Design of Integrated Flight Test for Avionics System Based on Test State Point Matrix

LI Jing, ZHANG Xingguo, CHEN Yu

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2020, Vol. 40 ›› Issue (1) : 31-34.

PDF(673 KB)
PDF(673 KB)
Journal of Projectiles, Rockets, Missiles and Guidance ›› 2020, Vol. 40 ›› Issue (1) : 31-34. DOI: 10.15892/j.cnki.djzdxb.2020.01.007

Design of Integrated Flight Test for Avionics System Based on Test State Point Matrix

    {{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

Download Citations
{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2020, 40(1): 31-34 https://doi.org/10.15892/j.cnki.djzdxb.2020.01.007

References

References

{{article.reference}}

Funding

RIGHTS & PERMISSIONS

{{article.copyrightStatement_en}}
{{article.copyrightLicense_en}}
PDF(673 KB)

Accesses

Citation

Detail

Sections
Recommended

/