DocumentCode :
2583648
Title :
A sliding window filter for real-time attitude independent TAM calibration
Author :
Grandvallet, B. ; Zemouche, A. ; Boutayeb, M. ; Changey, S.
Author_Institution :
Centre de Rech. en Autom. de Nancy, Univ. of Henri Poincare, Cosnes et Romain, France
fYear :
2010
fDate :
15-17 Dec. 2010
Firstpage :
467
Lastpage :
472
Abstract :
This paper deals with real time Three-Axis Magnetometers (TAM) calibration, applied to gun-launched spinning projectiles. The first part of this note present a new model used for real time estimation without any knowledge of the attitude of the projectile. Then the main contribution is a new simple and useful filter used for parameters estimation. The latter is formulated in the framework of a traditional Extended Kalman Filter (EKF), which include previous measurements in order to increase the performances and stability of the estimator. Finally numerical simulations support the contribution of the presented algorithm, and good performances are shown in a noisy context without requiring many more computation time than for the classical EKF.
Keywords :
Kalman filters; calibration; magnetometers; military equipment; nonlinear filters; numerical analysis; parameter estimation; projectiles; weapons; extended Kalman filter; gun-launched spinning projectiles; numerical simulation; parameters estimation; real time estimation; sliding window filter; three-axis magnetometer calibration; Calibration; Estimation; Noise; Noise measurement; Projectiles; Real time systems; Sensors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control (CDC), 2010 49th IEEE Conference on
Conference_Location :
Atlanta, GA
ISSN :
0743-1546
Print_ISBN :
978-1-4244-7745-6
Type :
conf
DOI :
10.1109/CDC.2010.5718124
Filename :
5718124
Link To Document :
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