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目标威胁规避约束下战斗机引导控制优化方法

于雷 付昭旺 李战武 李飞

于雷, 付昭旺, 李战武, 等 . 目标威胁规避约束下战斗机引导控制优化方法[J]. 北京航空航天大学学报, 2014, 40(2): 229-234.
引用本文: 于雷, 付昭旺, 李战武, 等 . 目标威胁规避约束下战斗机引导控制优化方法[J]. 北京航空航天大学学报, 2014, 40(2): 229-234.
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)

目标威胁规避约束下战斗机引导控制优化方法

基金项目: 国家自然科学基金资助项目(61172083);航空科学基金资助项目(20095196012)
详细信息
  • 中图分类号: V271.4

Guidance and control optimization method for fighter with threat avoidance

  • 摘要: 基于最优控制理论对威胁规避约束下战斗机引导控制方法进行研究.以空战态势参数为状态建立战斗机引导模型,以引导的快速性和经济性为性能指标,将战斗机引导问题建模为具有非线性状态约束和路径约束的最优控制问题,以武器攻击包线来描述目标火力威胁,并将威胁规避约束转化为引导过程的空战态势约束问题,为保证引导算法的实时性和有效性,引入滚动时域控制策略进行在线优化,并采用高斯伪谱法进行数值求解,基于典型作战场景进行仿真,结果表明所提出的引导控制方法能在保证引导安全性的前提下实现战斗机的最优引导.

     

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出版历程
  • 收稿日期:  2013-04-16
  • 网络出版日期:  2014-02-20

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