航空学报 > 1998, Vol. 19 Issue (3): 299-304

拦截机动目标的模糊导引律研究

萧昌美1, 张福恩1, 尔联结2   

  1. 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
  • 收稿日期:1997-06-16 修回日期:1998-02-11 出版日期:1998-06-25 发布日期:1998-06-25

FUZZY GUIDANCE LAW FOR INTERCEPTING MANEUVERING TARGET

Xiao Changmei1, Zhang Fuen1, Er Lianjie2   

  1. 1. Department of Automatic Control, Harbin Institute of Technology, Harbin,150001;2. Department of Automatic Control,Beijing University of Aeronautics and Astronautics,Beijing,100083
  • Received:1997-06-16 Revised:1998-02-11 Online:1998-06-25 Published:1998-06-25

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

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.

Key words: pursuit- evasion pr oblem in 3-dimensions, minimum ener gy guidance, fuzzy partitioning

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