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
Link To Document