DocumentCode :
3515405
Title :
Reliability modeling study of in-orbit satellite systems
Author :
Lu, Lianna ; Huang, Hong-Zhong ; Wu, Boyi ; Miao, Qiang ; Xu, Huanwei
Author_Institution :
Sch. of Mechatron. Eng., Univ. of Electron. Sci. & Technol. of China, Chengdu, China
fYear :
2009
fDate :
20-24 July 2009
Firstpage :
1
Lastpage :
4
Abstract :
System reliability modeling is one of the most important reliability modeling methods for satellite system. Based on the reliability characteristics of satellite system, we used reliability block diagram, fault tree, dynamic fault tree, Markov, and Monte Carlo modeling methods to build reliability models and summarize logic relationships of all kinds of modeling methods, the principle of choosing a modeling methods, and application field. The power controller was modeled as an example to specify the modeling effect. This work indicated that the result of satellite system reliability model is accurate and can be better used to solve the reliability modeling problems of large system. This research results is meaningful to the field of in-orbit satellite system reliability modeling.
Keywords :
Markov processes; Monte Carlo methods; artificial satellites; fault trees; Markov modeling; Monte Carlo modeling methods; dynamic fault tree; fault tree; in-orbit satellite systems; power controller; reliability block diagram; reliability modeling; Fault trees; Logic; Maintenance; Monte Carlo methods; Power system modeling; Power system reliability; Predictive models; Reliability engineering; Satellites; System analysis and design; Markov; Monte Carlo; dynamic fault tree; fault tree; reliability block diagram; satellite systems modeling;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability, Maintainability and Safety, 2009. ICRMS 2009. 8th International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-4903-3
Electronic_ISBN :
978-1-4244-4905-7
Type :
conf
DOI :
10.1109/ICRMS.2009.5270252
Filename :
5270252
Link To Document :
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