Journal of Systems Engineering and Electronics ›› 2011, Vol. 33 ›› Issue (3): 627-632.doi: 10.3969/j.issn.1001-506X.2011.03.32

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Differential game guidance law for dual control missiles

HUA Wen-hua, CHEN Xing-lin   

  1. School of Astronautics, Harbin Institute of Technology, Harbin 150001, China
  • Online:2011-03-21 Published:2010-01-03

Abstract:

According to the disadvantages of single canard fin control or tail fin control, a novel dual control differential game guidance law is presented based on twosided optimization game theory to realize the fusion of these two control methods. The differential game space of this guidance law is analyzed and the existence conditions of saddle point solutions for perfect interception scenario and non perfect interception scenario are researched . With the consideration of noisy measurements, an estimator and a performance index are designed. Based on Monte Carlo simulation, the results show that this dual control guidance law has better target interception performance and higher single shot kill probability as compared with the single control scenarios.

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