一些状态变量的定义域进行在线模糊分区,一方面,将非线性模型变为模糊T-S线性模型;另一方面,又能方便地处理目标的任意机动而引起的目标运动方向的变化。其次,利用RH(Receding Hori-zon)控制方法和伴随技术,在目标作对抗性机动条件下,获得了一个有效拦截的导引律。数值仿真结果表明,由这种导引律导引的导弹能够精确拦截任意机动的目标。

关 键 词:三维追逃问题  最小能量导引  模糊分区  

FUZZY GUIDANCE LAW FOR INTERCEPTING MANEUVERING TARGET
Xiao Changmei ,Zhang Fuen,Er Lianjie.FUZZY GUIDANCE LAW FOR INTERCEPTING MANEUVERING TARGET[J].Acta Aeronautica et Astronautica Sinica,1998,19(3):299-304.
Authors:Xiao Changmei  Zhang Fuen  Er Lianjie
Institution:1. Department of Automatic Control, Harbin Institute of Technology, Harbin,150001;2. Department of Automatic Control,Beijing University of Aeronautics and Astronautics,Beijing,100083
Abstract:A realistic three dimensional pursuit evasion game between a missile and an aircraft is considered by the fuzzy method, which not only reduces the nonlinear model into a linear one, but also deals with the changes of the evader′s motion. Next, the study is conducted by employing the receding horizon control strategy and adjoint technique. An efficient and robust guidance law is derived, while the evader uses maneuvering strategy to avoid capture. Numerical simulation demonstrates that the missile guided by this law can intercept the randomly maneuvering evader precisely.
Keywords:pursuit  evasion problem in 3  dimensions    minimum energy guidance    fuzzy partitioning  
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号