有向拓扑条件下针对机动目标的分布式协同制导律设计

doi:10.7527/S1000-6893.2019.23762

Abstract

Abstract: This paper studies the distributed cooperative guidance for maneuvering targets with directed communication topologies. First, a guidance system model is established based on the geometric relationship between the aircraft and the target, in which the nonlinear problem is solved by feedback linearization. In this design, the unknown maneuver of the target is observed by the extended state observer, and the estimation of the unknown maneuver of the target is applied to the design of the guidance law. In this process, the influence of the target maneuvering on the time-to-go is eliminated by means of direct compensation. Then, the designed guidance law is brought into the guidance model, transforming the problem of cooperative guidance into the problem of consensus. Next, the necessary and sufficient conditions for the convergence of the designed cooperative guidance law are obtained by conducting the pole analysis. Finally, the designed cooperative guidance law and the method of the parameter selection are analyzed by adopting the simulation analysis.

Key words: maneuvering target, distributed cooperative guidance, extended state observer, consensus, feedback linearization

CLC Number:

V448.1

DONG Xiaofei, REN Zhang, CHI Qingxi, LI Qingdong. Distributed cooperative guidance for maneuvering targets with directed conmunication topologies[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(S1): 723762-723762.

References 30

[1]	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.
[2]	ZHANG Y, WANG X, MA G. Impact time control guidance law with large impact angle constraint[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2015, 229(11):2119-2131.
[3]	孙阳平, 林王鹏, 范作娥, 等. 一种多约束条件下的最优末制导律研究[J]. 兵工自动化, 2013, 32(12):4-7. SUN Y P, LIN W P, FAN Z E, et al. Study on optimal guidance law under multiple-constrained condition[J]. Ordnance Industry Automation, 2013, 32(12):4-7(in Chinese).
[4]	张友根, 张友安, 施建洪, 等.基于双圆弧原理的协同制导律研究[J].海军航空工程学院学报, 2009, 24(5):537-542. ZHANG Y G, ZHANG Y A, SHI J H, et al. Research on cooperative guidance for multi-missiles based on bi-arcs[J]. Journal of Naval Aeronautical and Astronautical University, 2009, 24(5):537-542(in Chinese).
[5]	HARL N, BALAKRISHNAN S N. Impact time and angle guidance with sliding mode control[J]. IEEE Transactions on Control Systems Technology, 2011, 20(6):1436-1449.
[6]	KUMAR S R, GHOSE D. Sliding mode control based guidance law with impact time constraints[C]//2013 American Control Conference (ACC). Piscataway:IEEE Press, 2013:5760-5765.
[7]	KUMAR S R, GHOSE D. Impact time and angle control guidance[C]//AIAA Guidance, Navigation, and Control Conference. Reston:AIAA, 2015:1-22.
[8]	ZHAO E J, 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:IEEE Press. 2014:1163-1167.
[9]	ZHAO E J, CHAO T, 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.
[10]	QILUN Z, XIWANG D, JIAN C, et al. Coordinated guidance strategy for heterogeneous missiles intercepting hypersonic weapon[C]//Proceedings of the 34th Chinese Control Conference (CCC), 2015:5170-5175.
[11]	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.
[12]	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.
[13]	HARRISON G A.Hybrid Guidance law for approach angle and time-of-arrival control[J]. Journal of Guidance Control & Dynamics, 1971, 35(4):1104-1114.
[14]	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).
[15]	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).
[16]	WANG Y, DONG S, OU L, et al. Cooperative control of multi-missile systems[J]. IET Control Theory & Applications, 2014, 9(3):441-446.
[17]	ZHAO J, ZHOU S, ZHOU R. Distributed time-constrained guidance using nonlinear model predictive control[J]. Nonlinear Dynamics, 2016, 84(3):1399-1416.
[18]	ZHAO J, ZHOU R. Distributed three-dimensional cooperative guidance via receding horizon control[J]. Chinese Journal of Aeronautics, 2016, 29(4):972-983.
[19]	ZHAO Q L, DONG X W, LIANG Z X, et al. Distributed cooperative guidance for multiple missiles with fixed and switching communication topologies[J]. Chinese Journal of Aeronautics, 2017, 30(4):1570-1581.
[20]	NIKUSOKHAN M, NOBAHARI H. Closed-form optimal cooperative guidance law against random step maneuver[J]. IEEE Transactions on Aerospace and Electronic Systems, 2016, 52(1):319-336.
[21]	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.
[22]	ZHAO J, ZHOU R. Unified approach to cooperative guidance laws against stationary and maneuvering targets[J]. Nonlinear Dynamics, 2015, 81(4):1635-1647.
[23]	ZHAO Q L, DONG X W, SONG X, et al. Cooperative time-varying formation guidance for leader-following missiles to intercept a maneuvering target with switching topologies[J]. Nonlinear Dynamics, 2019, 95(1):129-141.
[24]	ZHOU J, LYU Y, LI Z, et al. Cooperative guidance law design for simultaneous attack with multiple missiles against a maneuvering target[J]. Journal of Systems Science and Complexity, 2018, 31(1):287-301.
[25]	SHAFEMAN 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.
[26]	SHAFEMAN V, SHIMA T. Cooperative differential games guidance laws for imposing a relative intercept angle[J]. Journal of Guidance, Control, and Dynamics, 2015, 40(10):2465-2480.
[27]	WANG X H, TAN C P. 3-D Impact angle constrained distributed cooperative guidance for maneuvering targets without angular-rate measurements[J]. Control Engineering Practice, 2018, 78:142-159.
[28]	REN W, BEARD R W. Consensus seeking in multi-agent systems under dynamically changing interaction topologies[J]. IEEE Transactions on Automatic Control, 2005, 50(5):665-671.
[29]	RAN M P, WANG Q, DONG C Y. Stabilization of a class of nonlinear systems with actuator saturation via active disturbance rejection control[J]. Automatica, 2016, 63:302-310.
[30]	ZAHREDDINE Z, ELSHEHAWEY E F. On the stability of a system of differential equations with complex coefficients[J]. Indian Journal of Pure and Applied Mathematics, 1988, 19(10):963-972.

