DocumentCode
2341833
Title
Design and application of new avionics control bus upon SPI
Author
Gao, Ke ; Mo, Bo
Author_Institution
Sch. of Aerosp. Eng., Beijing Inst. of Technol., Beijing, China
Volume
2
fYear
2011
fDate
22-23 Oct. 2011
Firstpage
203
Lastpage
205
Abstract
Traditional avionics control bus is neither portable nor scalable. The quantity of electronic devices in aircraft is expanding at an exponential rate. How to connect those devices together by a light, fast, scalable bus is a very urgent task. In this paper, we propose a new design and an application of new avionics control bus which combines the advantages of the SPI and FPGA IP-Core. Firstly, the overall structure of this new avionics control bus is put forward. Secondly, some key design points are discussed. Thirdly, the IP-Core examples are present. Finally, the experiment results show that this new avionics control bus is very suitable for aircraft systems which re-quire highly reliability, flexible configurations and compact size.
Keywords
avionics; field programmable gate arrays; FPGA IP-Core; SPI; aircraft systems; avionics control bus; electronic devices; Aerospace electronics; Computers; Avionics; Bus VHDL/Verilog; Control; FPGA; IP-Core; SPI;
fLanguage
English
Publisher
ieee
Conference_Titel
System Science, Engineering Design and Manufacturing Informatization (ICSEM), 2011 International Conference on
Conference_Location
Guiyang
Print_ISBN
978-1-4577-0247-1
Type
conf
DOI
10.1109/ICSSEM.2011.6081278
Filename
6081278
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