- MIL-STD-1553 Tutorial and Reference
- MIL-STD-1553B Notices
- MIL HDBK 1553A Notice II
- SAE AS15531 – Latest 1553 Standard
- SAE AS4111 – RT Validation Test Plan
- SAE AS4112 – RT Production Test Plan
- Example 1553 Bus Configuration Diagram
- Example 1553 Cable and Connector Diagram
MIL-STD-1553 has had a long, popular life – and will continue to be supported for decades to come in new and legacy applications. Alta engineers and managers have been in the avionics industry since the early 1980′s and have worked on nearly every major avionics program.
The links to the right provide some of the most useful 1553 references – the same references we use in our product development and support. The MIL-STD-1553 Tutorial and Reference is a summary of the standard and critical aspects in development of a 1553 computer (this document is ideal for quick reference for design and programming). We don’t bother to repeat the detailed parts of the standard because the MIL-STD-1553B Notices and MIL HDBK 1553A Notice II are the best resources. The SAE is the governing body of the 1553 standard and the current versions are copyright controlled under “AS15531″ titles.
Our AltaView and AltaRTVal products offer the best tools for debugging and validating your 1553 system. If you require more information, please contact us. If you need detailed test and training support, the best source in the world is Leroy Earhart of Test Systems, Inc of AZ, USA. www.testsystems.com.
Alta MIL-STD-1553 Tutorial and Reference
MIL-STD-1553 (1553) is a standard that describes a one megabit serial network physical layer (layer one: physical layer – PHY) and message level protocol (layer two: data link layer). Primarily used in legacy avionics, power, sensor and control systems, 1553 has been deployed on thousands of applications worldwide throughout its 35+ year existence including prototype passenger cars, oil platforms, subway control systems and the International Space Station. The US DoD gave-up oversight of the standard (and most MIL-STD documents) in the early 1990s and the standard is now overseen by the Society of Automotive Engineers (SAE) as commercial document “AS15531.”
This overview is designed to complement the referenced MIL HDBK 1553A Notice II document, which provides an excellent detailed review of the 1553 standard (MIL-HDBK-1553A Section 20 provides a summary of MIL-STD-1553B Notice 2). Commercially available chip-sets and interface cards (like Alta’s) “off load” the protocol processing (protocol engine) so the engineer’s primary concern is design/integration of application software and cabling issues. The following paragraphs will highlight the main points of the standard that the design or system engineer needs to know for a successful integration.
The following diagram shows a crude example of a simple network with computers (BC, RTs and/or Monitor), bus cabling, transformer couplers, stub cables and bus terminators. More description on these terms is provided in the following sections. The computers shown in the picture could be actual Line Replacement Units (LRUs) or a PC/VME computer with an Alta 1553 interface card.
A Brief History of Digital Data Busses and History of MIL-STD-1553
Before diving deeper in the review, let’s have a brief history lesson…Erwin Gangl was one of the early pioneers in integrating digital computers into military aircraft while working as an electrical engineer at Dayton’s Wright-Patterson Air Force Base from 1965 to 1988. In the late 1960s he was assigned to handle the digital computer requirements in the F-15 program office. (Ref1)
“With that came the requirement to set up the inter-communication with all of the other avionic subsystems like the radar navigation controls and displays,” said Gangl, who’s considered by many to be the father of the data bus standard (Mil-Std-1553) that led to plug-and-play digital avionics. “Where in the past all signals were connected by stringing point-to-point wires, resulting in big cables and connectors, it became very frustrating to me that this couldn’t be done digitally. So I recommended that we go to a timeshared digital multiplex data bus concept. The digital conversion is done at the sensor, and a digital signal is sent to the computer via a dual redundant shielded twisted wire pair. This replaced having to have the analog-to-digital converter hardware being part of the computer, and also reduced the number of wire cables needed to connect the computer to the rest of the avionics. It turned out that the concept was accepted, and we developed the Mil-Std-1553 data bus standard that is still in use today.” (Ref1)
Today, 1553 is regarded as a low speed computer interconnect standard that can be developed with readily available, low-cost commercial components and is ideal for environmentally harsh environments (especially environments with electrical noise).
(Ref1 = IEEE-USA http://www.ieeeusa.org/communications/features/100yrs.htm