

On receiving E/S the ‘First valid Frames win’.Integrity Checking is done per VL and per Network Frames are transmitted concurrently on both Networks.The Ports, Links and Switches are duplicated for Redundancy.The E/S controls the Flow for each VL in accordance with the Bandwidth Allocation Gap (BAG).An E/S performs Traffic Policing, Integrity Checking and Redundancy Management on a VL Basis.A VL defines the unidirectional Connection from 1 Source E/S to 1 or more Destination E/S(s).End Systems (E/S) exchange Frames through Virtual Links (VL).AFDX® uses special Extensions to provide deterministic Timing and Redundancy.Redundancy is achieved by Duplication of the Connections (Wires) and the Switches.All Connections are full-duplex 10Mbits/s or 100MBit/s (no dedicated backbone Bus for.There are 2 Types of Devices on the Bus: Switches and End Systems.The main Elements of an AFDX® Network are:.AFDX® uses a special Protocol to provide Deterministic Timing and Redundancy Management.AFDX® is based on IEEE 802.3 Standard (commercial Ethernet using Wire) with either 10Mbits/s or 100Mbits/s.AFDX® is used on the Airbus A380 as main Avionics databus and on the A400M.> complete AIM AFDX® Product InformationĪRINC 664P7 standard adopts the key elements from AFDX® to standardize a deterministic network for aircraft.

> AFDX® Training – Workshop Presentation.> AFDX® Aircraft Testing – Technical Article.
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The first flight of the Airbus Industries A380 in Toulouse on Apis a real testimony for the program and a major milestone with the ‘first-to-fly’ with AFDX® on-board based on the commercial 100Mbit/s switched Ethernet (wire) with deterministic behavior.ĪIM GmbH is a leading manufacturer of AFDX®/ARINC 664P7 test, simulation, monitoring, recording and analysis modules, analyzer software and systems for any or all phases of an aircraft project deploying AFDX®/ARINC 664P7 data communications networks.ĪFDX® is a registered trademark of Airbus Deutschland GmbH. The main Elements of an AFDX® Network are:ĪFDX® data communications are used on the Airbus A380/A350/A400M, Boeing B787 Dreamliner (ARINC 664), ARJ21 and Super jet 100.ĪFDX®/ARINC 664P7 is being used as the backbone for all systems including flight controls, cockpit avionics, air-conditioning, power utilities, fuel systems, landing gear and others. End Systems (or LRU’s) based on Virtual Links (VL’s) communicate with Traffic Shaping by use of Bandwidth Allocation Gaps (BAGs).ĪFDX® Switches incorporate functions for filtering and policing, switching (based on configuration tables), end-system and network monitoring.
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AFDX® uses a special protocol to provide deterministic timing and redundancy management providing secure and reliable communications of critical and non-critical data.ĪFDX® communication protocols have been derived from commercial standards (IEEE802.3 Ethernet MAC addressing, Internet Protocol IP, User Datagram UDP) to achieve the required deterministic behavior for avionics applications.
