• DocumentCode
    233654
  • Title

    Improved ICCP algorithm and its application in gravity matching aided inertial navigation system

  • Author

    Liu Meiqi ; Wang Bo ; Deng Zhihong ; Fu Mengyin

  • Author_Institution
    Nat. Key Lab. of Intell. Control & Decision of Complex Syst., Beijing Inst. of Technol., Beijing, China
  • fYear
    2014
  • fDate
    28-30 July 2014
  • Firstpage
    562
  • Lastpage
    567
  • Abstract
    Considering two disadvantages in traditional gravity matching aided inertial navigation system, low matching accuracy and error accumulation, we propose an improved gravity matching algorithm and aided method for inertial navigation system. Instead of using the sequence sampling, the single point sampling is applied to improve the structure of proposed algorithm, enhancing the matching speed and efficiency. In the aided navigation system method, we use combination of Sage-Husa adaptive filter and strong-tracked Kalman filter to make further optimal estimation of the matching trajectory. Simulation results show the effectiveness of the real-time ICCP algorithm and the combined filter algorithm. Comparing to the traditional methods, proposed method provides higher matching and navigation accuracy.
  • Keywords
    Kalman filters; adaptive filters; gravity; inertial navigation; signal sampling; ICCP algorithm; Sage-Husa adaptive filter; gravity matching algorithm; inertial navigation system; iterated closest contour point algorithm; single point sampling; strong tracked Kalman filter; trajectory matching; Accuracy; Algorithm design and analysis; Filtering algorithms; Filtering theory; Gravity; Navigation; combined filter; gravity aided navigation; single-point sampling;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2014 33rd Chinese
  • Conference_Location
    Nanjing
  • Type

    conf

  • DOI
    10.1109/ChiCC.2014.6896685
  • Filename
    6896685