Analytical Study on the Reliability of Redundancy Architecture for Flight Control Computer Based on Homogeneous Markov Process

In order to analyze the reliability of redundancy architecture for flight control computer, this paper gives the analytical study on the reliability based on the Homogeneous Markov Process in “Triplex Channels & Single Module”and “Double Channels & Do...

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Main Authors: Yaoming Zhou, Chenghao Lin, Yaolong Liu, Hongzhe Xu
Format: Article
Language:English
Published: IEEE 2018-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/8307055/
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spelling doaj-20bd1d9df9fc4ed8a9d539e46197e3f12021-03-29T21:00:53ZengIEEEIEEE Access2169-35362018-01-016182901829810.1109/ACCESS.2018.28128198307055Analytical Study on the Reliability of Redundancy Architecture for Flight Control Computer Based on Homogeneous Markov ProcessYaoming Zhou0https://orcid.org/0000-0003-0410-327XChenghao Lin1Yaolong Liu2Hongzhe Xu3School of Aeronautic Science and Engineering, Beihang University, Beijing, ChinaSchool of Aeronautic Science and Engineering, Beihang University, Beijing, ChinaNiedersächsisches Forschungszentrum für Luftfahrt, Braunschweig, GermanyShanghai Aircraft Design and Research Institute, Shanghai, ChinaIn order to analyze the reliability of redundancy architecture for flight control computer, this paper gives the analytical study on the reliability based on the Homogeneous Markov Process in “Triplex Channels & Single Module”and “Double Channels & Double Modules.”The paper analyzes the effect of fault rate and fault coverage rate on system reliabilities and MTTFs (mean time to failures). The index of fault tolerant capability is proposed. The analyzing results show that, for different redundancy architectures, the fault coverage rate or the branch fault rate have different effects on the reliability. Especially, the influence of the branch fault rate is more significant. In addition, the fault tolerant capability of the redundant system to multiple faults is determined by the system architecture scheme and the fault coverage rate. The results show that the method proposed in this paper can analyze reliability of redundancy architecture effectively.https://ieeexplore.ieee.org/document/8307055/Flight control computerredundancy architectureMarkovreliabilityfault tolerant capabilityfault rate
collection DOAJ
language English
format Article
sources DOAJ
author Yaoming Zhou
Chenghao Lin
Yaolong Liu
Hongzhe Xu
spellingShingle Yaoming Zhou
Chenghao Lin
Yaolong Liu
Hongzhe Xu
Analytical Study on the Reliability of Redundancy Architecture for Flight Control Computer Based on Homogeneous Markov Process
IEEE Access
Flight control computer
redundancy architecture
Markov
reliability
fault tolerant capability
fault rate
author_facet Yaoming Zhou
Chenghao Lin
Yaolong Liu
Hongzhe Xu
author_sort Yaoming Zhou
title Analytical Study on the Reliability of Redundancy Architecture for Flight Control Computer Based on Homogeneous Markov Process
title_short Analytical Study on the Reliability of Redundancy Architecture for Flight Control Computer Based on Homogeneous Markov Process
title_full Analytical Study on the Reliability of Redundancy Architecture for Flight Control Computer Based on Homogeneous Markov Process
title_fullStr Analytical Study on the Reliability of Redundancy Architecture for Flight Control Computer Based on Homogeneous Markov Process
title_full_unstemmed Analytical Study on the Reliability of Redundancy Architecture for Flight Control Computer Based on Homogeneous Markov Process
title_sort analytical study on the reliability of redundancy architecture for flight control computer based on homogeneous markov process
publisher IEEE
series IEEE Access
issn 2169-3536
publishDate 2018-01-01
description In order to analyze the reliability of redundancy architecture for flight control computer, this paper gives the analytical study on the reliability based on the Homogeneous Markov Process in “Triplex Channels & Single Module”and “Double Channels & Double Modules.”The paper analyzes the effect of fault rate and fault coverage rate on system reliabilities and MTTFs (mean time to failures). The index of fault tolerant capability is proposed. The analyzing results show that, for different redundancy architectures, the fault coverage rate or the branch fault rate have different effects on the reliability. Especially, the influence of the branch fault rate is more significant. In addition, the fault tolerant capability of the redundant system to multiple faults is determined by the system architecture scheme and the fault coverage rate. The results show that the method proposed in this paper can analyze reliability of redundancy architecture effectively.
topic Flight control computer
redundancy architecture
Markov
reliability
fault tolerant capability
fault rate
url https://ieeexplore.ieee.org/document/8307055/
work_keys_str_mv AT yaomingzhou analyticalstudyonthereliabilityofredundancyarchitectureforflightcontrolcomputerbasedonhomogeneousmarkovprocess
AT chenghaolin analyticalstudyonthereliabilityofredundancyarchitectureforflightcontrolcomputerbasedonhomogeneousmarkovprocess
AT yaolongliu analyticalstudyonthereliabilityofredundancyarchitectureforflightcontrolcomputerbasedonhomogeneousmarkovprocess
AT hongzhexu analyticalstudyonthereliabilityofredundancyarchitectureforflightcontrolcomputerbasedonhomogeneousmarkovprocess
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