Distributed cooperative guidance for maneuvering targets with directed conmunication topologies

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References 30

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Hongyan ZHANG, Wei WANG, Shiwei CHEN, Yi JI, Jiaqi LIU. Integrated guidance and control design based on fully actuated system method [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628891-628891.
[2]	Zeyang YIN, Youpeng XING, Fei HAN, Caisheng WEI, Yuxin LIAO. Fully-actuated prescribed performance control of spacecraft formation for flying cooperatively around non-cooperative target [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 628904-628904.
[3]	Xu ZHAO, Guoyuan QI, Xinchen YU, Jianbing HU, Xia LI. Compensation function observer and its application in flight vehicle attitude control [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(9): 327224-327224.
[4]	Zheng LI, Jianqiao YU, Xinyun ZHAO. Fixed⁃time convergent sliding mode control for agile turn of air⁃to⁃air missiles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 327262-327262.
[5]	Shihao XU, Yingzi GUAN, Jialun PU, Changzhu WEI. Predefined-time sliding mode control for VTHL launch vehicle in reentry phase [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 326857-326857.
[6]	Shengqing YANG, Jingyu WU, Wenshan ZHU, Chao ZHONG. Control method of constellation relative-configuration maintenance based on inter-satellite links [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 326796-326796.
[7]	Liang ZHANG, Danyu LI, Naigang CUI, Yuan LI. Full flight profile prescribed performance control for vertical take-off and vertical landing reusable launch vehicle [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(23): 628103-628103.
[8]	Yiting TAN, Wuxing JING, Changsheng GAO, Ruoming AN. Multiple constrained analytical capture region for hypersonic maneuvering target interception [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 328436-328436.
[9]	Wenxue CHEN, Changsheng GAO, Wuxing JING. Trust region policy optimization guidance algorithm for intercepting maneuvering target [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(11): 327596-327596.
[10]	Chuang XU, Baolin WU. Distributed fixed-time output-feedback attitude consensus control for multiple spacecraft with input saturation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(10): 327465-327465.
[11]	WANG Lin, ZHANG Qingjie, CHEN Hongwei. Optimal control method for swarm systems formation with LQR performance index [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S1): 726902-726902.
[12]	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.
[13]	XIONG Wei, ZHU Hongfeng, CUI Yaqi. Recurrent adaptive maneuvering target tracking algorithm based on online learning [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(5): 325250-325250.
[14]	LI Ning, LIU Zhiyong, WANG Na, YANG Lei. Simulation on antenna servo control system based on DUEA [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 324986-324986.
[15]	LI Xia, QI Guoyuan, GUO Xitong, ZHAO Xu. High-order differential feedback control and its application in quadrotor UAV [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 326047-326047.