• DocumentCode
    790296
  • Title

    Next generation space avionics: layered system implementation

  • Author

    Black, Randy ; Fletcher, Mitch

  • Author_Institution
    Honeywell Int., Glendale, AZ, USA
  • Volume
    20
  • Issue
    12
  • fYear
    2005
  • Firstpage
    9
  • Lastpage
    14
  • Abstract
    Advances in electronics over the past decade have produced major improvements in the power and flexibility of computer systems. Unfortunately current avionics systems for space applications typically have not leveraged these COTS advantages. A decade ago, the state-of-the-art for avionics systems made a step change to the Integrated Modular Avionics (IMA) used in the Boeing 777. This next generation avionics architecture is not based upon traditional Byzantine redundancy structures, but on a truth-based scheme where each element knows when an internal failure occurs and removes itself from the system. IMA utilizes a lock-step microprocessor design that communicates to a COTS Backplane for input/output, and to a Virtual Backplane™ (a reliable high-speed serial bus) for intra-system communication. The system functions are implemented using a time and space partitioned operating system. The entire system provides the simplicity of a simplex system, implements the highest level of reliability providing complete flexibility to reconfigure both software applications and hardware interfaces, allows for rapid prototyping using low-cost COTS hardware, and is easily expandable beyond the initial point implementation. As the only 5th generation avionics architecture, the concepts incorporated into Honeywell´s IMA are ideally suited to be the backbone of the next generation Space Exploration Program avionics architectures.
  • Keywords
    space vehicle electronics; COTS; IMA; Integrated Modular Avionics; Virtual Backplane; avionics architecture; internal failure; intra-system communication; layered system implementation; lock-step microprocessor design; simplex system; space avionics; truth-based scheme; Aerospace electronics; Application software; Backplanes; Computer architecture; Hardware; Microprocessors; Operating systems; Redundancy; Software prototyping; Spine;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/MAES.2005.1576097
  • Filename
    1576097