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
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2024年 / 47卷 / 07期
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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