• DocumentCode
    2178354
  • Title

    Ultra-reliable digital avionics (URDA) processor architecture

  • Author

    Branstetter, Reagan ; Harper, Angela ; Denton, Larry

  • Author_Institution
    Defense Syst. & Electron. Group, Texas Instrum. Inc., Dallas, TX, USA
  • fYear
    1994
  • fDate
    23-27 May 1994
  • Firstpage
    274
  • Abstract
    The objective of the URDA program is to develop a prototype advanced development model (ADM) processor that combines a data processor, signal processor, memory and system interface on a single SEM-E avionics card. TI´s approach integrates two Ada-programmable, URDA basic processor modules (BPMs) with a JIAWG-compatible PiBus and TMBus onto a common SEM-E format ADM module and provides a separate, high-speed (25-MWord/s 100-MByte/s) input/output bus for sensor data. Each BPM provides a peak throughput of 100 MIPS scalar concurrent with 400 MFLOPS vector processing in a removable multichip module (MCM). The URDA BPMs use the chipset and BPM architecture developed on the TI Aladdin program to implement a high-performance processor in an MCM package compatible with assembly onto standard form-factor, liquid-flow-through printed wiring board (PWB) modules. A Mips R4000 family reduced instruction set computer (RISC) processor and a TI 100-MHz bipolar complementary metal-oxide semiconductor (BiCMOS) vector co-processor (VCP) application-specific integrated circuit (ASIC) provide, respectively, the 100 MIPS of scalar processor throughput and 400 MFLOPS of vector processing throughput for each BPM. Extensive software development, system modeling and simulation, and system integration and test tools are provided with the URDA processor
  • Keywords
    BiCMOS integrated circuits; aerospace computing; aircraft; aircraft instrumentation; application specific integrated circuits; fault tolerant computing; multichip modules; reduced instruction set computing; reliability; system buses; vector processor systems; 100 MHz; 100 MIPS; 100 Mbyte/s; 400 MFLOPS; Ada; Ada-programmable modules; JIAWG-compatible PiBus; JIAWG-compatible TMBus; Mips R4000 family; RISC; SEM-E avionics card; SEM-E format ADM module; TI Aladdin program; TI BiCMOS vector co-processor; URDA; application-specific integrated circuit; high-performance processor architecture; high-speed input/output bus; prototype advanced development model; reduced instruction set computer; removable multichip module; scalar processor; software development; system interface; ultra-reliable digital avionics; vector processing; Aerospace electronics; Application specific integrated circuits; Assembly; Computer architecture; Integrated circuit packaging; Multichip modules; Prototypes; Semiconductor device packaging; Signal processing; Throughput;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace and Electronics Conference, 1994. NAECON 1994., Proceedings of the IEEE 1994 National
  • Conference_Location
    Dayton, OH
  • Print_ISBN
    0-7803-1893-5
  • Type

    conf

  • DOI
    10.1109/NAECON.1994.332995
  • Filename
    332995