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

doi:10.3969/j.issn.1000-1093.2019.04.001

Abstract

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

CLC Number:

TJ765.3⁺1

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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第40卷
第4期2019 年4月兵工学报ACTA
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