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清华大学学报(自然科学版)  2015, Vol. 55 Issue (8): 884-888    
  计算机科学与技术 本期目录 | 过刊浏览 | 高级检索 |
蛇形机动目标航迹旋转对射弹脱靶量的影响
付强1,2, 朱纪洪1, 王春平2
1. 清华大学 计算机科学与技术系, 北京 100084;
2. 军械工程学院, 石家庄 050003
Impact of space rotation on shell miss distances for serpentine flight path maneuvering
FU Qiang1,2, ZHU Jihong1, WANG Chunping2
1. Department of Computer Science and Technology, Tsinghua University, Beijing 100084, China;
2. Mechanical Engineering College, Shijiazhuang 050003, China
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摘要 结合蛇形机动目标对抗舰炮或高炮的作战过程, 定义了航迹直角坐标系和航迹旋转角, 在最小二乘法下建立了一次假定和二次假定的平滑滤波模型, 推导出目标运动参数、理想弹着点和射弹脱靶量的函数关系式, 证明了航迹旋转并不影响目标运动参数的求取, 但是能够引起射弹脱靶量的变化, 其原因在于理想弹着点位置的旋转影响了射弹飞行时间。若此因素可忽略, 则旋转角度与脱靶量无关。对主运动方向指向炮位原点的目标进行了仿真, 验证了上述结论。
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付强
朱纪洪
王春平
关键词 蛇形机动突防概率脱靶量射弹飞行时间    
Abstract:Targets maneuver along serpentine paths to avoid naval or antiaircraft gun fire. A method was developed to track a target's path and identify the target's rectangular coordinates and rotation angles. Least square filter models are then defined assuming first-order and second-order motion to predict the target motion, bomb impact points and shell miss distances in functional forms. Rotations of the flight path do not affect the filtered parameters for the target motion, but do affect the miss distance. Rotations of the bomb impact point change the shell's flight time. If the change in the flight time is ignored, the miss distance and the rotations do not affect the calculations. Finally, targeting of gun emplacements was simulated to verify the conclusions.
Key wordsserpentine maneuvers    penetration probability    miss distance    shell flight time
收稿日期: 2013-10-23      出版日期: 2015-08-15
ZTFLH:  V249.122+.3文献标识码:A  
通讯作者: 朱纪洪,教授,E-mail:jhzh@tsinghua.edu.cn     E-mail: jhzh@tsinghua.edu.cn
引用本文:   
付强, 朱纪洪, 王春平. 蛇形机动目标航迹旋转对射弹脱靶量的影响[J]. 清华大学学报(自然科学版), 2015, 55(8): 884-888.
FU Qiang, ZHU Jihong, WANG Chunping. Impact of space rotation on shell miss distances for serpentine flight path maneuvering. Journal of Tsinghua University(Science and Technology), 2015, 55(8): 884-888.
链接本文:  
http://jst.tsinghuajournals.com/CN/  或          http://jst.tsinghuajournals.com/CN/Y2015/V55/I8/884
  图1 大地直角坐标系和目标直角坐标系
  图2 垂直机动脱靶量时变曲线
  图3 改变α时的仿真结果
  图4 改变β 时的仿真结果
  图5 改变ε 时的仿真结果
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