• DocumentCode
    2791393
  • Title

    Best choice of coordinate system for tracking coordinated turns

  • Author

    Gustafsson, F. Redrik ; Isaksson, Alf J.

  • Author_Institution
    Dept. of Electr. Eng., Linkoping Univ., Sweden
  • Volume
    3
  • fYear
    1996
  • fDate
    11-13 Dec 1996
  • Firstpage
    3145
  • Abstract
    A standard approach to tracking is to use the extended Kalman filter (EKF) applied to a nonlinear state-space model. We compare two conceivable choices of state variables for modeling civil aircrafts. One where Cartesian velocities are used and one where absolute velocity and heading angle are used. In both choices, Cartesian coordinates are used for position and angular velocity for turning. It is shown that the latter state vector always performs better. This is proven by considering the linearization error made in the extended Kalman filter applied either to a time-continuous model or a discretized model. The result is supported by a Monte Carlo simulation study
  • Keywords
    Kalman filters; Monte Carlo methods; aircraft; covariance matrices; nonlinear filters; radar tracking; Cartesian velocities; Monte Carlo simulation study; civil aircrafts; coordinate system; coordinated turns; discretized model; extended Kalman filter; linearization error; nonlinear state-space model; time-continuous model; tracking; Acceleration; Air traffic control; Airborne radar; Aircraft propulsion; Angular velocity; Error analysis; Radar measurements; Radar tracking; Target tracking; Turning;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Decision and Control, 1996., Proceedings of the 35th IEEE Conference on
  • Conference_Location
    Kobe
  • ISSN
    0191-2216
  • Print_ISBN
    0-7803-3590-2
  • Type

    conf

  • DOI
    10.1109/CDC.1996.573612
  • Filename
    573612