| Reliability evaluation of PMS considering coupling effect of functional and physical dependency |
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| 作者姓名： | Ying CHEN Qichao MA Rui KANG |
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| 作者单位： | Science and Technology on Reliability and Environmental Engineering Laboratory,Beihang University,Beijing 100083,China;Institute of Electronic Engineering,China Academy of Engineering Physics,Mianyang 621999,China |
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| 基金项目： | funded by the National Natural Science Foundation of China (No. 61503014)； |
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| 摘 要： | Aviation and aerospace system are typical Phased-Mission Systems(PMSs) featured with varying configuration, phased load condition and cross phase failure correlation. The coupling effect of Functional Dependency(FDEP) and Physical Dependency(PDEP) has a unique influence on the failure behavior of PMS. In this article, the coupling effect is analyzed, and the degradation of components is modeled with the positive drift wiener process, in which the drift coefficient is related to environmental con...
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| 收稿时间： | 14 September 2020 |
Reliability evaluation of PMS considering coupling effect of functional and physical dependency |
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| Ying CHEN,Qichao MA,Rui KANG.Reliability evaluation of PMS considering coupling effect of functional and physical dependency[J].Chinese Journal of Aeronautics,2022,35(2):154-163. |
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| Authors: | Ying CHEN Qichao MA Rui KANG |
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| Institution: | 1. Science and Technology on Reliability and Environmental Engineering Laboratory, Beihang University, Beijing 100083, China;2. Institute of Electronic Engineering, China Academy of Engineering Physics, Mianyang 621999, China |
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| Abstract: | Aviation and aerospace system are typical Phased-Mission Systems (PMSs) featured with varying configuration,phased load condition and cross phase failure correlation.The coupling effect of Functional Dependency (FDEP) and Physical Dependency (PDEP) has a unique influence on the failure behavior of PMS.In this article,the coupling effect is analyzed,and the degradation of components is modeled with the positive drift wiener process,in which the drift coefficient is related to environmental conditions and operation stress.Finally,failure behavior and system reli-ability are simulated.An avionics controller is studied as a case,with the degradation time distri-bution model and simulation algorithm,the coupling effect and dynamical system reliability can be achieved.Results show that this modeling method can describe the coupling effects of FDEP and PDEP and their influence on the failure behavior and reliability of the PMS system. |
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| Keywords: | Functional dependency Phased-mission system Physical dependency Reliability evaluation Stochastic degradation process |
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