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ARINC659: BACKPLANE DATA BUS - SAE International
https://www.sae.org/standards/content/arinc659/
ARINC659. 1993-12-27. Latest. Defines standards for the transfer of digital data between components within an IMA cabinet. Includes the protocol and timing characteristics for a synchronous backplane data bus capable of transferring data at 60 Mbps using a data path that is two bits wide. The electrical characteristics and behav.
DA: 6 PA: 40 MOZ Rank: 29
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ARINC 659 - Backplane Data Bus | GlobalSpec - Engineering360
https://standards.globalspec.com/std/514584/arinc-659
Dec 27, 1993 · ARINC Specification 659 defines the protocol, timing, bit rate and power requirements for the physical backplane. It defines the physical medium, physical layer and parts of the Media Access Control (MAC) sublayer referred to in the OSI Reference Model. Document History. ARINC 659. December 27, 1993. Backplane Data Bus.
DA: 60 PA: 4 MOZ Rank: 93
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Architecture Design of Aviation Fault-tolerant Computer …
https://www.matec-conferences.org/articles/matecconf/pdf/2018/38/matecconf_2mae2018_03025.pdf
ARINC 659 is a kind of air bus with high data throughput, high fault tolerance and data certainty. The transmission rate is 60Mb/s and the coding efficiency is 98%. There is no need to transmit address information in transmission data, and 4 channel signals are used for error detection.
DA: 92 PA: 39 MOZ Rank: 46
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(PDF) Implementation of ARINC 659 Bus Controller for
https://www.researchgate.net/publication/332487103_Implementation_of_ARINC_659_Bus_Controller_for_Space-Borne_Computers
Apr 16, 2019 · As one of the key technologies of Honeywell, the aeronautical radio incorporated (ARINC) 659 bus is popular in current space-borne computers. However, Honeywell does not design ARINC 659 bus...
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Implementation of ARINC 659 Bus Controller for Space-Borne Computers …
https://www.mdpi.com/2079-9292/8/4/435
Apr 16, 2019 · This paper designs an ARINC 659 bus controller circuit, first to fill the gap in the design of the corresponding chip, second to improve the certainty and fault tolerance of space-borne computers by solving some key technologies, and third, to provide a novel architecture for ARINC 659 bus controller.
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BACKPLANE DATA BUS
https://img.antpedia.com/standard/files/pdfs_ora/20230613/ARINC/ARINC%20SPECIFICATION%20659-1993.pdf
Jun 13, 2023 · AERONAUTICAL RADIO, INC. 2551 Riva Road Annapolis, Maryland 21401-7465 USA. ARINC SPECIFICATION 659©. BACKPLANE DATA BUS. Published: December 27, 1993. Prepared by the Airlines Electronic Engineering Committee. Specification 659. Adopted by the Airlines Electronic Engineering Committee: October 20, 1993. Specification 659. Adopted by …
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A Radiation-hardened Bus Controller Chip for ARINC 659 | IEEE
https://ieeexplore.ieee.org/document/9205170/
Abstract: In this paper, a radiation-hardened bus controller chip for ARINC 659 is designed. To meet the needs of space radiation environment, most modules that may be affected by high-energy particles have been precisely hardened in terms of anti-SEU capability.
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[PDF] Implementation of ARINC 659 Bus Controller for Space …
https://www.semanticscholar.org/paper/Implementation-of-ARINC-659-Bus-Controller-for-Jiang-Liu/3c547bc2e09224c82528f37cfe4bd82a9293d804
Apr 16, 2019 · As one of the key technologies of Honeywell, the aeronautical radio incorporated (ARINC) 659 bus is popular in current space-borne computers. However, Honeywell does not design ARINC 659 bus controller separately, and there are only a few papers about FPGA-based ARINC 659 bus controllers.
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Implementation of ARINC 659 Bus Controller for Space …
https://mdpi-res.com/d_attachment/electronics/electronics-08-00435/article_deploy/electronics-08-00435.pdf
The ARINC 659 bus has many advantages, such as clear boundary between internal nodes, flexible bus architecture, convenient upgrading of hardware and software, 4-line cross check, double machine check, error silence tolerance, etc. It is easy to realize the robust partition in space and time and can realize the real-time switching of backup system.
DA: 51 PA: 64 MOZ Rank: 94
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SAFEbus | IEEE Conference Publication | IEEE Xplore
https://ieeexplore.ieee.org/document/282179/
It has been accepted as the draft for ARINC Project Paper 659. SAFEbus is designed to provide communications of all data among the line replaceable modules in the Boeing 777 Airplane Information Management System (AIMS) cabinets. The success of an integrated cabinet hinges on the backplane bus.
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