Low Cost AFDX End System Based on System on a Programmable Chip

Bing Yu; Tian Hong Zhang; Dong Dong Liu

doi:10.4028/www.scientific.net/AMM.29-32.2308

Paper Titles

Research on Design and Testing of a Novel Power Source for Hybrid Vehicles
p.2285

Laboratory Tests Study on the Power Dissipation Characteristics of Conductor Self-Damping and Aeolian Vibration Dampers
p.2290

Research on the Design of Motion Control System Based on a Novel 5-DOF PCMM
p.2296

MEMS Aided Design Method Based on 3D Features
p.2302

Low Cost AFDX End System Based on System on a Programmable Chip
p.2308

Software Design and Implement of Test System of a Certain Radar Transmitter Based on the 1553B Bus
p.2312

Manufacture Parameter Design of SMG Spiral Bevel Gears Based on Local Synthesis and Transmission Error Optimization
p.2319

Study of Magnetoelastic Torque Sensor for Cutting Processes Monitoring
p.2327

Research of H.264/AVC Error Control Approaches Base on FMO
p.2333

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 29-32Low Cost AFDX End System Based on System on a...

Low Cost AFDX End System Based on System on a Programmable Chip

Abstract:

AFDX (Avionics Full DupleX Switched Ethernet, ARINC 664) utilized in Airbus A380 and Boeing 787 represents a major upgrade in both bandwidth and capability; however some legacy systems are difficult to connect into the AFDX bus smoothly. A low cost AFDX end system based on SOPC (System On a Programmable Chip) is presented. A Xilinx Spartan 3AN FPGA is employed to build the whole system; and then a dedicated reduced Ethernet MAC controller for AFDX end system is designed; a MC8051 open core microcontroller is employed as the system controller and protocol processing unit. The whole design costs small FPGA resources and the experiments show that the designed AFDX end system works robustly and correctly.

You might also be interested in these eBooks

Applied Mechanics And Mechanical Engineering

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volumes 29-32)

Pages:

2308-2311

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.29-32.2308

Citation:

Cite this paper

Online since:

August 2010

Authors:

Bing Yu, Tian Hong Zhang, Dong Dong Liu

Keywords:

AFDX End System, Open Core Processor, Reduced Media Access Controller, System on Programmable Chip (SOPC)

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] ARINC 429, Aeronautical Radio Inc. ARI�C specification 429. Digital Information Transfer System (DITS) parts1, 2, 3., (2001).

Google Scholar

[2] ARINC 629 Communication System Description Document, D227W003, Rev. B, September 9, (1994).

Google Scholar

[3] ARINC Specification 664: Aircraft Data Network, Parts 1, 2, 7. Technical report, Aeronotical Radio Inc., (2005).

Google Scholar

[4] Jean-Luc Scharbarg: A Probabilistic Analysis of End-To-End Delays on an AFDX Avionic Network, IEEE TRANSACTIONS ON INDUSTRIAL INFORMATICS, Vol. 5 (2009), pp.38-49.

DOI: 10.1109/tii.2009.2016085

Google Scholar

[5] John McHale: AFDX technology to improve communications on Boeing 787, Military & Aerospace Electronics April, (2005).

Google Scholar

[6] Information on http: /www. xilinx. com/support/documentation/spartan-3an. htm.

Google Scholar

[7] Information on http: /www. opencores. org/project, 8051.

Google Scholar

[8] ARINC 653, Aeronautical Radio Inc. ARINC specification 653. Avionics application Software Standard Interface. (1997).

DOI: 10.1201/9781315222240-22

Google Scholar