| 超远程制导炮弹滑翔增程弹道仿真研究 |
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| 引用本文： | 符蓓蓓,雷娟棉,王冬梅.超远程制导炮弹滑翔增程弹道仿真研究[J].兵工学报,2010(Z2). |
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| 作者姓名： | 符蓓蓓 雷娟棉 王冬梅 |
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| 作者单位： | 中国兵器科学研究院;北京理工大学宇航学院;中国兵器工业系统总体部; |
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| 摘 要： | 本文对滑翔增程的原理及弹道特性进行了分析,建立了超远程制导炮弹滑翔增程外弹道的数学模型,对最大升阻比弹道进行了仿真,从而得出理想方案弹道及实际方案弹道。对仿真结果进行了分析,并对控制环节及鸭舵外形提出了改进措施,有效解决了飞行过程中姿态角及攻角震荡的问题,保证超远程制导炮弹能够进行稳定而有效的滑翔飞行。
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| 关 键 词： | 超远程制导炮弹 滑翔增程 弹道 仿真 |
Research on Trajectory Simulation for Gliding Extended Range Guided Munitions |
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| FU Bei-bei,LEI Juan-mian,WANG Dong-mei.Research on Trajectory Simulation for Gliding Extended Range Guided Munitions[J].Acta Armamentarii,2010(Z2). |
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| Authors: | FU Bei-bei LEI Juan-mian WANG Dong-mei |
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| Affiliation: | FU Bei-bei1,LEI Juan-mian2,WANG Dong-mei3(1.Science Research Institute of China North Industries Group Corporation,Beijing 100089,China,2.School of Aerospace Engineering,Beijing Institute of Technology,Beijing 100081,3.China North System Engineering Institute,China) |
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| Abstract: | On the base of theoretic analysis of gliding extended range,a mathematic model for exterior ballistics of gliding extended range guided munitions(ERGM) was established,and the maximum lift-to-drag ratio trajectory was simulated to obtain the ideal trajectory and actual trajectory.The simulation results were analyzed,and the improvement measures for the controlling system and the canard rudder surface shape were put forward to solve the oscillation problems of attack and attitude angles,thus assure the ERGM'... |
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| Keywords: | extended range guided munitions(ERGM) gliding extended range trajectory simulation |
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