Analysis of Non-synchronous Error of Gyros' Effect on Attitude Update

WENG  Jun; QIN  Yongyuan; ZHANG  Qiang; LIU  Zhenbo

doi:10.15892/j.cnki.djzdxb.2015.05.002

WENG Jun, QIN Yongyuan, ZHANG Qiang, LIU Zhenbo

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2015, Vol. 35 ›› Issue (5) : 5-8,12.

PDF(215 KB)

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2015, Vol. 35 ›› Issue (5) : 5-8,12. DOI: 10.15892/j.cnki.djzdxb.2015.05.002

MISSILES AND GUIDANCE TECHNOLOGY

Analysis of Non-synchronous Error of Gyros' Effect on Attitude Update

{{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}}, 2015, 35(5): 5-8,12 https://doi.org/10.15892/j.cnki.djzdxb.2015.05.002

References

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

References

Funding

RIGHTS & PERMISSIONS

PDF(215 KB)

Accesses

Citation

Detail

Sections

Recommended

Received	Published
2014-10-29	2015-10-20
Issue Date
2025-05-28

Please choose a citation manager

Content to export