-
摘要:
为解决综合模块化航空电子系统(IMA)动态重构机制导致其可靠性难以建模和评估的问题,分析了IMA的组成结构及资源备份和资源抢占2种动态重构机制。根据分析结果,在现有总线性能共享多状态系统模型的基础上,考虑动态重构机制下的计算资源再分配问题,建立适用于动态重构机制下IMA的可靠性模型。同时,提出一种基于通用生成函数(UGF)的动态重构机制下IMA可靠性评估算法,对不同动态重构机制下系统可靠度进行量化评估。以某型直升机IMA中综合任务处理系统为对象进行案例应用研究,分析其备用通用处理单元数量变化对系统可靠度的影响规律,并提出最优化设计方案,以验证所提可靠性建模和评估方法的可行性。
-
关键词:
- 直升机综合模块化航空电子系统 /
- 动态重构 /
- 多状态系统 /
- 通用生成函数 /
- 可靠性
Abstract:This study starts by examining the interconnection topology of integrated modular avionics (IMA) and two dynamic reconfiguration mechanisms: resource backup and resource preemption, in order to address the challenge of modeling and evaluating the dependability of IMA under dynamic reconfiguration. Subsequently, based on the operational principles of IMA and dynamic reconfiguration mechanisms, this paper extends a multi-state system with common bus performance sharing while considering the performance allocation problem for IMA under dynamic reconfiguration. Simultaneously, an algorithm about IMA reliability assessment under dynamic reconfiguration mechanisms based on the universal generating function (UGF) is proposed to quantitatively evaluate the reliability of IMA under different dynamic reconfiguration mechanisms. In order to confirm the viability of the suggested extended model and reliability assessment method, a case study is finally carried out on the IMA in the helicopter, examining the effects of variations in the number of standby processing units on the system’s dependability and suggesting an ideal design solution.
-
表 1 通用处理单元能力和任务需求的参数
Table 1. Parameters of the performance and the demand of general processing units
通用处理
单元型号数据处理与
运算能力发生
概率任务
需求发生
概率价格/
元Ⅰ 4 0.9 2 0.4 0.4 0 0.1 1 0.6 Ⅱ 2 0.9 2 0.4 0.2 0 0.1 0 0.6 表 2 总线传输能力的参数
Table 2. Parameters of performance of common bus
传输能力 发生概率 2 0.8 1 0.1 0 0.1 -
[1] BIRBER P, BONIOL F, BOYER M, et al. New challenges for future avionic architectures[J]. New Aerospace Lab, 2012(4): 1-10. [2] GASKA T, WATKIN C, CHEN Y. Integrated modular avionics-past, present, and future[J]. IEEE Aerospace and Electronic Systems Magazine, 2015, 30(9): 12-23. [3] 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: 测控技术编辑部, 2016: 201-203.ZHAN Z J, ZHOU Q, HONG R. Research on dynamic reconfiguration management method for distributed integrated modular avionics[C]//Proceedings of the 2016 Academic Conference on Aviation Test and Measurement Technology. Beijing: Measurement & Control Technology Editorial office, 2016: 201-203. [4] 丁明. 综合模块化航空电子系统重构与验证方法研究[D]. 西安: 西北大学, 2019: 1-5.DING M. Research on reconfiguration and verification methods for integrated modular avionics[D]. Xi’an: Northwestern University, 2019: 1-5(in Chinese). [5] 张安莉. 基于随机Petri网的航空电子综合化系统可靠性建模与分析[D]. 西安: 西北工业大学, 2006: 1-5.ZHANG A L. Reliability modeling and analysis of integrated avionics systems based on stochastic Petri nets [D]. Xi’an: Northwestern Polytechnical University, 2006: 1–5(in Chinese). [6] WANG R P, LU W T, ZENG C H, et al. Reliability modeling and verification method for dynamic reconfiguration system[C]//Proceedings of the 2018 Prognostics and System Health Management Conference. Piscataway: IEEE Press, 2019: 941-947. [7] JIANG Z Y, ZHAO T D, WANG S H, et al. New model-based analysis method with multiple constraints for integrated modular avionics dynamic reconfiguration process[J]. Processes, 2020, 8(5): 574. [8] JU H Y, WANG S H, ZHAO T D. A modeling method of IMA dynamic reconfiguration based on AADL[C]//Proceedings of the 2015 First International Conference on Reliability Systems Engineering. Piscataway: IEEE Press, 2016: 1-5. [9] 李伯宁. 