• DocumentCode
    2666442
  • Title

    Pave Pillar in-house research [avionics]

  • Author

    Blair, Jesse L.

  • Author_Institution
    Wright-Patterson Dev. Center, Wright-Patterson AFB, OH, USA
  • fYear
    1990
  • fDate
    21-25 May 1990
  • Firstpage
    197
  • Abstract
    The concepts and technologies required to develop, integrate, and test the Pave Pillar architecture in an avionics system are considered. An in-house research team was formed at the Wright-Patterson Development Center Avionics Laboratory to demonstrate and evaluate architectural and Ada software concepts that relate to modular avionics. The architectural concepts related to line replaceable modules are as defined by the architecture specification for Pave Pillar avionics. The hardware and software issues relating to multiprocessing, multitasking, and real-time reconfiguration are discussed. The integration issues of developing and testing the VHSIC avionic modular processors (VAMPs), high-speed data bus networks, and Ada software are examined. An avionic hot bench simulation was integrated to provide a closed-loop real-time test bed called the integrated test bed (ITB) facility. The configuration and test setup for the avionic modules were selected to provide a realistic environment. There are four VAMP clusters with each cluster consisting of two high-speed data bus modules, two to four Mil-Standard 1750A CPU modules, and one Mil-Standard 1553B bus module. The results from this testing prove the concept of common modules and modular avionics while quantifying the integration issues
  • Keywords
    Ada; aerospace computing; aerospace simulation; aircraft instrumentation; automatic test equipment; closed loop systems; computer architecture; computer networks; microprocessor chips; military computing; military systems; modules; multiprocessing systems; real-time systems; Ada software; Mil-Standard 1553B bus module; Mil-Standard 1750A CPU modules; Pave Pillar architecture; VAMP clusters; VHSIC avionic modular processors; avionic hot bench simulation; closed-loop real-time test bed; high-speed data bus networks; integrated test bed; line replaceable modules; modular avionics; multiprocessing; multitasking; real-time reconfiguration; Aerospace electronics; Aircraft; Computer architecture; Gallium arsenide; Hardware; Laboratories; Sensor systems; Testing; Vehicles; Very high speed integrated circuits;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace and Electronics Conference, 1990. NAECON 1990., Proceedings of the IEEE 1990 National
  • Conference_Location
    Dayton, OH
  • Type

    conf

  • DOI
    10.1109/NAECON.1990.112765
  • Filename
    112765