| 便携式红外寻的防空导弹超前修正导引规律研究与仿真 |
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| 引用本文： | 赵宇宏,朱华,任旭.便携式红外寻的防空导弹超前修正导引规律研究与仿真[J].军械工程学院学报,2008,20(6):41-44. |
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| 作者姓名： | 赵宇宏 朱华 任旭 |
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| 作者单位： | [1]军械工程学院导弹工程系,河北石家庄050003 [2]军械工程学院弹药工程系,河北石家庄050003 [3]军械工程学院科研部,河北石家庄050003 |
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| 摘 要： | 针对便携式红外寻的防空导弹瞄准点与理想命中点不重合的矛盾,提出导弹超前修正导引规律的末端修正方法,导出其数学模型和控制系统实现方法。仿真表明,简化后的导弹超前修正导引规律能够达到理想的前向偏移目的,且具有目标自适应导引（TAG）的特性。超前修正导引规律是对经典比例导引规律的修正和提升,更好地满足了便携式红外寻的防空导弹的性能指标和命中精度要求。
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| 关 键 词： | 经典比例导引规律 末端修正 超前修正导引规律 |
Simulation Research on the Lead-Correction Guidance Regulation of Portable Infrared Homing Air Defense Missile |
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| ZHAO Yu-hong,ZHU Hua,REN Xu.Simulation Research on the Lead-Correction Guidance Regulation of Portable Infrared Homing Air Defense Missile[J].Journal of Ordnance Engineering College,2008,20(6):41-44. |
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| Authors: | ZHAO Yu-hong ZHU Hua REN Xu |
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| Institution: | ZHAO Yu-hong1,ZHU Hua2,REN Xu3(1.Department of Missile Engineering 2.Department of Ammunition Engineering3.Department of Scientific Research,Ordnance Engineering College,Shijiazhuang 050003,China) |
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| Abstract: | To solve the problem that the aiming point of Portable Infrared Homing Air Defense Missile can not be kept the same as the ideal hit-point,a guidance method called lead-correction guidance regulation for correcting terminal trajectory is proposed.A Mathematics Model and the method for realizing the control system are deduced.Simulation shows that the simplification guidance regulation can satisfy the forward moving of missile trajectory and it also has a property of TAG.The lead correction guidance regulati... |
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| Keywords: | typical proportional guidance regulation terminal correction lead-correction guidance regulation |
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