Considering the dynamic reconfiguration of the Distributed Integrated Modular Avionics (DIMA) system, the dynamic reconfiguration strategy and reconfiguration process are analyzed, and a joint k/n (G) reliability model for the DIMA system is constructed. An experimental analysis of the comprehensive display function residing in the DIMA system is carried out. The relationship between reliability and time of the system reconfiguration process is discussed, and the change of reliability curve is given using the general k/n (G) reliability model. Comparative analysis is conducted to show the applicability and rationality of the joint k/n (G) model. Through the parameter sensitivity analysis, the impact of different model configuration parameters on the system reliability is observed. The results can provide effective guidance for improving the reliability of the dynamic reconfiguration process of the DIMA system and optimizing resource allocation.
YAN Fang
,
XING Peipei
,
ZHAO Changxiao
,
WANG Peng
. Reliability modeling and analysis of DIMA system based on joint k/n(G) model[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018
, 39(6)
: 321971
-321971
.
DOI: 10.7527/S1000-6893.2018.21971
[1] MOIR L, ALLAN S. 飞机航空电子系统[M]. 支超有, 秦成, 译. 北京:国防工业出版社, 2015:136-144. MOIR L, ALLAN S. Civil avionics systems[M]. ZHI C Y, QIN C, translated. Beijing:National Defence Industry Press, 2015:136-144(in Chinese).
[2] 王国庆, 谷青范, 王淼,等. 新一代综合化航空电子系统构架技术研究[J]. 航空学报, 2014, 35(6):1473-1486. WANG G Q, GU Q F, WANG M, et al. Research on the architecture technology for new generation integrated avionics system[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(6):1473-1486(in Chinese).
[3] ROBATI T, GHERBI A, MULLINS J. A modeling and verification approach to the design of distributed IMA architectures using TTEthernet[J]. Procedia Computer Science, 2016, 83:229-236.
[4] FUCHSEN R. IMA NextGen:A new technology for the Scarlett program[J]. IEEE Aerospace & Electronic Systems Magazine, 2010, 25(10):10-16.
[5] 王鹏, 阎芳, 白杰,等. 一种综合模块化航电系统重构决策系统及决策方法:CN 103825902A[P]. 2014-05-28. WANG P, YAN F, BAI J, et al. An IMA reconstruction decision system and decision method:CN 103825902A[P]. 2014-05-28(in Chinese).
[6] EFKEMANN C, PELESKA J. Model-based testing for the second generation of integrated modular avionics[C]//IEEE Fourth International Conference on Software Testing, Verification and Validation Workshops. Washington, D.C:IEEE Computer Society, 2011:55-62.
[7] ANNIGHÖFER B, THIELECKE F. A systems architecting framework for optimal distributed integrated modular avionics architectures[J]. Ceas Aeronautical Journal, 2015, 6(3):485-496.
[8] JU H Y, WANG S H. Reliability analysis for the process of DIMA dynamic reconfiguration[C]//Proceedings of the 26th European Safety and Reliability Conference. London:CRC Press, 2016:679-684.
[9] 王鹏, 刘锐, 刘万和,等. 综合模块化航空电子系统可靠性评估方法研究[J]. 电光与控制, 2015(10):56-61. WANG P, LIU R, LIU W H, et al. On reliability assessment method of integrated modular avionics system[J]. Electronics Optics & Control, 2015(10):56-61(in Chinese).
[10] ROBATI T, GHERBI A, KOUHENA E, et al. Design and simulation of distributed IMA architectures using TTEthernet:A model-driven approach[J]. Journal of Ambient Intelligence & Humanized Computing, 2017, 8(3):1-11.
[11] WANG G Q, GU Q F. Research on distributed integrated modular avionics system architecture design and implementation[C]//Digital Avionics Systems Conference. Piscataway, NJ:IEEE Press, 2014:7D6-1-7D6-10.
