多导弹协同制导研究综述

doi:10.7527/S1000-6893.2016.0136

Abstract

Abstract:

This paper reviews the development history of multi-missile cooperative guidance, including the main research findings and the latest progresses. In view of the fact that the existing results of the research on cooperative guidance are mainly concerned with time coordination and the open-loop cooperative guidance has been well reviewed, this paper focuses on the close-loop time cooperative guidance accordingly. Based on its framework, the multi-missile time cooperative guidance can be categorized into two types:the two-level guidance, and "leader-follower" one. It can be also categorized into centralized and decentralized one based on communication topology among missiles. The two types of cooperative guidance frameworks are discussed first. The centralized and decentralized multi-missile cooperative guidance laws are then analyzed. The merits and demerits of these types of cooperative guidance laws are also summarized. A short discussion section is included to propose several promising research directions for further investigation.

Key words: multi-missile, missile guidance, cooperative guidance, communication, two-level coordination, leader-follower, salvo attack, impact time

CLC Number:

ZHAO Jianbo, YANG Shuxing. Review of multi-missile cooperative guidance[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(1): 20256-020256.

References

[1] 王芳, 涂震飚, 魏佳宁. 战术导弹协同突防关键技术研究[J]. 战术导弹技术, 2013(3):13-17. WANG F, TU Z B, WEI J N. Research on key technical problems of cooperative penetration for tactical missile[J]. Tactical Missile Technology, 2013(3):13-17(in Chinese).
[2] 王建青, 李帆, 赵建辉, 等. 多导弹协同制导律综述[J]. 飞行力学, 2011, 29(4):6-10. WANG J Q, LI F, ZHAO J H, et al. Summary of guidance law based on cooperative attack of multi-missile method[J]. Flight Dynamics, 2011, 29(4):6-10(in Chinese).
[3] 肖志斌, 何冉, 赵超. 导弹编队协同作战的概念及其关键技术[J]. 航天电子对抗, 2013, 29(1):1-3. XIAO Z B, HE R, ZHAO C. Cooperative combat of missile formation:Concepts and key technologies[J]. Aerospace Electronic Warfare, 2013, 29(1):1-3(in Chinese).
[4] 张克, 刘永才, 关世义. 体系作战条件下飞航导弹突防与协同攻击问题研究[J]. 战术导弹技术, 2005(2):1-7. ZHANG K, LIU Y C, GUAN S Y. An investigation into the issues of penetration and cooperative engagement for aerodynamic missile under the condition of systems coutermeasures[J]. Tactical Missile Technology, 2005(2):1-7(in Chinese).
[5] 赵启伦, 陈建, 董希旺, 等. 拦截高超声速目标的异类导弹协同制导律研究[J]. 航空学报, 2016, 37(3):936-948. ZHAO Q L, CHEN J, DONG X W, et al. Cooperative guidance law for heterogeneous missiles intercepting hypersonic weapon[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(3):936-948(in Chinese).
[6] 胡正东, 林涛, 张士峰, 等. 导弹集群协同作战系统概念研究[J]. 飞航导弹, 2007(10):13-18. HU Z D, LIN T, ZHANG S F, et al. The concept study of multi-missile cooperative combat system[J]. Aerodynamic Missile Journal, 2007(10):13-18(in Chinese).
[7] 赵世钰, 周锐. 基于协调变量的多导弹协同制导[J]. 航空学报, 2008, 29(6):1605-1611. ZHAO S Y, ZHOU R. Multi-missile cooperative guidance using coordination variables[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(6):1605-1611(in Chinese).
[8] 林涛, 刘永才, 关成启, 等. 飞航导弹协同作战使用方法探讨[J]. 战术导弹技术, 2005(2):8-12. LIN T, LIU Y C, GUAN C Q, et al. An investigation into the methods of cooperative engagement for aerodynamic missile[J]. Tactical Missile Technology, 2005(2):8-12(in Chinese).
[9] JEON I S, LEE J I, TAHK M J. Impact-time-control guidance law for anti-ship missiles[J]. IEEE Transactions on Control Systems Technology, 2006, 14(2):260-266.
[10] 张友安, 马国兴, 王兴平. 多导弹时间协同制导:一种领弹-被领弹策略[J]. 航空学报, 2009, 30(6):1109-1118. ZHANG Y A, MA G X, WANG X P. Time-cooperative guidance for multi-missiles:A leader-follower strategy[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(6):1109-1118(in Chinese).
[11] 肖增博, 雷虎民, 滕江川, 等. 多导弹协同制导规律研究现状及展望[J]. 航空兵器, 2011(6):18-22. XIAO Z B, LEI H M, TENG J C, et al. The present status and prospect of multi-missile cooperative guidance law[J]. Aero Weaponry, 2011(6):18-22(in Chinese).
