Analytical Near-Optimal Distributed Consensus for Cooperative Salvo Guidance

被引:0
作者
Tao, Hong [1 ]
Li, Hongyan [2 ]
Wang, Jiang [1 ]
Song, Tao [1 ]
Lin, Defu [1 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
[2] Beihang Univ, Sch Elect Informat Engn, Beijing 100191, Peoples R China
基金
中国博士后科学基金;
关键词
Proportional Navigation; Optimal Control Problem; Numerical Simulation; Model Predictive Control; Guidance; Navigation; and Control Systems; Missile Guidance and Control; Flight Path Angle; Equations of Fluid Dynamics; Aerodynamics; Aerodynamically Controlled Missiles; MULTIAGENT SYSTEMS; ATTACK;
D O I
10.2514/1.G007869
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:1499 / 1506
页数:8
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