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Kalman Filter Based Integrated Air Data/GPS Navigation System - Couverture souple

Mutlu, Taner; HAJIYEV, CHINGIZ

 
9783844301755: Kalman Filter Based Integrated Air Data/GPS Navigation System
Couverture souple
ISBN 10 : 3844301755 ISBN 13 : 9783844301755
Editeur : LAP LAMBERT Academic Publishing, 2012

Synopsis

This monograph is focused on the improvement of the modern navigation systems. In aeronautics high precision is very essential. Global Positioning System (GPS) has revolutionized the navigation systems. In this study GPS position measurements obtained from a GPS receiver, are improved using Kalman Filter based Satellite Distances method. The GPS receiver provides us with both available satellite positions and the position of the receiver. Using this information in the Kalman Filter a better position compared to the GPS receiver alone was aimed. In the monograph the integration of two navigation systems ADS and GPS was aimed. ADS is a widely used navigation system which measures static and total air pressure and the air temperature. ADS has high sampling frequency and poor accuracy, on the other hand, GPS has high accuracy compared to ADS but lower sampling frequency. Kalman Filter is used to integrate and minimize the errors of the two navigation systems. By this integration a navigation system with high sampling frequency and high accuracy is aimed. Another object is to calculate the wind speed with high accuracy, which is actually the error of Air Speed measured by the ADS.

Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.

Présentation de l'éditeur

This monograph is focused on the improvement of the modern navigation systems. In aeronautics high precision is very essential. Global Positioning System (GPS) has revolutionized the navigation systems. In this study GPS position measurements obtained from a GPS receiver, are improved using Kalman Filter based Satellite Distances method. The GPS receiver provides us with both available satellite positions and the position of the receiver. Using this information in the Kalman Filter a better position compared to the GPS receiver alone was aimed. In the monograph the integration of two navigation systems ADS and GPS was aimed. ADS is a widely used navigation system which measures static and total air pressure and the air temperature. ADS has high sampling frequency and poor accuracy, on the other hand, GPS has high accuracy compared to ADS but lower sampling frequency. Kalman Filter is used to integrate and minimize the errors of the two navigation systems. By this integration a navigation system with high sampling frequency and high accuracy is aimed. Another object is to calculate the wind speed with high accuracy, which is actually the error of Air Speed measured by the ADS.

Biographie de l'auteur

Taner Mutlu graduated from Electronics Engineering Dept. of Istanbul University in 2003. He received MSc degree in Aeuronautical Enginnering at Istanbul Technical University(ITU) in 2007. At present he is doing PhD at the same department. He has worked as avionics and electrical systems designer at manned and unmanned helicopter projects at ITU.

Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.

Éditeur
LAP LAMBERT Academic Publishing
Date d'édition
2012
Langue
anglais
ISBN 10 
3844301755
ISBN 13 
9783844301755
Reliure
Broché
Nombre de pages
148
Coordonnées du fabricant
non disponible
Personne responsable
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