[12] 张友安, 王星亮, 吴华丽, 等. 带攻击时间约束的导引律综述[J]. 海军航空工程学院学报, 2015, 30(4):301-309. ZHANG Y A, WANG X L, WU H L, et al. Survey of guidance law with attack time constraint[J]. Journal of Naval Aeronautical and Astronautical University, 2015, 30(4):301-309(in Chinese).
[13] ZHAO S Y, ZHOU R, WEI C, et al. Design of time-constrained guidance laws via virtual leader approach[J]. Chinese Journal of Aeronautics, 2010, 23(1):103-108.
[14] 王晓芳, 林海. 多约束条件下导弹协同作战制导律[J]. 弹道学报, 2012, 24(3):59-64. WANG X F, LIN H. A guidance law for multiple missiles combating cooperatively under multiple constraints[J]. Journal of Ballistics, 2012, 24(3):59-64(in Chinese).
[15] HARL N, BALAKRISHNAN S N. Impact time and angle guidance with sliding mode control[J]. IEEE Transactions on Control Systems Technology, 2012, 20(6):1436-1449.
[16] KUMAR S R, GHOSE D. Sliding mode control based guidance law with impact time constraints[C]//Proceedings of the American Control Conference. Piscataway, NJ:IEEE Press, 2013:5760-5765.
[17] GUO C, LIANG X G. Cooperative guidance law for multiple near space interceptors with impact time control[J]. International Journal of Aeronautical & Space Sciences, 2014, 15(3):281-292.
[18] ZHAO S Y, ZHOU R, WEI C. Design and feasibility analysis of a closed-form guidance law with both impact angle and time constraints[J]. Journal of Astronautics, 2009, 30(3):1064-1072.
[19] KANG S, KIM H J. Differential game missile guidance with impact angle and time constraints[J]. World Congress, 2011, 18(1):3920-3925.
[20] WANG X, ZHENG Y, LIN H. Integrated guidance and control law for cooperative attack of multiple missiles[J]. Aerospace Science and Technology, 2015, 42:1-11.
[21] 施建洪, 张友安, 梁勇. 飞行器落角与撞击时间控制研究[J]. 海军航空工程学院学报, 2011, 26(4):398-404. SHI J H, ZHANG Y A, LIANG Y. Research on Impact angle control and impact time control for aircraft[J]. Journal of Naval Aeronautical and Astronautical University, 2011, 26(4):398-404(in Chinese).
[22] ZHAO E, WANG S, CHAO T, et al. Multiple missiles cooperative guidance based on leader-follower strategy[C]//Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference. Piscataway, NJ:IEEE Press, 2014:1163-1167.
[23] MCLAIN T W, BEARD R W. Coordination variables, coordination functions, and cooperative timing missions[J]. Journal of Guidance, Control, and Dynamics, 2005, 28(1):150-161.
[24] KUMAR S R, GHOSE D. Cooperative rendezvous guidance using sliding mode control for interception of stationary targets[C]//Proceedings of Third International Conference on Advances in Control and Optimization of Dynamical Systems. Dusseldorf:IFAC Secretariat, 2014:477-483.
[25] 邹丽, 丁全心, 周锐. 异构多导弹网络化分布式协同制导方法[J]. 北京航空航天大学学报, 2010, 36(12):1432-1435. ZOU L, DING Q X, ZHOU R. Distributed cooperative guidance for multiple heterogeneous networked missiles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(12):1432-1435(in Chinese).
[26] 王晓芳, 洪鑫, 林海. 一种控制多弹协同攻击时间和攻击角度的方法[J]. 弹道学报, 2012, 24(2):1-5. WANG X F, HONG X, LIN H. A method of controlling impact time and impact angle of multiple-missiles cooperative combat[J]. Journal of Ballistics, 2012, 24(2):1-5(in Chinese).
[27] 马国欣, 张友根, 张友安. 一领弹控制下的多导弹时间协同三维制导律[J]. 海军航空工程学院学报, 2013, 28(1):11-16. MA G X, ZHANG Y G, ZHANG Y A. Leader-controlled three-dimensional guidance law for time-cooperative multi-missiles[J]. Journal of Naval Aeronautical and Astronautical University, 2013, 28(1):11-16(in Chinese).
[28] SUN X, ZHOU R, HOU D, et al. Consensus of leader-followers system of multi-missile with time-delays and switching topologies[J]. Optik-International Journal for Light and Electron Optics, 2014, 125(3):1202-1208.
[29] 邹丽, 孔繁峨, 周锐, 等. 多导弹分布式自适应协同制导方法[J]. 北京航空航天大学学报, 2012, 38(1):128-132. ZOU L, KONG F E, ZHOU R, et al. Distributed adaptive cooperative guidance for multi-missile salvo attack[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(1):128-132(in Chinese).
