Optimal Design of Guidance Law for Missile Launch with Large Off-Axis Angle

LI Ruikang, CHEN Miao, ZHONG Yongjian

Aerospace Control ›› 2024, Vol. 42 ›› Issue (1) : 58-64.

PDF(2050 KB)
Email Alert　 RSS
PDF(2050 KB)
Aerospace Control ›› 2024, Vol. 42 ›› Issue (1) : 58-64.
Test, Launch and Control

Optimal Design of Guidance Law for Missile Launch with Large Off-Axis Angle

    {{javascript:window.custom_author_en_index=0;}}
  • {{article.zuoZhe_EN}}
Author information +
History +

HeighLight

{{article.keyPoints_en}}

Abstract

{{article.zhaiyao_en}}

Key words

QR code of this article

Cite this article

EndNote

Ris (Procite)

Bibtex

Download Citations
{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2024, 42(1): 58-64

References

Publishing order | Descend order by publishing year | Descend order by cited within

References

{{article.reference}}

Funding

RIGHTS & PERMISSIONS

{{article.copyrightStatement_en}}
{{article.copyrightLicense_en}}
PDF(2050 KB)

Accesses

Citation

Detail
Sections
Recommended
　 Copyright © Aerospace Control, All Rights Reserved.
Tel: 010-68762264、68388585　
E-mail：htkz2013@163.com
Powered by Beijing Magtech Co. Ltd,.

/

〈 〉