Volume 42 Issue 9
Sep.  2016
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HUA Wenhua, MENG Qingling, ZHANG Jinpeng, et al. Differential game guidance law for dual and bounded controlled missiles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(9): 1851-1856. doi: 10.13700/j.bh.1001-5965.2015.0574(in Chinese)
Citation: HUA Wenhua, MENG Qingling, ZHANG Jinpeng, et al. Differential game guidance law for dual and bounded controlled missiles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(9): 1851-1856. doi: 10.13700/j.bh.1001-5965.2015.0574(in Chinese)

Differential game guidance law for dual and bounded controlled missiles

doi: 10.13700/j.bh.1001-5965.2015.0574
Funds:  Aeronautical Science Foundation of China (2015ZC12006)
  • Received Date: 06 Sep 2015
  • Publish Date: 20 Sep 2016
  • Due to disadvantages of single canard fin control or tail fin control for bounded-control interception missiles, a novel dual and bounded controlled differential game guidance law is presented based on two-sided optimization differential game theory. This guidance law realizes fusion of these two fin controls and optimal distribution of control commands. The differential game space of this guidance law is analyzed and the existence conditions of saddle point solution are studied from the relationships between maneuvering performance ratio and time constant ratio of the two-sided control systems. With the consideration of imperfect information scenario, a filter for target accelerations and a performance index for target interception are presented. Based on Monte Carlo method, simulations are carried out and the results show that this dual and bounded controlled guidance law has higher single shot kill probability and lower maneuvering performance requirements compared with the single-controlled scenario.

     

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