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带有碰撞角约束的三维纯比例导引律研究 被引量:11

Study on Three-Dimensional PPN with Impact Angle Constraints
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摘要 为提高制导武器在目标区域的生存能力,增大对目标的杀伤威力,以及实际战术应用的需要,需要武器按期望的方位角、俯冲角对目标实施攻击,因此提出了带有碰撞角约束的导引问题。针对此问题,借鉴TV-BPN的基本思想,在三维空间中重新设计偏置项,来同时约束俯仰与偏航碰撞角,提出了带有碰撞角约束的三维纯比例导引律(3DPPNGL/IAC)。并对3DPPNGL/IAC下的理想弹道进行了数字仿真,结果证明,在能捕捉到目标的同时,也能够对碰撞俯仰角、偏航角同时进行控制。 For improving the survivability of the guided weapons in target district, aggrandizing its damaging power to target, and to satisfy the demand of the actual military tactics, the guided weapon must attack targets in the desired impact angle, thus the problem of homing guidance with impact angle constraints is put forward. Aiming at this problem, by using the basic thought of the TV-BPN and redesigning the biased item in the 3D space, the authors presented the three-dimensional Pure Proportional Navigation Guidance Law with Impact Angle Constraints (3DPPNGL/IAC) in order to realizing constraints of impact angle. The numerical simulation of ideal trajectory proved that impact angle of both pitching and yawing could be controlled at the time of target could be caught.
出处 《电光与控制》 北大核心 2009年第5期9-12,共4页 Electronics Optics & Control
关键词 制导武器 制导律 三维空间 纯比例导引 碰撞角约束 偏置比例导引 guided weapon guidance law 3D space Pure Proportional Navigation (PPN) impact angle constraints BPN
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参考文献11

  • 1KIM M, GRIDER K V. Terminal guidance for impact attitude angle constrained flight trajectories[J]. IEEE Trans Aerosp Electron Syst, 1973,9 (6) : 852 -859.
  • 2YORK R J, PASTRICK H L. Optimal terminal guidance with constraints at final time [ J ]. Journal of Spacecraft and Rockets, 1977, 14:381 -382.
  • 3BRYSON A E, HO Y C. Applied optimal control [ M]. Washington, DC : Hemisphere, 1975 : 154 -155.
  • 4SONG T L, SHIN S J, CHOL H. Impact angle control for planar engagements [ J ]. IEEE Trans Aerosp Electron Syst, 1999,35 (4) : 1439 -1444.
  • 5RYOO C K,CHO H,TAHK M J. Time to go weighted optimal guidance with impact angle constraints [ J ]. IEEE Transactions on Control Systems Technology, 2006, 14 (3) :483.492.
  • 6RYOO C K, CHO H ,TAHK M J. Optimal guidance laws with terminal impact angle constraint [ J ]. Journal of Guidance, Control and Dynamics,2005,28 (4) : 724 -732.
  • 7RYOO C K,CHO H,TAHK M J. Closed form solutions of optimal guidance with terminal impact angle constraint [ C ]//Proceedings of IEEE Conference on Control Applications Istanbul, Turkey,2003:504 -509.
  • 8KIM B S, LEE J G, HAN H S. Biased PNC law for impact with angular constraint [ J ]. IEEE Transactions on Aerospace and Electronic Systems, 1998,34( 1 ) :277-288.
  • 9DAS P G, PADHI R P. Nonlinear suboptimal missile guidance with terminal impact angle constrain:a model predictive static programming approach [ C ]//Proceedings of the International Conference on Advances in Control and Optimization of Dynamical Systems (ACODS2007) :344 -351.
  • 10KIM Y M, SEO J H. The realization of the three dimensional guidance law using modified augmented proportional navigation [ C ]//Proceedings of the 35th Conference on Decision and Control, Kobe, Japan, 1996 (3) :

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