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XMC-A825-16 ARINC-825 16 Channel XMC / CANFlight-16 User's Manual REV C
Document: TP2216-901_Users_Manual.pdf
Page 5 of 39
© Innovative Control Systems
Project:
TP2216-901
Author: K. Jacobson Date: 11.05.2019
Rev.: C
1 Introduction
The XMC-A825-16 interface system offers 16 electrically isolated CAN 2.0B interfaces according to ISO
11898, an IRIG-B time code input and a 10/100/1000 BaseT Ethernet interface. To minimize CPU load on host
computers, the XMC-A825-16 uses an onboard Xilinx Artix 7 FPGA with Five 128 MHz Microblaze processors
and 24 MByte SRAM to process and store CAN messages. The CAN bus interfaces are accessible via a VHD-
68 front panel connector as well as two 40-pin rectangular on-board connectors behind the VHD-68 connector.
Figure 1-1 XMC-A825-16 Hardware
The XMC-A825-16 features are:
•
Laptop-ready, 5 Processor Based Embedded Realtime Control System for Ground and Airborne Use
•
Sixteen (16) isolated, fully independent Controller Area Network (ISO 11898), ARINC825 and
CANaerospace protocol compliant interfaces
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Integrated µSDHC card-based Flight Data Recording Option available
•
IRIG-B Time Code Input for High Precision Data Synchronization
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Auto-negotiating 10/100/1000 BaseT Ethernet interface with CANaerospace over Ethernet (CoE) and
ARINC825 over Ethernet (A825oE) protocol and Application Programmer Interface (API)
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IEEE 802.11 Wireless LAN Option with CANaerospace over Wireless (CoW) and ARINC825 over Wireless
(A825oW) protocol available
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Frontpanel Activity LEDs for CAN and Ethernet
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Power Supply 5V through XMC interface or through ICS Stand Alone Aircraft power supply. Aircraft Power
(9-36VDC)
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Mechanical Dimensions 149mm L x 74mm W x 47mm H
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CAN/ARINC825/CANaerospace toolbox for Linux, MacOS and Windows
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Custom Software and FPGA firmware Options available on request