Research on Parachute and Aircraft Transition Control Algorithm for Coaxial Rotor Vehicle

XU Jiulong, HAO Yongping

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2022, Vol. 42 ›› Issue (4) : 51-56.

PDF(2127 KB)
JPRMG
PDF(2127 KB)
Journal of Projectiles, Rockets, Missiles and Guidance ›› 2022, Vol. 42 ›› Issue (4) : 51-56. DOI: 10.15892/j.cnki.djzdxb.2022.04.010

Research on Parachute and Aircraft Transition Control Algorithm for Coaxial Rotor Vehicle

    {{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}}, 2022, 42(4): 51-56 https://doi.org/10.15892/j.cnki.djzdxb.2022.04.010

References

List( Publishing order | Descend order by publishing year | Descend order by cited within ) Chart analysis

References

{{article.reference}}

Funding

RIGHTS & PERMISSIONS

{{article.copyrightStatement_en}}
{{article.copyrightLicense_en}}
PDF(2127 KB)

Accesses

Citation

Detail
Sections
Recommended
陕ICP备2025069823号-1

Copyright © Journal of Projectiles, Rockets, Missiles and Guidance, All Rights Reserved.
Address: No.10 East Zhangba Road, Xi'an PRC　 Zip Code: 710065
Tel:（+86）-（29）88293184，（+86）-（29）88293167　 E-mail: djxb1980@163.com
Powered by Beijing Magtech Co. Ltd,.

/

〈 〉