• DocumentCode
    3708577
  • Title

    Beacon aided attitude estimation using Angle of Arrival measurements

  • Author

    Kyungwoo Yoo;Joohwan Chun;Seungoh Yoo

  • Author_Institution
    Korea Advanced Institute of Science and Technology, KAIST, Daejeon, Republic of Korea
  • fYear
    2015
  • Firstpage
    1
  • Lastpage
    5
  • Abstract
    To improve accuracy of navigation solutions such as position, velocity and attitude etc., various navigation techniques are developed. Among them, Global Positioning System (GPS) and Inertial Navigation System (INS) are widely used in general navigation system. Additionally, in nowadays, to provide more accurate navigation solution, Extend Kalman Filter (EKF) based GPS/INS coupled system which calibrates navigation solution of INS by using GPS is proposed actively. However, in general GPS/INS coupled system, since GPS calibrates position and velocity only, the attitude cannot be calibrated directly in present GPS/INS coupled system and this feature can be vulnerable to sea environment where the attitude fluctuation occurs frequently. To complement this drawback, the angle-based attitude estimation technique using beacon is proposed in this paper. The proposed technique uses the Angle of Arrival (AoA) measurements of the received signals from array antenna and estimates the own attitude. The proposed technique is also coupled with INS and the performance of the proposed technique is shown through simulation results.
  • Keywords
    "Mathematical model","Estimation","Global Positioning System","Antenna measurements","Earth","Arrays"
  • Publisher
    ieee
  • Conference_Titel
    Navigation World Congress (IAIN), 2015 International Association of Institutes of
  • Type

    conf

  • DOI
    10.1109/IAIN.2015.7352234
  • Filename
    7352234