Enhanced Performance Capability in a Dual Redundant Avionics Platform -Fault Tolerant Scheduling with Comparative Evaluation

被引:2
作者
Sreekumar, Archana [1 ]
Swetha, K. [1 ]
Swetha, Annam [1 ]
Pillay, Radhamani, V [1 ]
机构
[1] Amrita Vishwa Vidyapeetham, Coimbatore 641112, Tamil Nadu, India
来源
PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ON INFORMATION AND COMMUNICATION TECHNOLOGIES, ICICT 2014 | 2015年 / 46卷
关键词
Real time Scheduling; Fault Tolerance; Safety Critical System; Avionic Missile System;
D O I
10.1016/j.procs.2015.01.001
中图分类号
TP3 [计算技术、计算机技术];
学科分类号
0812 ;
摘要
For mission critical applications like Avionics, dependability is to avoid consequences of catastrophic results. Traditionally fault tolerance is implemented using hardware redundancy, the higher the redundancy, greater the cost and possibilities of more failures occurring. In this paper, an adaptive fault tolerant scheduling mechanism developed earlier with augmented performance capability and online fault recovery for a dual redundant system has been extended for an avionics mission system. An algorithm has been developed, simulated and evaluated on the practical case study vis -a- vis a traditional dual redundant system. This paper also roposes an extension of earlier scheme to schedule arrival of either/and critical and non -critical aperiodic tasks. The augmented scheme helps to achieve full functionality when no fault occurs, a fail safe mechanism for a single fault and performance metrics highlights the better computational performance. It elucidates that the use of this adaptive model leverages better in terms of enhanced performance and throughput compared to the existing dual redundant systems. (C) 2015 The Authors. Published by Elsevier B.V.
引用
收藏
页码:921 / 932
页数:12
相关论文
共 25 条
[1]  
Abraham Sherin, 2011, 2 INT C ADV COMP COM
[2]  
[Anonymous], 2002, P 24 INT C SOFTW ENG
[3]  
Avizienis A., 1967, FALL JOINT COMP C
[4]  
Butazo Giorgio.C, 1997, HARD REAL TIME COMPU
[5]  
Chandran S.K., 2010, INT C COMP EL ENG IC
[6]  
Davis R.I., 2010, ACM COMPUTING SURVEY
[7]  
Dodd R. B., 2006, TECHNICAL REPORT ANA
[8]  
Douglass C. Locke, 1990, TECHNICAL REPORT GEN
[9]  
Hitt Ellis F., 2001, FAULT TOLERANCE AVIO
[10]  
Krishna C. M., 1985, P FAULT TOL COMP S, P234