水下微分对策协同拦截制导策略

刘卫东;程瑞锋;高立娥;张建军

兵工学报 ›› 2016, Vol. 37 ›› Issue (9) : 1684-1691.

兵工学报 ›› 2016, Vol. 37 ›› Issue (9) : 1684-1691. DOI: 10.3969/j.issn.1000-1093.2016.09.019
论文

水下微分对策协同拦截制导策略

  • 刘卫东1,2, 程瑞锋1, 高立娥1,2, 张建军1
作者信息 +

Cooperative Engagement-based Differential Guidance Law for Underwater Interceptor

  • LIU Wei-dong1,2, CHENG Rui-feng1, GAO Li-e1,2, ZHANG Jian-jun1
Author information +
文章历史 +

摘要

为提高对未知目标的拦截能力,基于博弈理论,研究了一种由水下拦截器和我方舰艇协同防卫来袭目标的微分制导策略。该策略在三方对策关系基础上,结合视线指令构造协同约束,建立三方自导约束模型,以终端脱靶量和最小能量为性能指标进行协同对策制导律设计。利用伴随原理解决终端问题方法导出具有反馈控制的“零效脱靶量”,并以滚动时域法对制导参数进行实时预测。通过对可捕获条件下不同制导方式来袭目标的拦截仿真表明:在相同条件下,该制导策略弹道性能良好,不受目标机动形式的限制,具有较强的鲁棒性和稳定性。

Abstract

A differential game guidance law based on game theory is developed for the underwater interceptor in order to improve the ability to intercept an unknown target in collaborative defense. A tripartite maneuvering game model is established, in which the homing constraint information can be obtained using the line-of-sight command. The method of solving the terminal problem by the adjoint mathematics is used to get the zero effort miss distance of the differential strategy by taking terminal miss distance and control energy as the performance indexes, which can be applied to arbitrary order control situation for tripartite strategies. The receding horizon control is used to predict the guidance law parameters in real time. The differential game strategy is simple to implement in practical applications under the conditions of homing. The performance of the guidance law is analyzed, and the effects of intercepting the targets by using different guidance laws are compared. The simulated results show that the differential game guidance law is robust adaptability and stability, which is not restricted by the maneuvering forms of targets under the condition of same constraints, and is of better trajectory characteristics.

关键词

兵器科学与技术 / 微分对策制导 / 水下拦截器 / 协同作战 / 零效脱靶量

Key words

ordnance science and technology / differential guidance law / underwater interceptor / cooperative engagement / zero effort miss distance

引用本文

导出引用
刘卫东, 程瑞锋, 高立娥, 张建军. 水下微分对策协同拦截制导策略. 兵工学报. 2016, 37(9): 1684-1691 https://doi.org/10.3969/j.issn.1000-1093.2016.09.019
LIU Wei-dong, CHENG Rui-feng, GAO Li-e, ZHANG Jian-jun. Cooperative Engagement-based Differential Guidance Law for Underwater Interceptor. Acta Armamentarii. 2016, 37(9): 1684-1691 https://doi.org/10.3969/j.issn.1000-1093.2016.09.019

基金

水下信息与控制重点实验室基金项目(9140C230202150C23001);国家自然科学基金项目(61473224)

