期刊文献+

基于目标加速度方向观测的微分对策制导律 被引量:3

Differential Games Guidance Law with Observation of Target’s Acceleration Orientation
下载PDF
导出
摘要 针对延迟信息条件下的机动目标拦截问题,研究了一种考虑目标加速度方向观测的微分对策制导律。首先,针对引入目标方向观测信息末制导博弈问题,建立了微分对策数学模型。随后,利用状态依赖黎卡提方程求解微分对策问题,得到包含无延迟目标机动项的微分对策制导律,可以更为有效地拦截机动目标。最后,在延迟信息条件下,利用目标加速度方向观测的方法补偿延迟的目标加速度,再将补偿后的目标加速度信息取代无延迟的目标加速度,得到延迟信息条件下考虑目标加速度方向观测的微分对策制导律。仿真结果表明,新的制导律可以在延迟信息条件下有效地拦截机动目标。 For the problem of intercepting a maneuvering target with delayed information,a differential-games based guidance law with observation of target’s acceleration orientation is studied.First,for the problem of terminal differential games guidance with observation of target’s acceleration orientation,the model of the differential games guidance is built.Then,the differential game is solved by the way of state-dependent Riccati equation.A differential-games based guidance law with target’s acceleration is achieved,which intercepts maneuvering targets better.Finally,under assumptions of delayed target acceleration,by the way of observing target’s acceleration orientation,a more accurate target acceleration is achieved.Replacing the target’s acceleration with no delay with compensated acceleration,a differential-games based guidance law with observation of target’s acceleration orientation is achieved.The simulation results shows that the new guidance law can intercepts maneuvering targets better with delayed target’s acceleration.
作者 许佳骆 胥彪 冯建鑫 张金鹏 XU Jialuo;XU Biao;FENG Jianxin;ZHANG Jinpeng(Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;China Airborne Missile Academy,Luoyang 471009,China;Aviation Key Laboratory of Science and Technology on Airborne Guided Weapons,Luoyang 471009,China)
出处 《宇航总体技术》 2021年第1期27-36,共10页 Astronautical Systems Engineering Technology
基金 国家自然科学基金(61603183)
关键词 制导 微分博弈 状态依赖黎卡提方程 延迟信息 加速度方向观测 Guidance Differential games State-dependent Riccati equation Delayed information Observation of acceleration orientation
  • 相关文献

参考文献1

二级参考文献37

  • 1刘智平,周凤岐,周军.战术导弹现代自动驾驶仪设计方法综述[J].航天控制,2006,24(5):91-96. 被引量:13
  • 2Buschek Harald.Full envelope missile autopilot design using gain scheduled robust control[J].Journal of Guidance,Control,and Dynamics,1999,22(1):115-124. 被引量:1
  • 3Cloutier J R.State-dependent riccati equation techniques:an overview[C].New Mexico:American Control Conference,1997:932-936. 被引量:1
  • 4Bogdanov Alexander,Wan Eric.SDRE control with nonlinear feedforward compensation for a small unmanned helicoper[C].San Diego,California:2nd AIAA "Unmanned Unlimited" Systems,Technologies,and Operations.AIAA 2003-6512,2003. 被引量:1
  • 5Katsev Sergey.Streamlining of the state-dependent Riccati equation controller algorithm for an embedded implementation[D].Rochester:Rochester Institute of Technology,2006:42-80. 被引量:1
  • 6Erdem Evrin B,Alleyne Andrew G.Design of a class of nonlinear controllers via state dependent Riccati equations[J].IEEE Transactions on Control Systems Technology,2004,12(1):133-137. 被引量:1
  • 7Pearson J D.Approximation Methods in Optimal Control[J].Journal of Electronics and Control,1962,13(2):453-465. 被引量:1
  • 8Cloutier J R,D'Souza C N,Mracek C P.Nonlinear regulation and nonlinear H control via the state-dependent Riccati equation techniques:Part 1,theory[C].Baytona Beach,FL:1st International Conference on Nonlinear Problems in Aviation and Aerospace,1996:117-130. 被引量:1
  • 9Cloutier J R,D'Souza C N,Mracek C P.Nonlinear regulation and nonlinear H control via the state-dependent Riccati equation techniques:Part 2,examples[C].Baytona Beach,FL:1st International Conference on Nonlinear Problems in Aviation and Aerospace,1996:131-142. 被引量:1
  • 10Stansbery Donald T,Cloutier J R.Nonlinear control of satellite formation flight[C].AIAA Guidance,Navigation,and Control Conference and Exhibit,Denver,CO.AIAA 2000-4436,2000. 被引量:1

共引文献3

同被引文献29

引证文献3

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部