Proceedings of the 2017 2nd International Conference on Electrical, Automation and Mechanical Engineering (EAME 2017)

Hazard Analysis and Error Proofing in Spacecraft General Assembly

Authors
Botao Xu, Zhikai Fang, Yugang Liu, Tao Guo, Zhengyi Xiao, Bin Zhang, Weibing Dai
Corresponding Author
Botao Xu
Available Online April 2017.
DOI
10.2991/eame-17.2017.48How to use a DOI?
Keywords
spacecraft general assembly; hazard analysis; error proofing
Abstract

The paper analyzes occurrence of hazardous factors in spacecraft general assembly process, and analyzes the level and effect of hazards in various general assembly units. The methodology of designing error proofing for general assembly is discussed, a database of error control elements is established. Process error analysis and error proofing technological evaluation is studied to ensure the quality of spacecraft general assembly.

Copyright
© 2017, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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Volume Title
Proceedings of the 2017 2nd International Conference on Electrical, Automation and Mechanical Engineering (EAME 2017)
Series
Advances in Engineering Research
Publication Date
April 2017
ISBN
978-94-6252-332-6
ISSN
2352-5401
DOI
10.2991/eame-17.2017.48How to use a DOI?
Copyright
© 2017, the Authors. Published by Atlantis Press.
Open Access
This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

Cite this article

TY  - CONF
AU  - Botao Xu
AU  - Zhikai Fang
AU  - Yugang Liu
AU  - Tao Guo
AU  - Zhengyi Xiao
AU  - Bin Zhang
AU  - Weibing Dai
PY  - 2017/04
DA  - 2017/04
TI  - Hazard Analysis and Error Proofing in Spacecraft General Assembly
BT  - Proceedings of the 2017 2nd International Conference on Electrical, Automation and Mechanical Engineering (EAME 2017)
PB  - Atlantis Press
SP  - 199
EP  - 202
SN  - 2352-5401
UR  - https://doi.org/10.2991/eame-17.2017.48
DO  - 10.2991/eame-17.2017.48
ID  - Xu2017/04
ER  -