Research on spin rate design method for flight vehicles based on dynamic stability criterion

HUANG Hao, DU Lifu, XUE Donglin, WANG Junzhe, WEI Changzhu

Aerospace Control ›› 2025, Vol. 43 ›› Issue (6) : 74-82.

PDF(2074 KB)
Email Alert　 RSS
PDF(2074 KB)
Aerospace Control ›› 2025, Vol. 43 ›› Issue (6) : 74-82.
Test， Launch and Control

Research on spin rate design method for flight vehicles based on dynamic stability criterion

    {{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}}, 2025, 43(6): 74-82

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(2074 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,.

/

〈 〉