• DocumentCode
    3613031
  • Title

    Attitude estimation and sensor identification utilizing nonlinear filters based on a low-cost MEMS magnetometer and sun sensor

  • Author

    Teshnizi, Masoud Mirzaei ; Shirazi, Abolfazl

  • Author_Institution
    Sharif Univ. of Technol., Tehran, Iran
  • Volume
    30
  • Issue
    12
  • fYear
    2015
  • fDate
    12/1/2015 12:00:00 AM
  • Firstpage
    20
  • Lastpage
    33
  • Abstract
    A combination of low-cost micro-electoro-mechanical sensors (MEMSs) and nonlinear attitude estimation algorithm techniques can provide an inexpensive and accurate system for navigation and attitude determination. The features of MEMSs are their light weight and small size; hence, the MEMSs have found significant attention in low-cost navigation and control systems. A common disadvantage of these sensors is the significant errors that accompany the corresponding measurements. The accuracy obtained using MEMSs depends on a number of factors, such as scale factor, bias, and random noise corrections. However, these low-cost sensors suffer from large noise and errors, making calibration and error identification of critical importance.
  • Keywords
    attitude measurement; calibration; magnetometers; microsensors; navigation; nonlinear filters; sun sensors; MEMS magnetometer; attitude determination; calibration; control system; error identification; microelectromechanical sensor; navigation; nonlinear attitude estimation algorithm; nonlinear filter; random noise correction; scale factor; sensor identification; sun sensor; Electromechanical devices; Magnetic field measurement; Magnetometers; Microelectoromechanical sensors; Nonlinear attitude estimation; Quaternions; Satellites; Sensors;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems Magazine, IEEE
  • Publisher
    ieee
  • ISSN
    0885-8985
  • Type

    jour

  • DOI
    10.1109/MAES.2015.150069
  • Filename
    7381287