[12] WOLFIG R. 综合化模块化航空电子系统的分布式平台[M]. 牛文生, 译. 北京:航空工业出版社, 2015:29-31. WOLFIG R. A distributed platform for integrated modular avionics[M]. NIU W S, translated. Beijing:Aviation Industry Press, 2015:29-31(in Chinese).
[13] 崔西宁, 沈玉龙, 李亚晖. 综合化航空电子系统安全技术研究进展[J]. 计算机应用与软件, 2012(11):130-136. CUI X N, SHEN Y L, LI Y H. Process in research of security technologies in integrated avionics system[J]. Computer Applications and Software, 2012(11):130-136(in Chinese).
[14] 熊华钢, 王中华. 先进航空电子综合技术[M]. 北京:国防工业出版社, 2009:266-269. XIONG H G, WANG Z H. Advanced integrated avionics technology[M]. Beijing:National Defence Industry Press, 2009:266-269(in Chinese).
[15] BIEBER P, NOULARD E, PAGETTI C, et al. Preliminary design of future reconfigurable IMA platforms[J]. ACM Sigbed Review, 2009, 6(3):1-5.
[16] 詹志娟, 周庆, 洪蓉. DIMA动态重构管理方法研究[C]//2016航空试验测试技术学术交流会论文集. 北京:测控技术杂志社, 2016:190-192. ZHAN Z J, ZHOU Q, HONG R. Research on the method of the dynamic reconfiguration management in DIMA[C]//Proceedings of Aeronautical Test and Measurement Technology Symposium in 2016. Beijing:Measurement & Control Technology Press, 2016:190-192(in Chinese).
[17] ASAAC. Final draft of proposed guidelines for system issues-Volume4:System configuration/reconfiguration:ASAAC-STANAG 4626(Part VI)[S]. Belgium Brussels:North Atlantic Treaty Organization, 2004.
[18] ASAAC. Ministry of defence interim defence standard 00-76 ASAAC standards part 1:Proposed standards for common functional modules[S]. Belgium Brussels:North Atlantic Treaty Organization, 2005.
[19] LI R C, MIN X. On a generalized k-out-of-n system and its reliability[J]. International Journal of Systems Science, 2005, 36(5):267-274.
[20] COIT D W, CHATWATTANASIRI N, WATTANAPONGSAKORN N, et al. Dynamic k-out-of-n system reliability with component partnership[J]. Reliability Engineering & System Safety, 2015, 138:82-92.
[21] COIT D W, CHATWATTANASIRI N, WATSOOKTIP T, WATTANAPONGSAKORN N. System reliability optimization with k-out-of-n subsystems and changing k[C]//International Conference on Reliability, Maintainability and Safety. Piscataway, NJ:IEEE Press, 2011:1382-1387.
[22] 宋成艳, 杨永华, 杨明. 基于APEX的飞机综合信息显示系统[C]//首届中国航空科学技术大会. 北京:中国航空学会,2013. SONG C Y, YANG Y H, YANG M. The integrated information display system of aircraft based on APEX[C]//First China Aviation Science and Technology Conference, Beijing:CSAA, 2013(in Chinese).
[23] 赵长啸, 何锋, 阎芳,等. 面向风险均衡的AFDX虚拟链路路径寻优算法[J]. 航空学报, 2018,39(1):321435. ZHAO C X, HE F, YAN F, et al. Path optimization algorithem of AFDX virtual link to balance the network risk[J]. Acta Aeronautica et Astronautica Sinica, 2018,39(1):321435(in Chinese).
[24] FAA. AC 25-11B, advisory circular:Transport category, airplane electronic Display System[S]. Washington, D. C.:Federal Aviation Authority, 2014.
[25] ASAAC. Final draft of proposed guidelines for system issues-Volume7:Safety:ASAAC-STANAG 4626(Part VI)[S]. Belgium Brussels:North Atlantic Treaty Organization, 2004.
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