• DocumentCode
    3456603
  • Title

    Application of extended Kalman filter in ultra-tight GPS/INS integration based on GPS software receiver

  • Author

    Yu, Jing ; Chen, Xiyuan

  • Author_Institution
    Key Lab. of Micro-Inertial Instrum. & Adv. Navig. Technol., Southeast Univ., Nanjing, China
  • fYear
    2010
  • fDate
    21-23 June 2010
  • Firstpage
    82
  • Lastpage
    86
  • Abstract
    When designing the ultra-tight GPS/INS integration, the architecture of Kalman filter is the key to its successful performance; the crux of this architecture is the measurement model. Aiming at the dependence of numbers of tracked GPS satellites and poor noise immunity in loose and tight integration modes, this paper proposes a new method of ultra-tight integration, using the Q(quadrature) signal from the GPS receiver correlator, receiver position and velocity to form the measurements of the extended Kalman filter. The experiments are carried out based on semi-physics, using the factual data solved by GPS software receiver, and the results show good performance.
  • Keywords
    Global Positioning System; Kalman filters; artificial satellites; inertial navigation; radio receivers; GPS satellites; GPS software receiver; GPS-INS integration; extended Kalman filter; noise immunity; quadrature signal; Application software; Global Positioning System; Instruments; Navigation; Position measurement; Q measurement; Satellites; Software performance; Tracking loops; Velocity measurement; Extended Kalman filter; GPS/INS; Ultra-tight integration;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Green Circuits and Systems (ICGCS), 2010 International Conference on
  • Conference_Location
    Shanghai
  • Print_ISBN
    978-1-4244-6876-8
  • Electronic_ISBN
    978-1-4244-6877-5
  • Type

    conf

  • DOI
    10.1109/ICGCS.2010.5543092
  • Filename
    5543092