Research on the Simulation Technology for multi-aerocraft cooperative guidance

doi:10.16182/j.issn1004731x.joss.19-FZ0355

Journal of System Simulation ›› 2019, Vol. 31 ›› Issue (12): 2775-2780.doi: 10.16182/j.issn1004731x.joss.19-FZ0355

Previous Articles Next Articles

Research on the Simulation Technology for multi-aerocraft cooperative guidance

Li Jing^1,2, Han Jian², Zhang Qing^1,2

1. Science and Technology on Complex System Control and Intelligent Agent Cooperation Laboratory, Beijing 100074, China;
2. Beijing Electromechanical Engineering Institute, Beijing 100074, China

Received:2019-05-10 Revised:2019-07-20 Published:2019-12-13

Abstract

Abstract: The formal system of multi- aerocraft cooperative simulation system is identified as the discrete event system & different equation system specifications (DEV&DESS) through the analysis of the composition and running mechanism. The running control problem of cooperative simulation system is transformed into simulation control problem of a specific DEV&DESS system. A dynamic operation control method for cooperative guidance simulation system based on coordinator is proposed, and this method is validated by real-time mathematical simulation experiments.

Key words: cooperative engagement, cooperative guidance, HIL (hardware-in-the-loop) simulation, DEV & DESS

CLC Number:

TP278A

Li Jing, Han Jian, Zhang Qing. Research on the Simulation Technology for multi-aerocraft cooperative guidance[J]. Journal of System Simulation, 2019, 31(12): 2775-2780.

References

[1] 李健. 浅议武器协同作战系统[J]. 现代导航, 2012(1): 73-79.
Li Jian.Analysis on weapon cooperative engagement system[J]. Modern Navigation, 2012(1): 73-79.
[2] Angelopoulou A, Mykoniatis K.UTASiMo: a simulation -based tool for task analysis[J]. Simulaion: Transactions of the society for Modeling and simulation International (S0037-5497), 2018, 94(I): 43-54.
[3] Dobson G B, Carley K M.Cyber-FIT: An Agent-based Modelling Approach to simulating cyber warfare[R]. SBP-BRIMS 2017, LNCS 10354, 2017: 139-148.
[4] 曾华, 樊波, 倪磊, 等. 多导弹协同作战目标分配方法研究[J]. 飞航导弹, 2016(9): 75-79.
Zeng Hua, Fan Bo, Ni Lei, et al.Target allocation methods for cooperative engagement of multiple missiles[J]. Cruising Missile, 2016(9): 75-79.
[5] 刘凌慧, 王元斌. 编队协同作战概念及指标体系[C]. 中国造船工程学会电子技术学术委员会2006学术年会论文集. 北京:中国造船工程学会, 2006: 122-124.
Liu Linghui, Wang Yuanbin.Concept and specification system of formation cooperative engagement[C]. Proceedings of 2006 Annual Conference of Electronic Technology Academic Committee of the Chinese Society of Naval Architects and Marine Angineers. Beijing: the Chinese Society of Naval Architects and Marine Angineers . 2006: 122-124.
[6] Mustafee N, Powell J H.From hybrid simulation to hybrid system modelling[C]. Proceedings of the 2017 Winter Simulation Conference. Las Vegas,USA:IEEE,: 2017: 1430-1439.
[7] Zeigler B P, Kim T G, Praehofer H.建模与仿真理论之集成离散事件与连续复杂动态系统[M]. 北京: 电子工业出版社, 2017.
Bernard P Zeigler, Tag Gon Kim, Herbert Praehofer.Theory of modeling and simulation: integrating discrete event and continuous complex dynamic systems[M]. Beijing: Publishing House of Electronics Industry, 2017.
[8] 王涛, 胡军, 黄克明. 多无人机协同作战系统运用方式研究[J]. 舰船电子工程, 2015(3): 4-7.
Wang Tao, Hu Jun, Huang Keming.Application methods of Multidrone cooperative engagement[J]. Ship Electronic Engineering, 2015(3): 4-7.
[9] 朱爱平, 叶蕾. 战术战斧导弹武器控制系统[J]. 飞航导弹, 2011(9): 61-66.
Zhu Aiping, Ye Lei.Weapon control system of tactical Tomahawk missile[J]. Cruising Missile, 2011(9): 61-66.

Research on the Simulation Technology for multi-aerocraft cooperative guidance

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 2

Recommended Articles

Metrics

Comments

[1]	Wan Jiaqing, Wang Pengfei, Tang Junlin, Zhang Dong, Li Xinguo. Research on Hybrid Deployment Strategy and Model for Key Position Air-defense Based on Multi-weapon Platforms [J]. Journal of System Simulation, 2021, 33(8): 1754-1765.
[2]	Li Bohao, Wu Yunjie. LSTM Model for Trajectory Design of Missile-Borne BFSAR Imaging Guidance [J]. Journal of System Simulation, 2019, 31(12): 2696-2701.