Impact of space rotation on shell miss distances for serpentine flight path maneuvering

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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.

Keywords serpentine maneuvers penetration probability miss distance shell flight time

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V249.122+.3文献标识码:A

Issue Date: 15 August 2015

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	FU Qiang
	ZHU Jihong
	WANG Chunping

Cite this article:

FU Qiang,ZHU Jihong,WANG Chunping. Impact of space rotation on shell miss distances for serpentine flight path maneuvering[J]. Journal of Tsinghua University(Science and Technology), 2015, 55(8): 884-888.

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http://jst.tsinghuajournals.com/EN/ OR http://jst.tsinghuajournals.com/EN/Y2015/V55/I8/884

[1] Zarchan P. Tactical and Strategic Missile Guidance [M]. 3rd ED. Reston VA: AIAA Inc, 1997.
[2] 顾文锦, 赵红超, 王凤莲. 反舰导弹末端机动的突防效果研究 [J]. 宇航学报, 2005, 26(6): 758-761.GU Wenjin, ZHAO Hongchao, WANG Fenglian. Research on the penetration effect of terminal maneuver for anti-ship missiles [J]. Journal of Astronautics, 2005, 26(6): 758-761. (in Chinese)
[3] 范作娥, 顾文锦, 姜鹏, 等. 基于蒙特卡洛法的反舰导弹末端机动突防效果研究 [J]. 海军航空工程学院学报, 2010, 25(3): 241-246.FAN Zuoe, GU Wenjin, JIANG Peng, et al. Research on penetration effect of terminal maneuver for anti-ship missile based on Monte Carlo method [J]. Journal of Naval Aeronautical and Astronautically University, 2010, 25(3): 241-246. (in Chinese)
[4] Ohlmeyer E J. Root-mean-square miss distance of proportional navigation missile against sinusoidal target [J]. Journal of Guidance, Control, and Dynamics, 1996, 19(3): 563-568.
[5] Ryoo C K, Whang I H, Tahk M J. 3-D evasive maneuver policy for anti-ship missiles against close-in weapon systems [C]// AIAA Guidance, Navigation, and Control Conference and Exhibit. Austin, Texas, USA: AIAA Inc, 2003: 1-7.
[6] 武志东, 顾文锦, 毕兰金. 反舰导弹最优末端蛇形机动策略 [J]. 战术导弹技术, 2011(3): 1-5.WU Zhidong, GU Wenjin, BI Lanjin. Optimal terminal weaving maneuver strategy for anti-ship missile [J]. Tactical Missile Technology, 2011(3): 1-5. (in Chinese)
[7] 冯元伟, 金振中, 郜彪. 导弹蛇形机动与摆式机动突防反导舰炮仿真 [J]. 导弹防御技术, 2010, 38(4): 22-25, 52. FENG Yuanwei, JIN Zhenzhong, GAO Biao. Simulation of penetration of horizontal S maneuver and cycloid maneuver against antimissile naval gun [J]. Modern Defense Technology, 2010, 38(4): 22-25, 52. (in Chinese)
[8] 王海斌, 江言林. 脱靶量在反舰导弹“蛇形机动”突防中的应用分析 [J]. 舰船电子工程, 2010, 30(12): 33-34, 90.WANG Haibin, JIANG Yanlin. Appliance investigation of the miss distance of ship to air missile in zigzag course of anti-ship missile [J]. Ship Electronic Engineering, 2010, 30(12): 33-34, 90. (in Chinese)
[9] Zarchan P. Proportional navigation and weaving targets [J]. Journal of Guidance, Control and Dynamics, 1995, 18(5): 969-974.
[10] Lee J I, Ryoo C K, Choi K. A guidance law with sinusoidal evasive maneuver for enhancing survivability of anti-ship missiles [J]. Automatic Control in Aerospace, 2007, 17(1): 804-809.
[11] 冯元伟, 夏小华, 吴艳征. 导弹两种蛇形机动对反导舰炮突防效果比较 [J]. 火力与指挥控制, 2011, 36(8): 107-109, 113.FENG Yuanwei, XIA Xiaohua, WU Yanzheng. Comparison of penetration effect of two kinds of S maneuver missile against anti-missile naval gun [J]. Fire Control & Command Control, 2011, 36(8): 107-109, 113. (in Chinese)
[12] 张贤椿. 高炮火控系统各子系统间信息传递的优化技术[D]. 南京: 南京理工大学博士学位论文, 2009.ZHANG Xianchun. Optimization Techniques of Information Transmission Between the Subsystems of Fire Control System [D]. Nanjing: Nanjing University of Science & Technology, 2009. (in Chinese)
[13] 肖元星, 张冠杰. 地面防空武器系统效费分析 [M]. 北京: 国防工业出版社, 2006.XIAO Yuanxing, ZHANG Guanjie. Effectiveness Cost Analysis on Land-based Air Defense Weapon System [M]. Beijing: National Defense Industry Press, 2006. (in Chinese)
[14] 张科南, 周浩, 陈万春. 超声速飞行器多约束多种机动突防模式弹道规划 [J]. 弹道学报, 2012, 24(3): 85-90.ZHANG Kenan, ZHOU Hao, CHEN Wanchun. Trajectory planning for hypersonic vehicle with multiple constraints and multiple maneuvering penetration strategies [J]. Journa1 of Ballistics, 2012, 24(3): 85-90. (in Chinese)
[15] 邵振星. 机动目标虚拟闭环校射原理研究[D]. 南京: 南京理工大学硕士学位论文, 2008.SHAO Zhenxing. Research of the Principle of Fictitious Closed-loop Amending for Maneuvering Targets [D]. Nanjing: Nanjing University of Science & Technology, 2008. (in Chinese)