• DocumentCode
    3612936
  • Title

    Improving GNSS carrier-phase tracking via oscillator g-sensitivity compensation

  • Author

    Bhaskar, Srinivas ; Curran, James T. ; Lachapelle, Gerard

  • Author_Institution
    Accord Software & Syst. Pvt. Ltd., Bangalore, India
  • Volume
    51
  • Issue
    4
  • fYear
    2015
  • Firstpage
    2641
  • Lastpage
    2654
  • Abstract
    In this paper the influence of oscillator g sensitivity on carrier-phase tracking performance in a global navigation satellite-system receiver is examined. It is illustrated that the local oscillator can be a limiting factor in the tracking threshold when the receiver is subject to pedestrian or vehicular dynamics. A novel feed-forward compensation technique is presented, which draws upon the inertial measurement unit resources of the receiver to alleviate these detrimental oscillator-based effects. Performance evaluation considered live global navigation satellite-system signals, a range of consumer-grade oscillators, and both high-quality and Microelectromechanical systems (MEMS)-grade inertial measurement units, in both pedestrian and vehicular operating environments. The results show that the process-noise spectral density corresponding to the signal acceleration state of the Kalman-filter-based tracker can be reduced significantly with compensation. It is also shown that three-dimensional velocity error reduces from 0.17 to 0.06 m/s with compensation.
  • Keywords
    Kalman filters; error compensation; feedforward; inertial navigation; micromechanical devices; satellite navigation; spectral analysis; GNSS carrier-phase tracking; Kalman-filter-based tracker; feed-forward compensation technique; global navigation satellite-system receiver; inertial measurement; microelectromechanical systems; oscillator g-sensitivity compensation; pedestrian dynamics; process-noise spectral density; signal acceleration state; three-dimensional velocity error; vehicular dynamics; Crystals; Global navigation systems; Local oscillators; Measurement units; Receivers; Satellite navigation systems; Satellites; Sensitivity; Tracking;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.2015.130197
  • Filename
    7376207