IBM AP-101

From Wikipedia, the free encyclopedia
Jump to: navigation, search
An upgraded AP-101S used in the Space Shuttle after 1991, left. The earlier model AP-101B used two boxes, right.

The IBM AP-101 is an avionics computer that has been used in the U.S. Space Shuttle, the B-52 and B-1B bombers,[1] and other aircraft. It is a repackaged version of the AP-1 used in the F-15 fighter.[2] When it was designed, it was a high-performance pipelined processor with core memory. While today its specifications are exceeded by most of the modern microprocessors, it was considered high-performance for its era as it could process 480,000 instructions per second (compared to the 7,000 instructions per second of the computer used on Gemini spacecraft).[1] It remains in service (formerly on the space shuttle) because it works and is flight-certified, whereas a new certification would be too expensive. The Space Shuttle AP-101s were augmented by glass cockpit technology.

The AP-101, being the top-of-the-line of the System/4 Pi range, shares its general architecture with the System/360 mainframes.[1] It has 16 32-bit registers, and uses a microprogram to define an instruction set of 154 instructions. Originally only 16 bits were available for addressing memory; later this was extended with four bits from the program status word register, allowing a directly addressable memory range of 1M locations.

The B-1B bomber employed a network of eight model AP-101F computers.[3]

Semiconductor memory board from an IBM AP-101S Space Shuttle General Purpose Computer.

The AP-101B originally used in the Shuttle had core memory. The AP-101S upgrade in the early 1990s used semiconductor memory.[4]

The space shuttle used five AP-101 computers as "general-purpose computers" (GPCs). Four operate in sync, for redundancy, while the fifth is a backup running software written independently. The shuttle software was written in HAL/S, a special-purpose high-level language, whereas AP-101s used by the US Air Force are mostly programmed in JOVIAL, such as the system found on the B-1B Lancer bomber.[5]

References[edit]

  1. ^ a b c Computers in Spaceflight: The NASA Experience - Chapter Four - Computers in the Space Shuttle Avionics System - The DPS hardware configuration
  2. ^ Computers in Spaceflight: The NASA Experience - Chapter Four - Computers in the Space Shuttle Avionics System
  3. ^ Stormont, D.P.; Welgan, R. (23–27 May 1994). "Risk management for the B-1B computer upgrade". Proceedings of National Aerospace and Electronics Conference (NAECON'94) 2: 1143–1149. doi:10.1109/NAECON.1994.332913. 
  4. ^ Norman, P. Glenn (1987), "The new AP101S General-Purpose Computer (GPC) for the Space Shuttle", IEEE Proceedings 75 (3): 308–319, doi:10.1109/PROC.1987.13738 
  5. ^ Jovial to smooth U.S. Air Force shift to Ada. (processing language)

Papers[edit]

  • Vandling, Gilbert C. Organization of a Microprogrammed Aerospace Computer. Computer Design, pp. 65–72, February 1975.

External links[edit]