[30] 邹丽, 周锐, 赵世钰, 等. 多导弹编队齐射攻击分散化协同制导方法[J]. 航空学报, 2011, 32(2):281-290. ZOU L, ZHOU R, ZHAO S Y, et al. Decentralized cooperative guidance for multiple missile groups in salvo attack[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(2):281-290(in Chinese).
[31] ZHAO E, TAO C, WANG S, et al. An adaptive parameter cooperative guidance law for multiple flight vehicles[C]//Proceedings of AIAA Atmospheric Flight Mechanics Conference. Reston:AIAA, 2015:2709-2718.
[32] 孙雪娇, 周锐, 吴江, 等. 多导弹分布式协同制导与控制方法[J]. 北京航空航天大学学报, 2014, 40(1):120-124. SUN X J, ZHOU R, WU J, et al. Distributed cooperative guidance and control for multiple missiles[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(1):120-124(in Chinese).
[33] 周锐, 孙雪娇, 吴江, 等. 多导弹分布式协同制导与反步滑模控制方法[J]. 控制与决策, 2014, 29(9):1617-1622. ZHOU R, SUN X J, WU J, et al. Multi-missile distributed cooperative guidance integrating backstepping sliding mode control[J]. Control and Decision, 2014, 29(9):1617-1622(in Chinese).
[34] 后德龙, 陈彬, 王青, 等. 碰撞自规避多弹分布式协同制导与控制[J]. 控制理论与应用, 2014, 31(9):1133-1142. HOU D L, CHEN B, WANG Q, et al. Collision avoidance multi-missile distributed cooperative guidance and control[J]. Control Theory and Applications, 2014, 31(9):1133-1142(in Chinese).
[35] 彭琛, 刘星, 吴森堂, 等. 多弹分布式协同末制导时间一致性研究[J]. 控制与决策, 2010, 25(10):1557-1561. PENG C, LIU X, WU S T, et al. Consensus problems in distributed cooperative terminal guidance time of multi-missiles[J]. Control and Decision, 2010, 25(10):1557-1561(in Chinese).
[36] ZHAO J, ZHOU R. Unified approach to cooperative guidance laws against stationary and maneuvering targets[J]. Nonlinear Dynamics, 2015, 81(4):1635-1647.
[37] ZHAO J, ZHOU R, DONG Z. Three-dimensional cooperative guidance laws against stationary and maneuvering targets[J]. Chinese Journal of Aeronautics, 2015, 28(4):1104-1120.
[38] 张保峰, 宋俊红, 宋申民. 具有角度约束的多导弹协同制导研究[J]. 弹箭与制导学报, 2014, 34(1):13-15. ZHANG B F, SONG J H, SONG S M. Research on multi-missile cooperative guidance with angle constraint[J]. Journal of Projectiles Rockets Missiles and Guidance, 2014, 34(1):13-15(in Chinese).
[39] 王青, 后德龙, 李君, 等. 具有角度约束的多导弹协同制导研究[J]. 兵工学报, 2014, 35(7):982-989. WANG Q, HOU D L, LI J, et al. Consensus analysis of multi-missile decentralized cooperative guidance time with time-delays and topologies uncertainty[J]. Acta Armamentarii, 2014, 35(7):982-989(in Chinese).
[40] HA I J, HUR J S, KO M S, et al. Performance analysis of PNG laws for randomly maneuvering targets[J]. IEEE Transactions on Aerospace and Electronic Systems, 1990, 26(5):713-721.
[41] JEON I S, LEE J I, TAHK M J. Homing guidance law for cooperative attack of multiple missiles[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(1):275-280.
[42] SONG S H, HA I J. A Lyapunov-like approach to performance analysis of 3-dimensional pure PNG laws[J]. IEEE Transactions on Aerospace and Electronic Systems, 1994, 30(1):238-248.
[43] WU X, WU S, XING Z. A guidance law with impact angle constraint for anti-ship missiles cooperative attack[C]//Proceedings of the 33rd Chinese Control Conference. Piscataway, NJ:IEEE Press, 2014:954-959.
[44] ZENG J, DOU L, XIN B. Cooperative salvo attack using guidance law of multiple missiles[J]. Journal of Advanced Computational Intelligence and Intelligent Informatics, 2015, 19(2):301-306.
[45] SUN X, XIA Y Q. Optimal guidance law for cooperative attack of multiple missiles based on optimal control theory[J]. International Journal of Control, 2012, 85(8):1063-1070.
[46] MORGAN R W, THARP H, VINCENT T L. Minimum energy guidance for aerodynamically controlled missiles[J]. IEEE Transactions on Automatic Control, 2011, 56(9):2026-2037.
[47] 张友安, 胡云安. 导弹控制和制导的非线性设计方法[M]. 北京:国防工业出版社, 2003:160-163. ZHANG Y A, HU Y A. Nonlinear design approaches for missile control and guidance[M]. Beijing:National Defense Industry Publisher, 2003:160-163(in Chinese).
