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反坦克导弹导引回路设计与仿真
引用本文:刘晓侠,杨凯,严宪军.反坦克导弹导引回路设计与仿真[J].弹箭与制导学报,2009,29(6).
作者姓名:刘晓侠  杨凯  严宪军
作者单位:1. 国防科技大学航天与材料工程学院,长沙,410073;中国兵器工业第203研究所,西安,710065
2. 中国兵器工业第203研究所,西安,710065
摘    要:导引回路是导弹系统设计的重要内容之一.文中对反坦克导弹末制导段的比例导引回路进行了设计,主要包括制导滤波器设计、比例导引回路变增益补偿信号设计和阻尼回路设计.通过数字仿真计算表明了设计结果能够满足导弹末制导的要求.

关 键 词:导引回路  制导滤波器  比例导引  阻尼回路

Design and Simulation of Anti-tank Missile Guidance Loop
LIU Xiaoxia,YANG Kai,YAN Xianjun.Design and Simulation of Anti-tank Missile Guidance Loop[J].Journal of Projectiles Rockets Missiles and Guidance,2009,29(6).
Authors:LIU Xiaoxia  YANG Kai  YAN Xianjun
Affiliation:LIU Xiaoxia1,2,YANG Kai2,YAN Xianjun2 (1 College of Aerospace , Material Engineering,National University of Defense Technology,Changsha 410073,China,2 No.203 Research Institute of China Ordnance Industries,Xi'an 710065,China)
Abstract:Guidance loop is important for missile system design. In the paper,make design of an anti-tank missile proportional navigation loop of final guidance,guidance design includes guidance filter design,varying gain compensation signal in proportional navigation loop design and damping loop design. At last the digital simulation calculation result indicats that the design of the guidance loop can achieve demand of anti-tank missile final guidance.
Keywords:guidance loop  guidance filter  proportional navigation  damping loop
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