Volume 40 Issue 2
Feb.  2014
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Yu Lei, Fu Zhaowang, Li Zhanwu, et al. Guidance and control optimization method for fighter with threat avoidance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(2): 229-234. (in Chinese)
Citation: Yu Lei, Fu Zhaowang, Li Zhanwu, et al. Guidance and control optimization method for fighter with threat avoidance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(2): 229-234. (in Chinese)

Guidance and control optimization method for fighter with threat avoidance

  • Received Date: 16 Apr 2013
  • Publish Date: 20 Feb 2014
  • Guidance method with threat avoidance was researched based on optimal control theory. Guidance model was established based on situation parameter of air combat, and fighter guidance problem was constructed as an optimal control problem with nonlinear state restriction and path restriction. Weapon effective envelope was adopted for threat description. In order to assure the safety for fighter, threat avoidance restriction was converted into state restriction based on fire threat model for target, receding horizon control (RHC) strategy was introduced for real-time requirement in guide control, and Gauss pseudospectral method (GPM) was adopted in numerical calculation for precision requirement. Simulation was given based on typical operational scenario. Result shows the guidance method can reach the optimal guidance under safety condition.

     

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