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带末端角度约束的空地反辐射导弹被动制导律

Passive guidance law for air-to-ground anti-radiation missile with terminal angular constraint
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摘要 针对被动跟踪问题,结合UKF和PF滤波各自优点,采用了UPF滤波器对弹目相对运动信息进行了精确估计。针对滤波器估计过程中,对系统状态可观测性的要求,在分析了系统可观测条件的基础上,结合空地反辐射导弹特点,设计了一种带末端角度约束,且能够增强系统状态可观测性的被动制导律。仿真结果表明,UPF滤波器结合所设计的被动制导律能有效准确地估计弹目相对运动信息,实现了精确制导,同时能有效地约束末端攻击角度,保证了空地反辐射导弹的杀伤效果。 For passive tracing problem,combined with the advantages of UKF and PF filters,an UPF filter was adopted to realize the accurate estimation of the information of missile-target relative movement. For the requirement of the observability of system states during estimating,combined with the characteristic of air-to-ground anti-radiation missile,a passive guidance law with terminal angular constraint and observability enhancement was designed. The simulation result shows that the UPF filter combined with the designed passive guidance law can estimate the relative information accurately and effectively and realize accurate guidance. Meanwhile,with effective terminal angular constraint,the damage effect of the missile is guaranteed.
出处 《固体火箭技术》 EI CAS CSCD 北大核心 2016年第4期594-600,共7页 Journal of Solid Rocket Technology
基金 航空科学基金(20140196004) 航空科学基金(20130196004)
关键词 末端角度约束 UPF滤波 滑模制导律 被动制导 terminal angular constraint UPF filter sliding mode guidance passive guidance
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  • 1宋建梅,张天桥.用于被动寻的导弹的带末端落角约束的变结构导引律[J].Chinese Journal of Aeronautics,2001,14(2):83-87. 被引量:27
  • 2刘小刚,宋凯.攻击机动目标的最优导引规律[J].空军工程大学学报(自然科学版),2002,3(1):18-21. 被引量:3
  • 3孙未蒙,郑志强.一种多约束条件下的三维变结构制导律[J].宇航学报,2007,28(2):344-349. 被引量:14
  • 4刘健,刘忠,玄兆林.方位时延的TMA算法及其可观测性研究[J].声学技术,2007,26(3):371-375. 被引量:6
  • 5Zhang Y,Hu Y,Gu W.Lyapunov stability based on three-dimensinal guidance for missiles against maneuvering targets[C]// World Congress on Intelligent Control and Automation,2002:2836-2840.
  • 6Kim B S,Lee J G,Han H S.Biased PNG law for impact with angular constraint[J].IEEE Transactions on Aerospace and Electronic Systems,1998,34(1):277-288.
  • 7Dimirovski G M,Deskovski S M,Gacovski Z M.Classical and fuzzy-system guidance laws in homing missiles systems[C]//IEEE Aerospace Conference Proceedings,2004:3032-3047.
  • 8Lin C,Hung H,Chen Y.Development of an integrated fuzzy-logic-based missile guidance law against high speed target[J].IEEE Transactions on Fuzzy Systems,2004,12(2):157-169.
  • 9HEPNER S A R, GEERING H P. Observability analysis for target maneuver estimation via bearing-only and bearingrateonly measurements[J]. AIAA Journal of Guidance, Control and Dynamics, 1990,13(6) : 977- 983.
  • 10HULL D G, SPEYER J I.. Linear-quadratic guidance law for dual control of homing missiles [J]. A1AA Journal of Guidance,Control,and Dynamics,1990,13(1):137-144.

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