Volume 37 Issue 4
Apr.  2011
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Sun Jian, Liu Xing, Wu Sentanget al. Guidance method of low altitude penetration missile based on optical sensor[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(4): 379-383. (in Chinese)
Citation: Sun Jian, Liu Xing, Wu Sentanget al. Guidance method of low altitude penetration missile based on optical sensor[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(4): 379-383. (in Chinese)

Guidance method of low altitude penetration missile based on optical sensor

  • Received Date: 12 Jan 2010
  • Publish Date: 30 Apr 2011
  • To increase penetration rate for low attitude cruise missile, a minimum deviation of the missile along the flight path must be satisfied, after the flight path plan to be finished. During the missile flight simulation, missile overload exceeds requirement when waypoint is switching and overshoot time becomes extended. To solve this problem, new missile guidance method for longitudinal and lateral aisles and command generated method were proposed, control law of missile was designed to satisfy requirement of the missile low attitude penetration. By way of terrain following and terrain avoidance (TF/TA) 6-degree of freedom simulation, performances of two guidance methods on TF/TA were compared. Simulation results shows that, use this new guidance method of longitudinal and lateral aisles and command generated method, TF/TA performance of missile is increased.

     

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  • [1] 王长青,李景源.一类地形跟踪控制系统方案探讨[J].战术导弹技术,1998,2:35-39 Wang Changqing,Li Jingyuan.An approach to the design of terrain following control systems[J].Tactical Missile Technology,1998,2:35-39(in Chinese) [2] 南英,彭云.一种实用的地形回避/地形跟踪算法[J].飞行力学,2006,24(4):73-75 Nan Ying,Peng Yun.An effective algorithm of terrain avoidance/terrain following[J].Flight Dynamics,2006,24(4):73-75(in Chinese) [3] Twigg S,Calise A,Johnson E.3D trajectory optimization for terrain following and terrain masking .AIAA-2006-6102,2006 [4] 钱杏芳,林瑞雄,赵亚男.导弹飞行力学[M].北京:北京理工大学出版社,2008:2-27 Qian Xingfang,Lin Ruixiong,Zhao Yanan.Missile flight dynamics[M].Beijing:Beijing Institute of Technology Press,2008:2-27(in Chinese) [5] 吴森堂,费玉华.飞行控制系统[M].北京:北京航空航天大学出版社,2005:191-255 Wu Sentang,Fei Yuhua.Flight control system[M].Beijing:Beijing University of Aeronautics and Astronautics Press,2005:191-255(in Chinese) [6] 姚宏浩,章卫国,李爱军.非线性PD控制在自动地形跟随系统中的应用[J].飞行力学,2005,23(1):73-74 Yao Honghao,Zhang Weiguo,Li Aijun.Application of the nonlinear PD controller in an autonomous terrain following flight control system[J].Flight Dynamics,2005,23(1):73-74(in Chinese) [7] 穆晓敏.多弹自主编队控制与协同航路规划方法研究 .北京:北京航空航天大学自动化科学与电气工程学院,2010 Mu Xiaomin.Methods of autonomous formation control and cooperative route planning for multi-missiles .Beijing:School of Automation Science and Electrical Engineering,Beijing University of Aeronautics and Astronautics,2010(in Chinese)
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