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Longitudinal optimal analytical midcourse guidance for cruise-glide integrated hypersonic vehicles

Xin Li Guangbin Cai Hui Xu Jianwen Zhu Chaoxu Mu

Defence Technology(防务技术)2025，Vol.50Issue(8)：P.288-303,16.

Defence Technology(防务技术)2025，Vol.50Issue(8)：P.288-303,16.DOI:10.1016/j.dt.2025.04.020

Longitudinal optimal analytical midcourse guidance for cruise-glide integrated hypersonic vehicles

Xin Li ¹Guangbin Cai ¹Hui Xu ¹Jianwen Zhu ²Chaoxu Mu³

作者信息

1. College of Missile Engineering,Rocket Force University of Engineering,Xi''an,710025,China
2. College of Missile Engineering,Rocket Force University of Engineering,Xi''an,710025,China School of Aerospace Science and Technology,Xidian University,Xi''an,710025,China
3. School of Electrical and Information Engineering,Tianjin University,Tianjin,300072,China
折叠

摘要

关键词

Cruise-glide integrated hypersonic vehicle/Optimal guidance/Velocity control/Costate variable/Longitudinal analytical solution

分类

航空航天

引用本文复制引用

Xin Li,Guangbin Cai,Hui Xu,Jianwen Zhu,Chaoxu Mu..Longitudinal optimal analytical midcourse guidance for cruise-glide integrated hypersonic vehicles[J].Defence Technology(防务技术),2025,50(8):P.288-303,16.

基金项目

supported by the National Natural Science Foundation of China(Grant Nos.62473374,62403487 and U2441243). （Grant Nos.62473374,62403487 and U2441243）

Defence Technology(防务技术)

ISSN：2096-3459

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