Guidance law in distributed cooperative air-to-air missile considering detection effectiveness

被引：0
|
作者：
Yang H.-M. [1 ]
Li Y. [1 ]
Zhang F. [1 ]
Wang Y.-C. [1 ]
Li C. [1 ]
机构：
[1] Shanghai Academy of Spaceflight Technology, Shanghai Institute of Mechanical and Electrical Engineering, Shanghai
来源：
Kongzhi Lilun Yu Yingyong/Control Theory and Applications | 2024年 / 41卷 / 04期
关键词：
cooperative detection; distributed control; multi-agent system; optimal control; spatio-temporal cooperative guidance law; virtual guidance point;
D O I：
10.7641/CTA.2023.20055
中图分类号：
学科分类号：
摘要：
With multiple air-to-air missiles intercepting high-speed moving targets against the trajectory as a background, a distributed cooperative mid-guidance law with coordinated detection as the terminal constraint is proposed. By analyzing the error source and the error transmission link, a calculation model of the mid-end handover probability is established, and the collaborative visual field splicing method is studied based on the virtual guide point. In the normal direction of the line of sight, an optimal guidance law based on Gaussian pseudospectral method is designed for the constraint conditions such as position coordination and angle coordination. In the line of sight, based on the second-order multi-agent consistency theory, a distributed time cooperative guidance law is designed, and the Lyapunov functional is constructed to prove that the method can stabilize the system in a finite time, and the upper bound of the consistency time is derived. The simulation results show that the guidance law can enable multiple missiles to reach the designated handover area at the same time with their respective expected line-of-sight angles, realizing the needs of field of view splicing and cooperative detection and effectively improving the probability of middle-end handover. © 2024 South China University of Technology. All rights reserved.
引用
收藏
页码：638 / 648
页数：10
相关论文
共 26 条
  • [1] TANG Mingnan, ZHENG Xuehe, WANG Tianshu, Et al., Handover of guidance from midcourse to terminal in the maneuvering target interception based on multi-platform information, Systems Engineering and Electronics, 39, 12, pp. 2757-2764, (2017)
  • [2] WANG Yanyan, YUAN Jianquan, HAO Mingrui, Et al., Research status and application of the cooperative guidance technology for aerial vehicle swarm systems based on spatiotemporal coordination, Flight Control & Detection, 4, 4, pp. 32-39, (2021)
  • [3] JEON I S, LEE J I, TAHK M J., Homing guidance law for cooperative attack of multiple missiles, Journal of Guidance Control Dynamics, 33, 1, pp. 275-280, (2010)
  • [4] ZHANG Gong, LI Fan, ZHAO Jianhui, Et al., Impact-time-control guidance law for multi-missile cooperative model with mobility of the target considered, Command Control & Simulation, 32, 1, pp. 52-55, (2010)
  • [5] DONG G, PENG J, LIANG Z, Et al., Three-dimensional guidance method for air to ground missile with impact time constraint, Chinese Control Conference, pp. 4917-4921, (2018)
  • [6] DHANANJAY N, GHOSE D., Accurate time-to-go estimation for proportional navigation guidance, Journal of Guidance Control and Dynamics, 37, 4, pp. 1378-1383, (2015)
  • [7] HOU Delong, CHEN Bin, WANG Qing, Et al., Collision avoidance multi-missile distributed cooperative guidance and control, Control Theory & Applications, 31, 9, pp. 1133-1142, (2014)
  • [8] ZHANG Zhenlin, ZHANG Ke, GUO Zhengyu, Et al., Design of a new guidance law for guided multiple missiles, Aero Weaponry, 27, 5, pp. 33-38, (2020)
  • [9] WANG Y, ZHANG X, SHUI Y, Et al., Three-dimensional distributed cooperative guidance law with high reliability communication, International Symposium on Autonomous Systems, pp. 222-226, (2019)
  • [10] ZHOU J, YANG J., Distributed guidance law design for cooperative simultaneous attacks with multiple missiles, Journal of Guidance Control & Dynamics, 39, 10, pp. 1-9, (2016)
123