[48] WANG X, ZHANG Y, WU H. Distributed cooperative guidance of multiple anti-ship missiles with arbitrary impact angle constraint[J]. Aerospace Science and Technology, 2015, 46:299-311.
[49] 马国欣, 张友安. 多导弹时间协同分布式导引律设计[J]. 控制与决策, 2014, 29(5):843-847. MA G X, ZHANG Y A. Time-cooperative distributed guidance law design for multi-missiles[J]. Control and Decision, 2014, 29(5):843-847(in Chinese).
[50] ZHAO S Y, ZHOU R. Cooperative guidance for multimissile salvo attack[J]. Chinese Journal of Aeronautics, 2008, 21(6):533-539.
[51] HOU J, JI X, LIU Z, et al. Distributed multi-missile salvo attack[C]//Proceedings of the 33rd Chinese Control Conference. Piscataway, NJ:IEEE Press, 2014:887-890.
[52] PARK J, YOO J H, KIM H J. Two distributed guidance approaches for rendezvous of multiple agents[C]//Proceedings of the 2010 International Conference on Control, Automation and Systems. Piscataway, NJ:IEEE Press, 2010:2128-2132.
[53] SONG L, ZHANG Y, HUANG D, et al. Cooperative simultaneous attack of multi-missiles under unreliable and noisy communication network:A consensus scheme of impact time[J]. Aerospace Science and Technology, 2015, 47:31-41.
[54] 孙雪娇, 周锐, 吴江, 等. 攻击机动目标的多导弹分布式协同制导律[J]. 北京航空航天大学学报, 2013, 39(10):1403-1407. SUN X J, ZHOU R, WU J, et al. Distributed cooperative guidance law for multiple missiles attacking maneuver target[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(10):1403-1407(in Chinese).
[55] HOU D, WANG Q, SUN X, et al. Finite-time cooperative guidance laws for multiple missiles with acceleration saturation constraints[J]. IET Control Theory & Applications, 2015, 9(10):1525-1535.
[56] WEI X, WANG Y, DONG S, et al. A three-dimensional cooperative guidance law of multimissile system[J]. International Journal of Aerospace Engineering, 2015, 2015(4):1-8.
[57] DAUGHTERY E, QU Z. Optimal design of cooperative guidance law for simultaneous strike[C]//Proceedings of the 53rd IEEE Conference on Decision and Control. Piscataway, NJ:IEEE Press, 2014:988-993.
[58] ZHANG Y A, MA G X, WU H L. A biased proportional navigation guidance law with large impact angle constraint and the time-to-go estimation[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2014, 228(10):1725-1734.
[59] LEE J I, JEO I S, TAHK M J. Guidance law to control impact time and angle[J]. IEEE Transactions on Aerospace and Electronic Systems, 2007, 43(1):301-310.
[60] QU Z, WANG J, HULL R A. Cooperative control of dynamical systems with application to autonomous vehicles[J]. IEEE Transactions on Automatic Control, 2008, 53(4):894-911.
[61] 李东岩, 张志峰, 王飞, 等. 基于制导/估计综合设计的协同制导律[J]. 北京理工大学学报, 2012, 32(5):508-512. LI D Y, ZHANG Z F, WANG F, et al. Cooperative guidance law based on integration design of guidance and estimation[J]. Transactions of Beijing Institute of Technology, 2012, 32(5):508-512(in Chinese).
[62] GHOSH S, GHOSE D, RAHA S. Three dimensional Retro-PN based impact time control for higher speed nonmaneuvering targets[C]//Proceedings of the 52nd IEEE Conference on Decision and Control. Piscataway, NJ:IEEE Press, 2013:4865-4870.
[63] GHOSH S, GHOSE D, RAHA S. Retro-PN based simultaneous salvo attack against higher speed nonmaneuvering targets[C]//Proceedings of the third International Conference on Advances in Control and Optimization of Dynamical Systems. Dusseldorf:IFAC, 2014:34-40.
[64] ZHAO J, ZHOU S Y, ZHOU R. Distributed time-constrained guidance using nonlinear model predictive control[J]. Nonlinear Dynamics, 2016, 84(3):1399-1416.
[65] ZHAO J, ZHOU R. Obstacle avoidance for multi-missile network via distributed coordination algorithm[J]. Chinese Journal of Aeronautics, 2016, 29(2):441-447.
[66] SHAFERMAN V, SHIMA T. Cooperative optimal guidance laws for imposing a relative intercept angle[J]. Journal of Guidance, Control, and Dynamics, 2015, 38(8):1395-1408.

