| MIL-1553 was originally issued by the Department of | | | | 1533 defines data flow, error handling and terminal |
| Defense for military applications. It defines standards | | | | operations requirements. A uniform approach to |
| for functional, mechanical and electrical characteristics | | | | message transmission, data and error handling bus |
| of the serial data bus commonly used in the avionics | | | | components and the associated interfaces, assures |
| of military aircraft. It was developed when the | | | | interoperability. Specifically, multiplex data bus systems |
| integration of computers systems into military aircraft | | | | must function asynchronously in command/response |
| became imminent. Prior to employment of the data bus | | | | mode, with transmission occurring in half-duplex. |
| for digital communications, transmissions were carried | | | | Information transmission control resides solely with the |
| through cables. Erwin Gangl one of the earliest | | | | bus controller. Messages are formed by specified |
| scientists to work on this project set up a method to | | | | command, data, and status words. The standard |
| facilitate digital communications among all avionics | | | | provides a high degree of interoperability. Standard |
| systems, such as radar navigation and data displays | | | | interchangeability makes maintenance manageable and |
| by employing the serial data bus, rather than miles of | | | | allows for a fair amount of innovation in employing |
| cable. | | | | various 1533-compliant components. |
| First seen in the 70's on military fighter jets, it is has | | | | Hardware |
| both military and civil applications. The standard covers | | | | Beyond the two-conductor, twisted, shielded, jacketed |
| the data bus and all associated interface electronics. | | | | cable requirement, the standard defines impedance, |
| 1533 governs bus and terminal operation, data flow, | | | | attenuation, termination and stub requirements. This |
| error handling, hardware and wiring. Although new | | | | section also governs the noise emitted by operations |
| technology would seem to threaten its longevity, | | | | as well the tolerance of data transmissions for noise in |
| durability of 1533 can be attributed to its vast | | | | the environment. Given the challenging environments in |
| international installed base. With so many installations, | | | | which avionics components operate, strict standards |
| manufacture of compliant systems is still good | | | | must be employed with the physical construction of |
| business. So what is the scope of MIL-1533 and what | | | | the data bus and associated electronics. |
| does it mean in avionics? | | | | Redundancy |
| Testing | | | | All standards for testing operations and hardware |
| To be 1533 compliant, all components must to work | | | | apply in their entirety to all redundant systems. There |
| properly under all environmental conditions to which it | | | | are additional requirements to isolate the redundant |
| will be subjected. Consider its application for devices | | | | components to avoid a failure of one eliminating the |
| used on spacecraft which will be subjected to | | | | other as a viable back-up and support a high degree |
| temperature and electrical field extremes. MIL-1533 | | | | of fault tolerance. In general, the standard provides for |
| does not specify the environmental conditions for | | | | only one data bus being active at a time. The |
| testing. These will be determined by the intended use | | | | redundancy standards in MIL-1533 are flexible enough |
| of the specific device employing the multiplex data bus. | | | | to accommodate a variety of applications while still |
| Operations and Messaging | | | | maintaining integrity in redundancy. |