• DocumentCode
    1496664
  • Title

    X-33 redundancy management system

  • Author

    Bolduc, L.P.

  • Author_Institution
    Aerosp. Electron. Syst., Honeywell Int. Inc., Columbia, MD
  • Volume
    16
  • Issue
    5
  • fYear
    2001
  • fDate
    5/1/2001 12:00:00 AM
  • Firstpage
    23
  • Lastpage
    28
  • Abstract
    The X-33 is an unmanned advanced technology demonstrator with a mission to validate new technologies for the next generation of Reusable Launch Vehicles. Various system redundancies are designed in the X-33 to enhance the probability of successfully completing its mission in the event of faults and failures during flight. One such redundant system is the Vehicle and Mission Computer that controls the X-33 ea, and manages the avionics subsystems. Historically, redundancy management and applications such as flight control and vehicle management tended to be highly coupled. One of the technologies that the X-33 will demonstrate is the Redundancy Management System (RMS) that uncouples the applications from the redundancy management details, in the same way that real-time operating systems have uncoupled applications from task scheduling, communication and synchronization details
  • Keywords
    aerospace control; real-time systems; redundancy; space vehicles; X-33 redundancy management system; avionics subsystems; flight control; real-time operating systems; reusable launch vehicles; synchronization details; system redundancies; task scheduling; unmanned advanced technology demonstrator; vehicle management; Aerospace control; Aerospace electronics; Application software; Computer architecture; Fault detection; Hardware; Physics computing; Redundancy; Technology management; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/62.925693
  • Filename
    925693