Design and architecture of a hardware platform to support the development of an avionic network prototype

The objective of the present project is to design three modules for a hardware platform that will support the implementation of an avionic network prototype based on the FPGA technology. The considered network has been conceived to reduce cabling weight and to improve the available bandwidth, and it exploits the recently introduced ARINC 825 and AFDX protocols. In order to support the implementation of both these protocols, a CAN bus controller, an AFDX End System, and an AFDX Switch have been designed. After an extensive review of the existing literature about the two related avionic protocols, a study of the existing solutions for CAN and Ethernet protocols, on which they are based, has been done as well to identify what knowledge and technology could be reused.;Because they are very similar, a flexible CAN controller has been implemented in hardware instead of an ARINC 825 one in order to support both these technologies and in order to reduce the IP core size. A combined HW/SW approach has been preferred for the AFDX End System architecture to leverage an existing UDP/IP protocol stack and the Ethernet layer included in the Linux kernel has been modified to create a portable and configurable implementation of AFDX. Since various problems have been encountered to reproduce an ARINC 653 compliant environment on the embedded system, the suggested design has been ported in a PC. Finally, an original solution for the implementation of the AFDX switch fabric has been finally presented; a space-division switching architecture has been chosen and tailored to meet the AFDX specification. Hardware parallelism is exploited to reduce the latency introduced on each frame by filtering them concurrently. Input buffers have been duplicated to separate high from low priority traffics, further reducing latency of critical frames and creating a redundancy that reduce the possibility of packet loss. Packet scheduling and double queuing guarantee that all critical frames are forwarded before low priority ones.;Keywords: Avionic Full-Duplex Switched Ethernet, AFDX, ARINC 664, ARINC 825, CAN, Avionic Data Networks, Ethernet Switch, FPGA.