This paper begins by reviewing the essential features of data bus concepts and continues by describing the key features of the most commonly used data buses on aircraft today. The following data buses are covered: ARINC 429; ARINC 629; MIL-STD-1553B; MIL-STD-1773; and STANAG 3910. The paper is intended to refresh and update those engineers not dealing with data buses, or the associated technology on a day-to-day basis.
ARINC specification 429-14. Mark 33 digital information transfer system (DITS). 1 July 1990.
2.
MIL-STD-1553B notice 3. Digital time division command/response multiplex data bus. 31 January 1993.
3.
ARINC specification 629. Multi-transmitter data bus, Part 1—technical description. 7 March 1990.
4.
MIL-STD-1773 notice 1. Fibre optics mechanization of an aircraft internal time division command/response multiplex data bus. 2 October 1989.
5.
EFJ-PDR-EFA-403-00003 issue A. Fibre optic digital time division command/response multiplex data bus STANAG 3910 (EFA). October 1987.
6.
SpitzerC. R.Digital avionics systems: principles and practices.
7.
MIL-HDBK-1553A notice 1. Multiplex application handbook. 31 January 1993.
8.
PitotC.VauboisC. C.ProstM.PotL. ARINC 429 data concentrator. EURO ASIC '90, pp. 68–72, IEEE Comp. Soc.
9.
StoneF. W.1553 overview. IEE Colloquium on Buses for instruments: VXI and beyond, Digest No. 63, pp. 8/1–7, IEE.
10.
HallW. H.MIL-STD-1553B systems issues. MIL-STD-1553B and the next generation, ERA 89-0591, pp. 1. 3/1–6 (ERA Technology).
11.
ParkerD. A.MIL-STD-1553 usage background and current definition. IICIT Symposium '91, pp. 505–9.
12.
AirnesA. M.WoodsS. A.The EAP data buses—an overview of the implementation. MIL-STD-1553B: applications, developments and components, ERA report 86-0237, pp. 1. 2–13 (ERA Technology).
13.
ChownD. P. M.LeeJ. S. F.PressR. W.A high performance fibre optic MIL-STD-1553B data bus. MIL-STD-1553B: applications, developments and components, ERA report 86-0237, pp. 6. 1–13 (ERA Technology).
14.
MooreJ. F.ARINC 629. The civil aircraft databus for the 1990s. IEE Colloquium on Time critical communications for instrumentation and control, Digest No. 122, pp. 5/1–2, IEE.
15.
DoddsG. M.AtkinsD. J.EMC implications of using unshielded twisted pair data buses in the aircraft environment. Seventh International Conference on Electromagnetic compatibility, conference publication no. 326, pp. 184–93, IEE.
16.
HillM.Commercial aircraft and fibre optics—are they compatible? Proceedings of the Conference on Advances in systems engineering for civil and military avionics, ERA 91-0634, pp. 4. 2/1–8 (ERA Technology).
17.
HallW. H.Introduction to STANAG 3910. MIL-STD-1553B and the next generation, ERA 89-0591, pp. 3. 3/1–7 (ERA Technology).
18.
MayouxJ.-J.The data bus of the next generation European fighters. Proceedings of the IEEE 1993 National Conference on Aerospace and electronics, NAECON 1993, Vol. 1, pp. 152–6, IEEE.
19.
BogenbergerR.Performance aspects and design considerations for STANAG 3910 and succeeding bus systems. MIL-STD-1553B and the next generation, ERA 89-0591, pp. 6. 13/1–17 (ERA Technology).
20.
WindettJ. D.Application of STANAG 3910 to the European Fighter Aircraft. Proceedings of Conference on Real-time data communications for military applications, ERA 90-0301, pp. 6. 1/1–8 (ERA Technology).
21.
UhlhornR. W.Fiber optic buses and networks for advanced avionics architectures. Computing systems configuration forum for highly integrated guidance and control systems, AGARD-LS-158, pp. 7/1–15, AGARD.
22.
BerggrenC.Communications for real-time distributed systems. Proceedings of Conference on Advances in systems engineering for civil and military avionics, ERA 91-0634, pp. 4. 3/1–8 (ERA Technology).
23.
LewisN. E.Fiber optic data buses for aircraft. Fiber and Integrated Optics, 11(4), 337–52.
24.
BicknellJ.The high speed data bus (for military applications). Proceedings of Seminar on Military avionics architectures for today and tomorrow, ERA 88-0437, pp. 4***-1/1–13 (ERA Technology).