综合模块化航电系统分区资源分配方法研究[D]. 天津: 中国民航大学, 2022: 8-11.LI B N. Research on partition resource allocation method of integrated modular avionics system [D]. Tianjin: Civil Aviation University of China, 2022: 8-11(in Chinese). [10] LISNIANSKI A, DING Y. Redundancy analysis for repairable multi-state system by using combined stochastic processes methods and universal generating function technique[J]. Reliability Engineering & System Safety, 2009, 94(11): 1788-1795. [11] LEVITIN G. Reliability of multi-state systems with common bus performance sharing[J]. IIE Transactions, 2011, 43(7): 518-524. [12] CHENG C, YANG J, LI L. Reliability assessment of multi-state phased mission systems with common bus performance sharing considering transmission loss and performance storage[J]. Reliability Engineering & System Safety, 2020, 199: 106917. [13] ZHAO X, WU C S, WANG S Q, et al. Reliability analysis of multi-state k-out-of-n: G system with common bus performance sharing[J]. Computers & Industrial Engineering, 2018, 124: 359-369. [14] WU D, CHI Y Y, PENG R, et al. Reliability of capacitated systems with performance sharing mechanism[J]. Reliability Engineering & System Safety, 2019, 189: 335-344. [15] SU P, WANG G J, DUAN F J. Reliability evaluation of a k-out-of-n(G)-subsystem based multi-state system with common bus performance sharing[J]. Reliability Engineering & System Safety, 2020, 198: 106884. [16] ZHAI Q Q, YE Z S, PENG R, et al. Defense and attack of performance-sharing common bus systems[J]. European Journal of Operational Research, 2017, 256(3): 962-975. [17] QIU S, MING H X G. Reliability analysis of multi-state series systems with performance sharing mechanism under epistemic uncertainty[J]. Quality and Reliability Engineering International, 2019, 35(6): 1998-2015. [18] YU H, YANG J, MO H D. Reliability analysis of repairable multi-state system with common bus performance sharing[J]. Reliability Engineering & System Safety, 2014, 132: 90-96. [19] XIAO H, PENG R. Optimal allocation and maintenance of multi-state elements in series-parallel systems with common bus performance sharing[J]. Computers & Industrial Engineering, 2014, 72: 143-151. [20] AERONAUTICAL RADIO, INC. ARINC specification 653: avionics application software standard interface, part Ⅰ−required services [S]. 2015. [21] ASAAC. Final draft of proposed guidelines for system issues-volume 1-2: system configuration/reconfiguration: ASAAC-STANAG 4626(Part VI)[S]. Belgium Brussels: North Atlantic Treaty Organization, 2004. [22] 阎芳, 邢培培, 赵长啸, 等. 基于联合k/n(G)模型的DIMA系统可靠性建模与分析[J]. 航空学报, 2018, 39(6): 185-193.YAN F, XING P P, ZHAO C X, et al. Reliability modeling and analysis of DIMA system based on joint k/n(G) model[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(6): 185-193(in Chinese). [23] 王鹏, 刘嘉琛, 董磊, 等. 面向任务的民机DIMA动态重构策略[J]. 系统工程与电子技术, 2021, 43(6): 1618-1627.WANG P, LIU J C, DONG L, et al. Task oriented DIMA dynamic reconfiguration strategy for civil aircraft[J]. Systems Engineering and Electronics, 2021, 43(6): 1618-1627(in Chinese). [24] LEVITIN G. The universal generating function in reliability analysis and optimization[M]. London: Springer-Verlag, 2005. -


下载: