基于非数据通信的导弹编队制导律算法

doi:10.3969/j.issn.1000-1093.2018.05.010

兵工学报 ›› 2018, Vol. 39 ›› Issue (5): 910-918.doi: 10.3969/j.issn.1000-1093.2018.05.010

基于非数据通信的导弹编队制导律算法

黄伟^1，2，徐建城¹，吴华兴²，李俊兵²

（1.西北工业大学电子信息学院，陕西西安 710072; 2.空军工程大学航空航天工程学院，陕西西安 710038）

收稿日期:2017-10-13 修回日期:2017-10-13 上线日期:2018-06-22
通讯作者: 徐建城(1957—)，男，教授，博士生导师 E-mail:xujchg@nwpu.edu.cn
作者简介:黄伟(1980—)，男，副教授，博士研究生。E-mail：huangwei800519@163.com
基金资助:
国家自然科学基金项目（61472441）

Missile Formation Guidance Algorithm Independent of Data Communication

HUANG Wei^1,2, XU Jian-cheng¹, WU Hua-xing², LI Jun-bing²

(1.School of Electronics and Information, Northwestern Polytechnic University, Xi'an 710072, Shaanxi, China;2.College of Aeronautics and Astronautics Engineering, Air Force Engineering University, Xi'an 710038, Shaanxi, China)

Received:2017-10-13 Revised:2017-10-13 Online:2018-06-22

摘要/Abstract

摘要： 针对无数据链支持的作战条件下，仅利用导弹主动雷达导引头量测的弹间相对位置和相对速度等参数，基于多智能体一致性理论，提出一种适用于解决领从结构导弹编队队形控制问题的制导律算法。该算法在实现过程中无需各弹之间进行数据通信，即无需弹间数据链传递编队成员的绝对位置信息，就可实现既定队形的收敛和速度一致。应用代数图论证明了闭环制导控制系统的渐进稳定性，并基于坐标变换和导弹运动学方程，建立了编队控制过程中所需的导弹控制力模型。仿真结果表明该算法有效，适用于导弹编队系统的总体设计。

关键词: 导弹, 制导律, 相对运动参数, 闭环控制系统, 导弹控制力, 编队总体设计

Abstract: To solve the control problem of missile formation without support of weapon data-link, a new guidance algorithm for systems grouped by the leader-follower structure based on multi-agent consensus theory is proposed, which only requires the motion parameters, such as relative distance and relative speed among missiles, which can be measured by the followers’ active radar seeker. The proposed algorithm needs no data communication among missiles and absolute positions of formation members, but can make all members approach to ideal positions and consistent velocity simultaneously. Algebraic graph theory is employed to prove the asymptotic stability of closed loop control system, and a model of required force for missile formation control is built based on coordinate conversion and missile motion equation. Simulated results are used to verify the validity of the proposed algorithm and its application prospect for general design of missile formation system. Key

Key words: missile, guidancelaw, relativemotionparameter, closedloopcontrolsystem, missilecontrolforce, generaldesignofformation

中图分类号:

TJ765.3⁺39

黄伟，徐建城，吴华兴，李俊兵. 基于非数据通信的导弹编队制导律算法[J]. 兵工学报, 2018, 39(5): 910-918.

HUANG Wei, XU Jian-cheng, WU Hua-xing, LI Jun-bing. Missile Formation Guidance Algorithm Independent of Data Communication[J]. Acta Armamentarii, 2018, 39(5): 910-918.

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第39卷
第5期2018 年5月兵工学报ACTA
ARMAMENTARIIVol.39No.5May2018

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基于非数据通信的导弹编队制导律算法

Missile Formation Guidance Algorithm Independent of Data Communication

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