Design of Attitude Autopilots with Pseudo Angle of Attack Basedon Parameter Space Method

WANG  Shuaiwei; MA  Qinghua; ZHENG  Jianqiang; YANG  Shujun; CHENG  Pengfei; LIANG  Yiming

doi:10.15892/j.cnki.djzdxb.2018.02.020

WANG Shuaiwei, MA Qinghua, ZHENG Jianqiang, YANG Shujun, CHENG Pengfei, LIANG Yiming

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2018, Vol. 38 ›› Issue (2) : 88-92.

PDF(721 KB)

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2018, Vol. 38 ›› Issue (2) : 88-92. DOI: 10.15892/j.cnki.djzdxb.2018.02.020

Design of Attitude Autopilots with Pseudo Angle of Attack Basedon Parameter Space Method

{{article.zuoZhe_EN}}

Author information +

History +

HeighLight

Abstract

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}}, 2018, 38(2): 88-92 https://doi.org/10.15892/j.cnki.djzdxb.2018.02.020

References

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

References

Funding

RIGHTS & PERMISSIONS

PDF(721 KB)

Accesses

Citation

Detail

Sections

Recommended

Received	Published
2017-08-31	2018-04-20
Issue Date
2025-05-28

Please choose a citation manager

Content to export