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
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