• DocumentCode
    3368506
  • Title

    The research on rotation self-compensation scheme of strapdown inertial system

  • Author

    Lin, Zhao ; Xin-zhe, Wang ; Chen, Huang ; Jian-hua, Cheng

  • Author_Institution
    Sch. of Autom., Harbin Eng. Univ., Harbin, China
  • fYear
    2009
  • fDate
    9-12 Aug. 2009
  • Firstpage
    4760
  • Lastpage
    4764
  • Abstract
    The error of inertial measurement unit is the main error of strapdown inertial system. Aiming at the problem that constant error may cause error accumulation of navigation parameters, the paper analyzes the propagation rule of the strapdown inertial system error, and proposes rotation self-compensation technology to modulate the error of inertial measurement unit. Considering rotation around azimuth axis, the paper proposes three representative rotation methods. By analyzing modulation effect on inertial measurement unit error and comparing confine effect on navigation parameters error of the three methods, indicate that the reciprocation rotation self-compensation is the better method. The computer simulation and engineering experiment results show that reciprocating rotation method can confine error effectively and improve the precision of system.
  • Keywords
    compensation; error analysis; inertial navigation; modulation; computer simulation; inertial measurement unit error; modulation effect; navigation parameters; reciprocation rotation self-compensation; strapdown inertial system error; Accelerometers; Computer errors; Costs; Earth; Error analysis; Inertial confinement; Inertial navigation; Measurement units; Mechatronics; Power system reliability; error analysis; self-compensation; single axis rotation; strapdown inertial system;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronics and Automation, 2009. ICMA 2009. International Conference on
  • Conference_Location
    Changchun
  • Print_ISBN
    978-1-4244-2692-8
  • Electronic_ISBN
    978-1-4244-2693-5
  • Type

    conf

  • DOI
    10.1109/ICMA.2009.5246467
  • Filename
    5246467