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基于非数据通信的导弹编队制导律算法
引用本文: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.
作者姓名:黄伟  徐建城  吴华兴  李俊兵
作者单位:西北工业大学电子信息学院,陕西西安710072;空军工程大学航空航天工程学院,陕西西安710038;西北工业大学电子信息学院,陕西西安,710072;空军工程大学航空航天工程学院,陕西西安,710038
基金项目:国家自然科学基金项目(61472441)
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
收稿时间:2017-10-13

Missile Formation Guidance Algorithm Independent of Data Communication
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.
Authors:HUANG Wei  XU Jian-cheng  WU Hua-xing  LI Jun-bing
Affiliation:(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)
Abstract:To solve the control problem of missilc 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.
Keywords:missile  guidance law  relative motion parameter  closed loop control system  missile control force  general design of formation  
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