Review of multi-missile cooperative guidance

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Cheng’an ZHANG, Baoguo LI, Xiang WANG, Qiang XU. Radar-embedded communication waveform design with low complexity [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 326471-326471.
[2]	HU Yangxiu, ZHAO Changchun, JIA Chenglong, QIAN Zhouyuan, HU Tao. Synchronous path formation control of UAV swarm based on robot operating system (ROS) [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S1): 726914-726914.
[3]	YU Jianglong, DONG Xiwang, LI Qingdong, LYU Jinhu, REN Zhang. Distributed cooperative encirclement hunting guidance method for intercepting maneuvering target [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 325817-325817.
[4]	LI Baoguo, ZHANG Cheng'an, XU Jianqiu. A radar-embedded communication waveform design method based on SVD [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 325401-325401.
[5]	ZHANG Yi, ZHAI Shenghua, TAO Haihong. Identification of interference source for single satellite geolocation using chaotic mapping [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 325407-325407.
[6]	ZHU Zhengyu, WANG Zixuan, XU Jinlei, WANG Zhongyong, WANG Ning, HAO Wanming. Future wireless communication assisted by intelligent reflecting surface: State of art and prospects [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 25014-025014.
[7]	REN Shaorui, LU Zhongmei, SHI Yuanming, LI Lixin, CHEN Wei. UAV communication coverage model based on pheromone map [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 324939-324939.
[8]	LIU Haining, ZHANG Shaoqing, E Siyu. Application of wireless communication of aviation airborne platform based on 5G technology [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 326233-326233.
[9]	LUO He, LI Xiaoduo, WANG Guoqiang. Energy-balanced communication topology generation of three-dimensional optimally persistent formation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 324922-324922.
[10]	TANG Yang, ZHU Xiaoping, ZHOU Zhou, YAN Fei. Cooperative guidance method based on impact time and angle control [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 324844-324844.
[11]	CHEN Pu, YAN Fei, LIU Zhao, CHENG Guoda. Communication-constrained task allocation of heterogeneous UAVs [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525844-525844.
[12]	HE Feng, LI Ershuai, ZHOU Xuan, LI Haoruo, GONG Zijie. Design optimization and evaluation method for time-triggered communication scheduling in airborne networks [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 324258-324258.
[13]	LI Qiao, LI Jia, XIONG Huagang, YANG Jinhe. Accessing capacity of Deficit Round-Robin (DRR) in avionics very-short range THz interconnections [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 624082-624082.
[14]	DONG Wenqi, HE Feng. Hierarchical and distributed generation of information interaction topology for large scale UAV formation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(6): 324380-324380.
[15]	JIANG Xia, ZENG Xianlin, SUN Jian, CHEN Jie. Research status and prospect of distributed optimization for multiple aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(4): 524551-524551.