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Journal of Projectiles, Rockets, Missiles and Guidance >

2021 , Vol. 41 >Issue 6: 1 - 6

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.06.001

Research on Three-dimensional Guidance Law for Cooperative Attack of Multi-unpowered Missiles

  • ZHANG Mingyang 1 ,
  • MA Zeyuan 2 ,
  • XIA Qunli 1 ,
  • LI Moyin 1 ,
  • LI Wei 1
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  • 1 School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
  • 2 Shanghai Electro-mechanical Engineering Institute, Shanghai 201109, China

Received date: 2021-08-20

  Online published: 2025-02-07

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Abstract

A time-cooperative three-dimensional guidance method based on dynamic inversion is proposed for the simultaneous attack on high-value time-sensitive targets by multiple unpowered aircrafts in the terminal guidance stage. First, a three-dimensional nonlinear model of the relative movement of the missile and the target is established. Then, the lead missile adopts proportional guidance in both the pitch channel and the yaw channel, and the follow missiles adopt a combination of proportional guidance and maneuver control. Finally, in order to achieve multiple missiles attacking the moving target at the same time, the remaining time error of the leader missile and the follow missiles is selected as the coordination variable, and the time-scale decomposition method is used to decompose the relative motion nonlinear model of follow missiles into a fast subsystem and a slow subsystem, then dynamic inversion is used to feedback linearization of two subsystems and the yaw channel overload command is solved under certain overload constraints. The simulation results verify the effectiveness of the proposed guidance method.

Key words： multiple missiles; time-cooperative guidance; time-varying velocity; moving target; dynamic inversion

Cite this article

ZHANG Mingyang , MA Zeyuan , XIA Qunli , LI Moyin , LI Wei . Research on Three-dimensional Guidance Law for Cooperative Attack of Multi-unpowered Missiles[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2021 , 41(6) : 1 -6 . DOI: 10.15892/j.cnki.djzdxb.2021.06.001

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References

Publishing order | Descend order by publishing year | Descend order by cited within
[1]
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.

[2]
赵恩娇, 孙明玮. 多飞行器协同作战关键技术研究综述[J]. 战术导弹技术, 2020, 26(4):175-182.

[3]
CHEN X T, WANG J Z. Nonsingular sliding-mode control for field-of-view constrained impact time guidance[J]. Journal of Guidance, Control, and Dynamics, 2018, 41(5): 1-9.

[4]
KIM M, JUNG B, HAN B, et al. Lyapunov-based impact time control guidance laws against stationary targets[J]. Aerospace & Electronic Systems IEEE Transactions on, 2015, 51(2): 1111-1122.

[5]
SALEEM A, RATNOO A. Lyapunov-based guidance law for impact time control and simultaneous arrival[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(1): 164-173.

[6]
WEI X, WANG Y, DONG S, et al. A three-dimensional cooperative guidance law of multimissile system[J]. International Journal of Aerospace Engineering, 2015, 32(4): 1-8.

[7]
ZHAO Q, DONG X, LIANG Z, et al. Distributed cooperative guidance for multiple missiles with fixed and switching communication topologies[J]. Chinese Journal of Aeronautics, 2017, 30(4): 1570-1581.

[8]
HE S, WANG W, LIN D, et al. Consensus-based two-stage salvo attack guidance[J]. IEEE Transactions on Aerospace and Electronic Systems, 2018, 54(3): 1555-1566.

[9]
张友安, 马国欣, 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.

[10]
赵斌, 黄晓阳, 周军, 等. 基于滑模控制的多弹分布式视线协同制导律设计[J]. 空天防御, 2020, 3(3):16-23.

[11]
SONG T L, SHIN S J. Time-optimal impact angle control for vertical plane engagements[J]. Aerospace & Electronic Systems IEEE Transactions on, 1999, 35(2): 738-742.

[12]
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.

[13]
赵恩娇, 晁涛, 王松艳, 等. 攻击运动目标的参数自适应多弹协同制导方法[J]. 固体火箭技术, 2016, 39(2):287-294.

[14]
SHAFERMAN V, SHIMA T. Cooperative differential games guidance laws for imposing a relative intercept angle[J]. Journal of Guidance, Control, and Dynamics, 2017, 40(10): 2465-2480.

[15]
LEE C H T A. Cooperative control for multiple interceptors to maximize collateral damage[J]. IFAC-Papers Online, 2018, 51: 56-61.

[16]
王晓芳, 郑艺裕, 林海. 多导弹协同作战制导律研究[J]. 弹道学报, 2014, 26(1):61-66.

[17]
马国欣, 张友安. 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.

[18]
张亚南. 多弹编队飞行协同制导方法研究[D]. 哈尔滨: 哈尔滨工业大学, 2014.

[19]
SCHUMACHER C J, KHARGONEKAR P P. Stability analysis of a missile control system with a dynamic inversion controller[J]. Journal of Guidance, Control, and Dynamics, 1998, 21(3): 508-514

[20]
苏身榜, 张友安. 动态逆方法在空空导弹控制系统设计中的应用[J]. 海军航空工程学院学报, 2003, 18(6):601-604.

[21]
李春文, 冯元琨. 多变量非线性控制的逆系统方法[M]. 北京: 清华大学出版社, 1991.

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