• DocumentCode
    1797639
  • Title

    Geomagnetic field aided inertial navigation using the SITAN algorithm

  • Author

    Zhiguo Dai ; Chong Kang

  • Author_Institution
    Coll. of Sci., Harbin Eng. Univ., Harbin, China
  • fYear
    2014
  • fDate
    15-17 Nov. 2014
  • Firstpage
    79
  • Lastpage
    83
  • Abstract
    The SITAN algorithm makes use of terrain elevation information to aid inertial navigation system and achieves good results. The geomagnetic field can be used as the conditions of the auxiliary inertial navigation, because the geomagnetic value map and the terrain elevation map have high similarity. By using the SITAN algorithm and combining the contour information of existed geomagnetic map with the processed by the method of interpolation and linear processing at the same time, the aid inertial navigation simulation was carried out for the measured geomagnetic map to provide reference for a new passive and covert method of geomagnetic field aided navigation.
  • Keywords
    aerospace computing; aircraft navigation; geomagnetic navigation; inertial navigation; interpolation; terrain mapping; SITAN algorithm; Sandia inertial terrain aided navigation algorithm; geomagnetic field aided inertial navigation; geomagnetic value map; interpolation method; linear processing method; terrain elevation information; terrain elevation map; Equations; Inertial navigation; Kalman filters; Linearization techniques; Mathematical model; Noise; Aided Inertial Navigation; Geomagnetic field; Linearization technique; SITAN algorithm; Terrain elevation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Systems and Informatics (ICSAI), 2014 2nd International Conference on
  • Conference_Location
    Shanghai
  • Print_ISBN
    978-1-4799-5457-5
  • Type

    conf

  • DOI
    10.1109/ICSAI.2014.7009263
  • Filename
    7009263