Hostname: page-component-5cf477f64f-n7lw4 Total loading time: 0 Render date: 2025-04-08T04:48:27.376Z Has data issue: false hasContentIssue false
  • English
  • Français

The MIL-STD-1553B data bus: What does the future hold?

Published online by Cambridge University Press:  03 February 2016

D. R. Bracknell
D. R. Bracknell*
Affiliation:
Avionics consultant, Farnborough, UK
Get access Rights & Permissions [Opens in a new window]

Abstract

Numerous military platforms (land, sea and air) feature serial data bus technology based on the US MIL-STD-1553B data bus standard for integration of their digital systems. Many of these platforms have 15-20 years of operational life remaining, but the installed 1553B data buses (data networks) having only a 1Mbit/sec transfer rate are unable to meet many of the future data networking requirements. Research into new, higher performance data networks has concentrated on modern alternatives with throughput increases of two to three orders of magnitude (100Mbit/sec to 1Gbit/sec). These are generally based on modern commercial-off-the-shelf (COTS) standards, good examples being Ethernet and Fibre Channel. Some are already being employed in military platforms having been ruggedised for the harsh physical and electro-magnetic environment. However these COTS systems while being a natural choice for new platforms may not be cost effective for upgrading older platforms. This paper plots the history of MIL-STD-1553, possibly the most successful military platform standard of all time, and discusses some of the options for increasing its performance and economically extending its life into the future.

Type
Research Article
Information
The Aeronautical Journal , Volume 111 , Issue 1118 , April 2007 , pp. 231 - 246
Copyright
Copyright © Royal Aeronautical Society 2007 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Aircraft internal time division command/response multiplex data bus, 21 September 1978, US MIL-STD-1553B, US Department of Defense.Google Scholar
2. Aircraft internal time division command/response multiplex data bus, September 1990, UK MoD Def Stan 00-18, Part 2, Issue 2, UK MoD Directorate of Standardisation.Google Scholar
3. Aircraft internal time division command/response multiplex data bus, July 2003, NATO STANAG 3838, NATO Standardisation AgreementGoogle Scholar
4. Digital time division command/response multiplex data bus, 8 February 2006, US MIL-STD-001553B (USAF) w/CHANGE 5, US Department of Defense.Google Scholar
5. Comparison of SAE standard AS15531 with US MIL-STD-1553B plus Notice 2, ASSC/110/3/225, Avionics Systems Standardisation Committee (ASSC).Google Scholar
6. Use of installed AS15531 data bus networks at over-clocked bit rates, ASSC/110/3/231, Draft 3A, September 2000, Avionics Systems Standardisation Committee (ASSC).Google Scholar
7. Study of maximum signalling speed for electrical def stan 00-18, December 2005, Part 2/US MIL-STD-1553B data buses, ASSC/13/009, Draft Issue 1, Avionics Systems Standardisation CommitteeGoogle Scholar
8. NATO STANAG 3910 AVS, 8 November 2002, Edition 1, NATO Standardisation Agreement.Google Scholar
9. USAF Pre-solicitation notice number 01553DB, December 2004, USAF contracting office, ASC/LPKC, Wright Patterson AFB.Google Scholar
10. Hegarty, M.G., High performance 1553: a feasibility study, 2004, Data Device Corporation, Bohemia, NY.Google Scholar