DocumentCode
2535389
Title
Avionics hard real-time systems´ concerning fault tolerance
Author
Loubach, D.S. ; Da Cunha, Adilson Marques
Author_Institution
Electron. & Comput. Eng. Dept., Brazilian Aeronaut. Inst. of Technol., Sao Paulo, Brazil
fYear
2012
fDate
14-18 Oct. 2012
Abstract
It is unrealistic to assume that a computer system will never fail. Yet, there is no fault-free system. Nevertheless, even in the presence of possible faults, the system should continue operating as normal as possible and it is not expected to crash. That assertion is especially true for hard real-time systems on which human lives may depend on. Considering this scenario, this paper introduces a computational and conceptual model addressing the fault resilience improvement in a class of hard real-time system named avionics systems. Essentially, the proposed computational and conceptual model consists of a fundamental schedulability analysis and three other different algorithms. This paper shows the improvement of fault resilience, on up to 80%, by composing and applying space and time redundancy (i.e., multiprocessors and scheduling) with task migration among processors in hard real-time systems´ design.
Keywords
avionics; fault tolerance; multiprocessing systems; processor scheduling; real-time systems; computational model; computer system; conceptual model; fault resilience improvement; fault tolerance; fault-free system; fundamental schedulability analysis; hard real-time avionic system; multiprocessor; scheduling; space-time redundancy; Aerospace electronics; Fault tolerant systems; Processor scheduling; Program processors; Real-time systems; Redundancy;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference (DASC), 2012 IEEE/AIAA 31st
Conference_Location
Williamsburg, VA
ISSN
2155-7195
Print_ISBN
978-1-4673-1699-6
Type
conf
DOI
10.1109/DASC.2012.6382379
Filename
6382379
Link To Document