帮助 关于我们

返回检索结果

带有不同视场约束的多导弹分布式协同制导
Distributed Cooperative Guidance of Multiple Missiles with Heterogeneous Constraints of Field-of-view

查看参考文献23篇

叶鹏鹏 1   张蛟 2   李银伢 1 *   戚国庆 1   盛安冬 1  
文摘 针对带有不同视场约束的多导弹,提出一种分布式协同制导策略。各导弹以固定周期与网络中的邻居导弹节点交互剩余距离信息,生成一致性误差。根据导弹视场范围和前置角,采用饱和函数将一致性误差生成协同一致律,以确保相关变量实现状态一致。当导弹相关变量状态一致且接近目标后,各导弹断开通信连接,独立导引至目标。依据反馈线性化、图论和矩阵理论,给出协同制导律成立的充分条件。与传统多导弹协同制导研究相比,所提协同制导律能满足导弹各自不同的视场约束要求,且通信负担较小。仿真结果表明,多导弹协同制导实现了对目标的齐射攻击,飞行过程中各导弹能始终锁定目标。
其他语种文摘 Distributed cooperative guidance is proposed for the missiles with heterogeneous constraints of field-of-view.Communication among missiles is periodic,and only the information of range-to-go is exchanged among the neighboring missiles in the network to generate a consensus error.Based on the missile's field-of-view and the lead angle,a saturation function is used,and a distributed consensus protocol is developed by the consensus error so that the coordination variables can reach consensus.Multiple missiles are disconnected to the communication network and are guided to a target independently when they approach a target and their coordination variables are consistent.Based on feedback linearization,graph and matrix theories,the sufficient conditions are established to make the multiple missiles realize the cooperative attack under the cooperative guidance law.Compared with the conventional cooperative guidance of multiple missiles,the proposed cooperative guidance law can satisfy each missile's constraints of heterogeneous field-of-views,and the communication effort is easy.Simulated results show that the salvo attack of multiple missiles is achieved,and the target is locked on during each missile's flight.
来源 兵工学报 ,2019,40(3):506-515 【核心库】
DOI 10.3969/j.issn.1000-1093.2019.03.008
关键词 导弹 ; 协同制导 ; 不同视场约束 ; 分布式 ; 饱和函数
地址

1. 南京理工大学自动化学院, 江苏, 南京, 210094  

2. 63961部队, 北京, 100012

语种 中文
文献类型 研究性论文
ISSN 1000-1093
学科 武器工业
基金 国家自然科学基金项目
文献收藏号 CSCD:6473874

参考文献 共 23 共2页

1.  滕克难. 网络化舰空导弹超视距协同反导的关键技术. 电光与控制,2012,19(12):1-5 CSCD被引 3    
2.  关世义. 飞航导弹突防技术与战术导论. 战术导弹技术,2006(4):1-8 CSCD被引 7    
3.  曾家有. 多平台舰舰导弹饱和攻击几个协同问题与模型. 兵工学报,2014,35(2):256-261 CSCD被引 12    
4.  赵建博. 多导弹协同制导研究综述. 航空学报,2017,38(1):17-29 CSCD被引 13    
5.  Jeon I S. Impact-time-control guidance law for anti-ship missiles. IEEE Transactions on Control Systems Technology,2006,14(2):260-266 CSCD被引 183    
6.  Hou D L. Finite-time cooperative guidance laws for multiple missiles with acceleration saturation constraints. IET Control Theory & Applications,2015,9(10):1525-1535 CSCD被引 25    
7.  Zhou J L. Distributed guidance law design for cooperative simultaneous attacks with multiple missiles. Journal of Guidance, Control, and Dynamics,2016,39(10):2439-2447 CSCD被引 43    
8.  Zhao Q L. Distributed group cooperative guidance for multiple missiles with fixed and switching directed communication topologies. Nonlinear Dynamics,2017,90(4):2507-2523 CSCD被引 7    
9.  叶鹏鹏. 非持续连通通信拓扑下的多导弹协同制导. 兵工学报,2018,39(3):474-484 CSCD被引 9    
10.  Lee C H. A hybrid guidance law for a strapdown seeker to maintain lock-on conditions against high speed targets. Journal of Electrical Engineering & Technology,2013,8(1):190-196 CSCD被引 3    
11.  Zhang Y A. Impact time control guidance law with field of view constraint. Aerospace Science and Technology,2014,39:361-369 CSCD被引 21    
12.  Jeon I S. Impact-time-control guidance law with constraints on seeker look angle. IEEE Transactions on Aerospace and Electronic Systems,2017,53(5):2621-2627 CSCD被引 20    
13.  Chen X T. Nonsingular sliding-mode control for field-of-view constrained impact time guidance. Journal of Guidance Control & Dynamics,2018,41(3):1-9 CSCD被引 26    
14.  张春妍. 带落角和时间约束的网络化导弹协同制导律. 兵工学报,2016,37(3):431-438 CSCD被引 38    
15.  吕腾. 带视线角约束的多导弹有限时间协同制导律. 兵工学报,2018,39(2):305-314 CSCD被引 19    
16.  Zhang Y A. A distributed cooperative guidance law for salvo attack of multiple anti-ship missiles. Chinese Journal of Aeronautics,2015,28(5):1438-1450 CSCD被引 23    
17.  Wang X L. Distributed cooperative guidance of multiple anti-ship missiles with arbitrary impact angle constraint. Aerospace Science and Technology,2015,46:299-311 CSCD被引 28    
18.  赵启伦. 高超武器与常规导弹协同攻击策略可行域研究. 航空学报,2015,36(7):2291-2300 CSCD被引 15    
19.  赵启伦. 拦截高超声速目标的异类导弹协同制导律. 航空学报,2016,37(3):936-948 CSCD被引 30    
20.  张友安. 角度控制与时间控制导引律,2017:53 CSCD被引 1    
引证文献 5

1 李文 速度时变情况下多飞行器时间协同制导方法研究 兵工学报,2020,41(6):1096-1110
CSCD被引 12

2 赵启伦 高抛弹道三维复合协同制导律设计 航空兵器,2021,28(1):26-33
CSCD被引 1

显示所有5篇文献

论文科学数据集
PlumX Metrics
相关文献

 作者相关
 关键词相关
 参考文献相关

版权所有 ©2008 中国科学院文献情报中心 制作维护:中国科学院文献情报中心
地址:北京中关村北四环西路33号 邮政编码:100190 联系电话:(010)82627496 E-mail:cscd@mail.las.ac.cn 京ICP备05002861号-4 | 京公网安备11010802043238号