• DocumentCode
    835834
  • Title

    Autonomous fault-tolerant attitude reference system using DTGs in symmetrically skewed configuration

  • Author

    Murugesan, Sugumar

  • Author_Institution
    Indian Space Res. Org., Bangalore
  • Volume
    25
  • Issue
    2
  • fYear
    1989
  • fDate
    3/1/1989 12:00:00 AM
  • Firstpage
    302
  • Lastpage
    307
  • Abstract
    A novel symmetrically skewed configuration for an attitude reference system (ARS) using three dynamically tuned gyros (DTGs) is developed. Simple schemes for autonomous detection and identification of a faulty DTG in real time and subsequent reconfiguration of the attitude estimation algorithm are proposed. The performance of the present configuration is shown to be better than that of configurations proposed earlier, and it is shown to have better features. It tolerates all types of failures of DTG failures, requires very simple computations, and gives less error in attitude estimate than the other configurations
  • Keywords
    aerospace instrumentation; attitude control; gyroscopes; parameter estimation; aerospace instrumentation; attitude estimation algorithm; autonomous detection; dynamically tuned gyros; fault-tolerant attitude reference system; identification; real time; reconfiguration; symmetrically skewed configuration; Attitude control; Error correction; Fault detection; Fault diagnosis; Fault tolerance; Fault tolerant systems; Filters; Space vehicles; State estimation; Target tracking; Yield estimation;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/7.18695
  • Filename
    18695