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http://dx.doi.org/10.5392/JKCA.2012.12.08.077

HM System Design for Fault Tolerance on the IMA System  

Ko, Young-Kwan (충남대학교 컴퓨터공학과)
Lee, Seung-Hoon (충남대학교 컴퓨터공학과)
Park, Se-Young (충남대학교 컴퓨터공학과)
Ban, Chang-Bong (LIG 넥스원)
Kang, Dai-Il (LIG 넥스원)
Jeong, Jae-Yeop (LIG 넥스원)
Lee, Cheol-Hoon (충남대학교 컴퓨터공학과)
Publication Information
The Journal of the Korea Contents Association / v.12, no.8, 2012 , pp. 77-86 More about this Journal
Abstract
Avionics system are composed of multiple electronic device that performs important missions the number of electronic devices for the performance of aircraft has been gradually increasing. As a result, cost of development, maintenance and operating have increased. To solve this problem, technology paradigm of avionics has been shifting from federated avionics systems that manage to each system independently to IMA(Integrated Modular Avionics) systems. Unlike federated systems, fault tolerance becomes an essential technology in IMA systems. Because each aircraft features integrated in the an IMA system, a fault can jeopardize the entire system. In this paper, we define faults which can occur on the ARINC 653 based IMA system first, and design the ARINC 653 compliant HM(health Monitoring) system for the system can continue to operate be normal when occur a fault.
Keywords
Integrated Modular Avionics System; Fault Tolerance; Health Monitoring System;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
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