[go: up one dir, main page]
More Web Proxy on the site http://driver.im/ skip to main content
10.1145/3459104.3459108acmotherconferencesArticle/Chapter ViewAbstractPublication PagesiseeieConference Proceedingsconference-collections
research-article

Research on Availability Model of Test Aircraft Mission System Based on Mission

Published: 20 July 2021 Publication History

Abstract

The flight test of transport aircraft is an important segment in the process of aircraft development. In the effectiveness evaluation architecture of the test aircraft mission system, the availability of the test aircraft mission system is not only an important basis for measuring the system in an executable mission state but also an important evaluation parameter for the effectiveness of the aircraft and its system in completing the mission. Based on WSEIAC system effectiveness evaluation model, this paper analyzes the availability of test aircraft and its system in mission, and proposes a feasible availability analysis model based on the mission characteristics of flight tests.

References

[1]
Wei L, Ning M, Wei P . The Effectiveness Evaluation Model of Radar Jamming System Based on, WSEIAC Model[C]// Control & Decision Conference. IEEE, 2008.
[2]
Fowler P H . Analytic Justification of the WSEIAC Formula[J]. IEEE Transactions on Reliability, 1969, R-18(1):29-29.
[3]
Nicolosi F, Marco A D, Vecchia P D. Flight Tests, Performances, and Flight Certification of a Twin-Engine Light Aircraft [J]. Journal of Aircraft, 2011, 48(1):177-192.
[4]
Hong-Xiao Z, Cheng-Hong W. Operational Availability of Surface to Air Missile [J]. Modern Defence Technology, 2015.
[5]
Zhang Tingliang, Chen Lixin. Methods for conducting efficiency evaluation and operational analysis of military helicopter[M]. Beijing: National defense industry press, 2013.
[6]
Borovkov A A . Probability Theory[M]. Springer London, 2013.
[7]
Lou S C. Analysis of surface to air missile weapon system [M]. Beijing: National defense industry press, 2013.
[8]
Y.-Q. Zhao, Q. Mai, Q.-Y. Xu. Dependability modeling research of air-defense missile weapon systems[J]. Systems Engineering & Electronics, 2016, 38(12):2777-2784.

Recommendations

Comments

Please enable JavaScript to view thecomments powered by Disqus.

Information & Contributors

Information

Published In

cover image ACM Other conferences
ISEEIE 2021: 2021 International Symposium on Electrical, Electronics and Information Engineering
February 2021
644 pages
ISBN:9781450389839
DOI:10.1145/3459104
Permission to make digital or hard copies of all or part of this work for personal or classroom use is granted without fee provided that copies are not made or distributed for profit or commercial advantage and that copies bear this notice and the full citation on the first page. Copyrights for components of this work owned by others than ACM must be honored. Abstracting with credit is permitted. To copy otherwise, or republish, to post on servers or to redistribute to lists, requires prior specific permission and/or a fee. Request permissions from [email protected]

Publisher

Association for Computing Machinery

New York, NY, United States

Publication History

Published: 20 July 2021

Permissions

Request permissions for this article.

Check for updates

Qualifiers

  • Research-article
  • Research
  • Refereed limited

Conference

ISEEIE 2021

Contributors

Other Metrics

Bibliometrics & Citations

Bibliometrics

Article Metrics

  • 0
    Total Citations
  • 23
    Total Downloads
  • Downloads (Last 12 months)2
  • Downloads (Last 6 weeks)0
Reflects downloads up to 14 Jan 2025

Other Metrics

Citations

View Options

Login options

View options

PDF

View or Download as a PDF file.

PDF

eReader

View online with eReader.

eReader

HTML Format

View this article in HTML Format.

HTML Format

Media

Figures

Other

Tables

Share

Share

Share this Publication link

Share on social media