• DocumentCode
    280735
  • Title

    Integrated navigation system architecture

  • Author

    Smith, S.G. ; Stokes, R.F.

  • Author_Institution
    Air Navigation Syst. Div., R. Aerosp. Establ., Farnborough, UK
  • fYear
    1990
  • fDate
    33009
  • Firstpage
    42614
  • Lastpage
    42616
  • Abstract
    The essence of an integrated navigation system is to combine the long-term accuracy of position fixing aids such as GPS, LORAN C, and TRN with the short-term accuracy and continuous availability of the dead-reckoning systems such as INS and Doppler radar. Modern systems use Kalman filter techniques with time-varying gains and which make extensive use of mathematical models of the system dynamics to accomplish this task. An important design feature of an integrated navigation system is the provision of `graceful degradation´, with an indication of the expected level of accuracy to the user. Several conflicting aspects which have to be considered when deciding upon a system architecture are discussed
  • Keywords
    Kalman filters; aerospace computing; aircraft instrumentation; computerised navigation; computerised signal processing; military systems; radionavigation; Doppler radar; GPS; INS; Kalman filter; LORAN C; TRN; dead-reckoning systems; graceful degradation; integrated navigation; military systems; system architecture;
  • fLanguage
    English
  • Publisher
    iet
  • Conference_Titel
    Future Military Avionic Architectures, IEE Colloquium on
  • Conference_Location
    London
  • Type

    conf

  • Filename
    191134