参考文献

[1] 陈春玉.反鱼雷技术[M].北京:国防工业出版社,2006.
CHEN Chun-yu. Anti-torpedo technology[M].Beijing: National Defense Industry Press,2006.(in Chinese)
[2] ShimaT. Optimal cooperative pursuit and evasion strategies against a homing missile[J].Journal of Guidance, Control, and Dynamics,2011,34(2):414-425.
[3] 肖增博,雷虎民,滕江川,等.目标飞行器反拦截协同制导策略[J].兵工学报,2011, 32 (12):1486-1492.
XIAO Zeng-bo,LEI Hu-min,TENG Jiang-chuan, et al. Cooperative guidance strategy in anti-interception for target aircrafts[J]. Acta Armamentarii, 2011, 32 (12):1486-1492. (in Chinese)
[4] 花文华,陈兴林,宋超. 主动防御协同自适应滑模制导律[J].飞行力学,2012,30(1):66-70.
HUA Wen-hua, CHEN Xing-lin, SONG Chao. Cooperative guidance law for active protection based on adaptive sliding-mode control[J]. Flight Dynamics, 2012,30(1):66-70. (in Chinese)
[5] Perelman A, Shima T. Cooperative differential games strategies for active aircraft protection from a homing missile[J]. AIAA Journal of Guidance, Control, and Dynamics,2011,34(3):761-773.
[6] 邹昕光,周荻,杜润乐,等.主动防御非奇异终端滑模协同制导律[J].兵工学报,2015, 36(3):475-485.
ZOU Xin-guang, ZHOU Di, DU Run-yue, et al. Active defense nonsingular terminal sliding mode cooperative guidance[J]. Acta Armamentarii, 2015, 36(3):475-485. (in Chinese)
[7] 徐德民.鱼雷自动控制系统[M].西安:西北工业大学出版社,2001.
XU De-min. Torpedo auto-control system[M].Xi'an: Northwestern Polytechnical University Press, 2001.(in Chinese)
[8] 聂卫东,王岚,马玲.水下网络中心战环境下鱼雷战术概念研究[J].鱼雷技术,2015, 23 (5):384-388.
NIE Wei-dong,WANG Lan, MA Ling. Conceptual study on tactics of torpedo in underwater network centric warfare[J]. Torpedo Technology,2015,23(5):384-388.(in Chinese)
[9] 孟秀云.导弹制导与控制系统原理[M].北京:北京理工大学出版社,2009.
MENG Xiu-yun. Principle of missile guidance and control system[M].Beijing:Beijing Institute of Technology Press, 2009.(in Chinese)
[10] 花文华,陈兴林,宋申民.主动防御的协同微分对策制导[J].高技术通讯,2012, 22(1):94-99.
HUA Wen-hua,CHEN Xing-lin,SONG Shen-min. Cooperative differential game guidance strategy for active defense[J].High Technology Letters,2012,22(1):94-99. (in Chinese)
[11] 李运迁,齐乃明.基于零控脱靶量的大气层内拦截弹制导律[J].宇航学报,2010, 31(7):1768-1774.
LI Yun-qian, QI Nai-ming. A zero-effort miss distance based guidance law for endoatmospheric interceptor[J].Journal of Astronautics,2010, 31(7): 1768-1774. (in Chinese)
[12] 方洋旺,伍友利,王洪强,等.导弹先进制导与控制理论[M].北京:国防工业出版社,2015.
FANG Yang-wang, WU You-li, WANG Hong-qiang, et al. Missile advanced guidance and control theory[M].Beijing: National Defense Industry Press,2015. (in Chinese)
[13] 张士熊,刘新学,李斌,等.基于微分对策的拦截末段突防导弹机动突防制导律研究[J]. 导弹与航天运载技术, 2015(2):81-86.
ZHANG Shi-xiong, LIU Xin-xue, LI Bin,et al. Study on maneuver penetration guidance law of ballistic based on differential games in the terminal of interception[J]. Missiles and Space Vehicles, 2015(2):81-86. (in Chinese)
[14] 蔡艳利.基于滚动时域控制的无人直升机飞行控制研究[D].南京:南京航空航天大学,2009.
CAI Yan-li. Research on flight control of unmanned helicopter based on receding horizon control[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2009.(in Chinese)
[15] 曹宇光.基于滚动时域的卫星姿态最优控制研究[D].哈尔滨:哈尔滨工业大学,2011.
CAO Yu-guang. Optimal control base for satellite attitude based on receding horizon[D].Harbin:Harbin Institute of Technology,2011. (in Chinese)

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