An Evaluation Method for the Head Accuracy of Inertial Navigation System in Flight Test

doi:10.3969/j.issn.1674-5558.2017.04.002

HUANG Xue-ni, LIU Jun-yuan, YANG Wu

Navigation and Control ›› 2017, Vol. 16 ›› Issue (4) : 7-12.

PDF(3863 KB)

Navigation and Control ›› 2017, Vol. 16 ›› Issue (4) : 7-12. DOI: 10.3969/j.issn.1674-5558.2017.04.002

System and Application

An Evaluation Method for the Head Accuracy of Inertial Navigation System in Flight Test

{{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}}, 2017, 16(4): 7-12 https://doi.org/10.3969/j.issn.1674-5558.2017.04.002

References

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

References

Funding

RIGHTS & PERMISSIONS

PDF(3863 KB)

Accesses

Citation

Detail

Sections

Recommended

Received	Published
2016-11-04	2017-08-05
Issue Date
2020-02-25

Please choose a citation manager

Content to export