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

被引：34

作者：

Zhou, Jialing ^{[1
,2
]}

Lu, Yuezu ^{[3
]}

Li, Zhongkui ^{[3
]}

Yang, Jianying ^{[3
]}

机构：

[1] Nanjing Univ Sci & Technol, Sch Mech Engn, Ministerial Key Lab ZNDY, Nanjing 210094, Jiangsu, Peoples R China

[2] China Aerosp Sci & Technol Corp, Acad 8, Natl Def Key Lab Sci & Technol Electromagnet Scat, Shanghai Acad Space Flight Technol,Inst 802, Shanghai 200090, Peoples R China

[3] Peking Univ, Coll Engn, Dept Mech & Engn Sci, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China

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; DISTRIBUTED CONTROL; MULTIAGENT SYSTEMS; VEHICLES; CONSENSUS; TRACKING; AGENTS;

D O I：

10.1007/s11424-018-6317-7

中图分类号：

O1 [数学];

学科分类号：

0701 ; 070101 ;

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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