Cooperative Guidance Law Design for Simultaneous Attack with Multiple Missiles Against a Maneuvering Target

被引：0

作者：

ZHOU Jialing ^{[1
,2
]}

Lü Yuezu ^{[3
]}

LI Zhongkui ^{[3
]}

YANG Jianying ^{[3
]}

机构：

[1] Ministerial Key Laboratory of ZNDY, School of Mechanical Engineering, Nanjing University of Science and Technology

[2] National Defense Key Laboratory of Science and Technology on Electromagnetic Scattering, the 802 Institute of Shanghai Academy of Space Flight Technology, the Eighth Academy of China Aerospace Science and Technology Corporation

[3] State Key Laboratory for Turbulence and Complex Systems, Department of Mechanics and Engineering Science, College of Engineering, Peking University

来源：

Journal of Systems Science & Complexity | 2018年 / 31卷 / 01期

基金：

中国国家自然科学基金;

关键词：

consensus problem; distributed control; guidance law design; simultaneous attack;

D O I：

暂无

中图分类号：

TJ765.3 [制导];

学科分类号：

081105 ;

摘要：

This paper considers the simultaneous attack problem of multiple missiles against a maneuvering target. Different from most of the existing literature in which the simultaneous attack problem is formulated as a consensus problem of missiles’ time-to-go estimates, this paper formulates it as the consensus problem of missiles’ ranges-to-go. Based on this strategy, novel distributed guidance laws are proposed to solve the simultaneous attack problem with the target of unknown maneuverability.Adaptive control method is introduced to estimate the upper bound of the target’s acceleration. The effectiveness of the proposed guidance laws is verified both theoretically and numerically.

引用

页码：287 / 301

页数：15

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