基于领弹-从弹架构的无导引头导弹协同定位与制导方法

doi:10.3969/j.issn.1000-1093.2019.04.001

兵工学报 ›› 2019, Vol. 40 ›› Issue (4): 673-679.doi: 10.3969/j.issn.1000-1093.2019.04.001

基于领弹-从弹架构的无导引头导弹协同定位与制导方法

赵建博¹，杨树兴²，熊芬芬¹

(1.北京理工大学宇航学院, 北京 100081; 2.西安现代控制技术研究所, 陕西西安 710065)

收稿日期:2018-06-29 修回日期:2018-06-29 上线日期:2019-06-10
通讯作者: 杨树兴(1962—),男,教授，博士生导师 E-mail:yangshx@bit.edu.cn
作者简介:赵建博(1991—),男,博士研究生。E-mail: zhjb_cn@126.com
基金资助:
国家自然科学基金项目（11532002）

Cooperative Localization and Guidance for Seeker-less Missile Based on Leader-follower Framework

ZHAO Jianbo¹， YANG Shuxing², XIONG Fenfen¹

(1.School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081， China;2.Xi'an Modern Control and Technology Institute, Xi'an 710065, Shaanxi, China)

Received:2018-06-29 Revised:2018-06-29 Online:2019-06-10

摘要/Abstract

摘要： 针对无导引头导弹在采用现有制导律时定位误差会产生较大脱靶量的问题，通过双领弹的领弹-从弹协同架构，设计了一种协同定位与制导策略，以实现无导引头导弹对静止目标的精确命中。基于扩展卡尔曼滤波，提出了一种无导引头导弹的协同定位方法。该协同定位方法与比例导引结合时存在终止时刻过载指令过大问题，因此设计一种新型变系数比例导引律，分析了变系数比例导引律的制导系数对脱靶量、终止时刻过载与最大过载的影响。仿真结果表明：采用所提出的协同定位方法可减小具有定位误差的无导引头导弹脱靶量，而采用变系数比例导引律可避免终止时刻过载指令过大。

关键词: 导弹制导, 无导引头, 协同定位, 卡尔曼滤波, 变系数比例导引, 领弹, 从弹

Abstract: A novel cooperative localization and guidance approach based on the leader-follower framework with two leaders is proposed to allow the seeker-less missile to hit a stationary target accurately. A cooperative localization method for seeker-less missile is designed based on the extended Kalman filter to enhance the localization accuracy. To address the issue that a large terminal acceleration command is required for the proportional navigation guidance (PNG) law combined with the proposed localization method, a novel PNG law with time-varying navigation gain is presented. The impacts of the guidance parameters on miss distance, terminal acceleration and maximum acceleration are demonstrated through si- mulation. Simulated results show that the large miss distance due to the localization error of seeker-less missile could be reduced by the proposed cooperative localization method, and the large terminal acceleration command could be avoided by PNG law with time-varying navigation gain. Key

Key words: missileguidance, seeker-lessmissile, cooperativelocalization, Kalmanfilter, proportionalnavigationguidancewithtime-varyingnavigationgain, leader, follower

中图分类号:

TJ765.3⁺1

赵建博，杨树兴，熊芬芬. 基于领弹-从弹架构的无导引头导弹协同定位与制导方法[J]. 兵工学报, 2019, 40(4): 673-679.

ZHAO Jianbo， YANG Shuxing, XIONG Fenfen. Cooperative Localization and Guidance for Seeker-less Missile Based on Leader-follower Framework[J]. Acta Armamentarii, 2019, 40(4): 673-679.

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基于领弹-从弹架构的无导引头导弹协同定位与制导方法

Cooperative Localization and Guidance for Seeker-less Missile Based on Leader-follower Framework

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