Mission reliability model of spacecraft launch based on bisimulation of continuous-time Markov processes

DONG Xue-jun, WU Xiao-yue, CHEN Ying-wu

Systems Engineering - Theory & Practice ›› 2012, Vol. 32 ›› Issue (10) : 2323-2331.

PDF(618 KB)
PDF(618 KB)
Systems Engineering - Theory & Practice ›› 2012, Vol. 32 ›› Issue (10) : 2323-2331. DOI: 10.12011/1000-6788(2012)10-2323

Mission reliability model of spacecraft launch based on bisimulation of continuous-time Markov processes

    {{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}}. Systems Engineering - Theory & Practice, 2012, 32(10): 2323-2331 https://doi.org/10.12011/1000-6788(2012)10-2323

References

References

{{article.reference}}

Funding

RIGHTS & PERMISSIONS

{{article.copyrightStatement_en}}
{{article.copyrightLicense_en}}
PDF(618 KB)

Accesses

Citation

Detail

Sections
Recommended

/