• DocumentCode
    2015382
  • Title

    An Attitude and Heading Reference System (AHRS) based in a dual filter

  • Author

    Munguia, Rodrigo ; Grau, Antoni

  • Author_Institution
    Dept. of Autom. Control, UPC, Barcelona, Spain
  • fYear
    2011
  • fDate
    5-9 Sept. 2011
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    This paper describes the design, analysis, and experimental results of an Attitude and Heading System based on a Dual Kalman Filtering technique. The presented scheme is suitable for implementation using low cost sensors. Attitude determination systems are essential for real time vehicle navigation, guidance and control applications. When low cost sensors are used, efficient and robust algorithms become necessary for an acceptable performance. For the proposed approach, a low cost Inertial Measurement Unit (IMU), formed by 3-axis gyroscope, 3-axis accelerometer, and 3-axis magnetometer, provides the input measurements. Experimental results with real data show that the proposed algorithm is able to maintain an accurate and drift-free attitude and heading estimation.
  • Keywords
    Kalman filters; accelerometers; aircraft instrumentation; attitude measurement; gyroscopes; inertial navigation; magnetometers; 3-axis accelerometer; 3-axis gyroscope; 3-axis magnetometer; attitude determination system; attitude reference system; dual Kalman filtering technique; heading reference system; inertial measurement unit; real time vehicle control; real time vehicle guidance; real time vehicle navigation; sensor; Accelerometers; Covariance matrix; Estimation; Kinematics; Magnetometers; Quaternions; Sensors;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Emerging Technologies & Factory Automation (ETFA), 2011 IEEE 16th Conference on
  • Conference_Location
    Toulouse
  • ISSN
    1946-0740
  • Print_ISBN
    978-1-4577-0017-0
  • Electronic_ISBN
    1946-0740
  • Type

    conf

  • DOI
    10.1109/ETFA.2011.6059089
  • Filename
    6059089