DocumentCode
2901280
Title
Research on Distributed Integrated Modular Avionics system architecture design and implementation
Author
Guoqing Wang ; Qingfan Gu
Author_Institution
China Nat. Aeronaut. Radio Electron. Res. Inst., Shanghai, China
fYear
2013
fDate
5-10 Oct. 2013
Abstract
A well-designed Distributed Integrated Modular Avionics (DIMA) should keep the complexity of system interconnections to a minimum with the constraints set by communication links, LRM size, and fault tolerance requirements. In this paper, a basic DIMA model is put forward and the design philosophy is detailed for constructing DIMA system framework which enhanced capabilities with improved reliability and lower cost. The paper analyzes the system framework model, ability and effectiveness, discusses the organization mode, management mode and process scheduling management mode of DIAM system, and created an organization and management mode for DIMA system architecture. Furthermore, the key enable technologies for DIMA system implementation are analyzed which can guide implementing DIMA system.
Keywords
avionics; fault tolerance; reliability; DIMA system architecture; DIMA system framework model; LRM size; communication links; distributed integrated modular avionics system architecture design; fault tolerance; management mode; organization mode; process scheduling management mode; reliability; Aerospace electronics; Aircraft; Complexity theory; Computer architecture; Organizations; Organizing; Resource management;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference (DASC), 2013 IEEE/AIAA 32nd
Conference_Location
East Syracuse, NY
ISSN
2155-7195
Print_ISBN
978-1-4799-1536-1
Type
conf
DOI
10.1109/DASC.2013.6712647
Filename
6712647
Link To Document