Near-Optimal Impact-Vector-Control Guidance

被引：0
|
作者：
Li, Hongyan [1 ]
Wang, Jiang [2 ]
Tao, Hong [2 ]
Lin, Defu [2 ]
机构：
[1] Beihang Univ, Sch Elect Informat Engn, Beijing 100191, Peoples R China
[2] Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2024年 / 47卷 / 09期
基金：
中国博士后科学基金;
关键词：
Guidance; Navigation; and Control Systems; Energy Consumption; Structural Kinematics and Dynamics; Optimal Control Problem; Flight Path Angle; Monte Carlo Simulation; International Organizations; Authorities and Agencies; Homing Guidance; Flight Control Surfaces; Aerodynamically Controlled Missiles; MIDCOURSE GUIDANCE; LAWS;
D O I：
10.2514/1.G008294
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：1965 / 1972
页数：8
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