Reliability Modelling and Analysis of Satellite Propulsion System Based on Reliability Block Diagram and Extended Object-Oriented Petri Net
Modern satellite propulsion systems are generally designed to fulfill multiphase-missions.Traditional reliability modelling methods have problems of inadequate depict capacity considering complex systems such as satellite propulsion system.An extended object-oriented Petri net（EOOPN）method was propo...
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| Published in | 东华大学学报（英文版） Vol. 32; no. 6; pp. 1001 - 1005 |
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| Main Author | |
| Format | Journal Article |
| Language | English |
| Published |
College of Mechanical and Electronic Engineering, University of Electronic Science and Technology, Chengdu 611731, China
31.12.2015
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| Subjects | |
| Online Access | Get full text |
| ISSN | 1672-5220 |
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| Summary: | Modern satellite propulsion systems are generally designed to fulfill multiphase-missions.Traditional reliability modelling methods have problems of inadequate depict capacity considering complex systems such as satellite propulsion system.An extended object-oriented Petri net（EOOPN）method was proposed to facilitate the reliability modelling of satellite propulsion system in the paper.The proposed method was specified for modelling of phased mission system,and it could be implemented by generating combination of Petri net（PN）principles and object-oriented（OO）programming.The effectiveness of the proposed method was demonstrated through the reliability modelling of a satellite propulsion system with EOOPN.The major advantage of the proposed method is that the dimension of net model can be reduced significantly,and phased mission system at system,phase,or component levels can be respectively depicted.Furthermore,the state-space explosion problem is solved by the proposed EOOPN model efficiently. |
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| Bibliography: | 31-1920/N ZHOU Hang, HUANG Hong-zhong（ College of Mechanical and Electronic Engineering, University of Electronic Science and Technology, Chengdu 611731, China） satellite propulsion system extended object-oriented Petri net（EOOPN） object-oriented programming reliability modeling reliability analysis Modern satellite propulsion systems are generally designed to fulfill multiphase-missions.Traditional reliability modelling methods have problems of inadequate depict capacity considering complex systems such as satellite propulsion system.An extended object-oriented Petri net（EOOPN）method was proposed to facilitate the reliability modelling of satellite propulsion system in the paper.The proposed method was specified for modelling of phased mission system,and it could be implemented by generating combination of Petri net（PN）principles and object-oriented（OO）programming.The effectiveness of the proposed method was demonstrated through the reliability modelling of a satellite propulsion system with EOOPN.The major advantage of the proposed method is that the dimension of net model can be reduced significantly,and phased mission system at system,phase,or component levels can be respectively depicted.Furthermore,the state-space explosion problem is solved by the proposed EOOPN model efficiently. |
| ISSN: | 1672-5220 |