DDC’s AFDX®/ARINC Part 7 Switch provides the key element of an AFDX network—the physical infrastructure to interconnect end systems and regulate. The AFDXEnd System Pro is certifiable to civil aerospace standards and enables safety-critical data transfer between a computer and an AFDX switch. 10// Mbit/s 24+1 port AFDX® switch for rapid system development of all technical functionalities of TTTech’s certifiable AFDX production switches.
|Published (Last):||12 September 2006|
|PDF File Size:||16.71 Mb|
|ePub File Size:||17.89 Mb|
|Price:||Free* [*Free Regsitration Required]|
Archived copy as title All Wikipedia articles needing clarification Wikipedia articles needing clarification from September To get access to the document please fill in the following form.
Therefore, in a network with multiple switches cascaded star topologythe total number of virtual links is nearly limitless. This is the maximum rate data can be sent, and it is guaranteed to be sent at that interval.
Each virtual link is allocated dedicated bandwidth [sum of all VL bandwidth allocation gap BAG rates x MTU] with the total amount of bandwidth defined by the system integrator. This ADN operates without the use of a bus controller thereby increasing the reliability of the network architecture.
The virtual link ID is a bit unsigned integer value that follows a constant bit field. There is no specified limit to the number of virtual links that can be handled by each end system, although this will be determined by the BAG rates and maximum frame size specified for each VL versus the Ethernet data rate.
However, some features of a real AFDX switch may be missing, such as traffic policing and redundancy functions.
The switch must also be non-blocking at the data rates that are specified by the system integrator, and in practice this may mean that the switch shall have a switching capacity that is the sum of all of its physical ports. This type of network can significantly reduce wire runs and, thus, the overall weight of the aircraft.
There can be one or more receiving end systems connected within each virtual link. Also sub-virtual links do not provide guaranteed bandwidth or latency due to the buffering, swutch AFDX specifies that latency is measured from the traffic regulator function anyway.
Each VL is frozen switdh specification to ensure that the network has a designed maximum traffic, hence determinism. The drawback is that it requires custom hardware which can add significant cost to the aircraft. Avionics Full-Duplex Switched Ethernet AFDX is a data network, patented by international aircraft manufacturer Airbus for safety-critical applications that utilizes dedicated bandwidth while providing deterministic quality of service QoS.
AgustaWestland asserts its independence in the cockpit”. Archived from the original PDF on However, total bandwidth cannot exceed the maximum available bandwidth on the network.
Retrieved from ” https: Virtual links are unidirectional logic paths from the source end-system to all of the destination end-systems. Many commercial aircraft use the ARINC switcj developed in for safety-critical applications. This product provides the full range of technical functionalities of our certifiable production switches making it the optimal solution for various applications.
Additionally, there can be sub-virtual links sub-VLs that are designed to carry less critical data. Airbus and Rockwell Collins: AFDX is a worldwide registered trademark by Airbus. Ethernet family of local area network technologies. ARINC utilizes a unidirectional bus with a single transmitter and up to twenty receivers. This page was last edited on 10 Novemberat AFDX extends standard Ethernet to provide high data integrity and deterministic timing.
AFDX® / ARINC 664 Part 7 Switch for Flight Test
The architecture adopted by AgustaWestland is centered around the AFDX data network developed for the latest commercial airliners. Basing on standards from the IEEE AFDX was designed as the next-generation aircraft data network. AFDX was developed by Airbus Industries for the A,  initially to address real-time issues for flight-by-wire system development. Webarchive template wayback links CS1 maint: In addition, AFDX can provide quality of service and dual link redundancy.
Innovating together for the A XWB”. In one abstraction, it is possible to visualise the VLs as an ARINC style network each with one source and one or more destinations. This high-performance port switch is certifiable to civil aerospace standards and supports bandwidth-regulated traffic filtering and policing.
DDW: AFDX® / ARINC Part 7 Switch for Flight Test
Further a redundant pair of networks is used to improve the system integrity although a virtual link may be configured to use one or the other network only. Also the switch, having a VL configuration switcu loaded, can reject any erroneous data transmission that may otherwise swamp other branches of the network. The switches are designed to route an incoming frame from one, and only one, end system to a predetermined set of end systems.
A similar implementation [ clarify ] of deterministic Ethernet is used on the Boeing Dreamliner. AFDX Switch Lab This product provides the full range of technical functionalities of our certifiable production switches making it swihch optimal solution for various applications.
A data word consists of 32 bits communicated over a twisted pair cable using the bipolar return-to-zero modulation.