DocumentCode
3054342
Title
Development of GPS aided INS via Federated Kalman filter
Author
Hajiyev, Ch ; Tutucu, M. Aykut
Author_Institution
Fac. of Aeronaut. & Astronaut., Istanbul Tech. Univ., Turkey
fYear
2003
fDate
20-22 Nov. 2003
Firstpage
569
Lastpage
574
Abstract
In the paper an algorithm on aiding the Inertial Navigation System with GPS is presented. Federated Kalman filter, which includes two different Kalman filters and processes INS and GPS data in real time, is designed for this reason. Simulation is made and presented on the flight dynamics, and it is determined that the algorithm for aiding the INS with GPS, evaluates the motion parameters with high accuracy.
Keywords
Global Positioning System; Kalman filters; aerodynamics; aerospace simulation; GPS aided INS; Global Positioning System; Inertial Navigation System; federated Kalman filter; flight dynamics; motion parameters; real time data; Acceleration; Accelerometers; Aerospace control; Aircraft navigation; Global Positioning System; Gyroscopes; Inertial navigation; Laser radar; Radio navigation; Satellite broadcasting;
fLanguage
English
Publisher
ieee
Conference_Titel
Recent Advances in Space Technologies, 2003. RAST '03. International Conference on. Proceedings of
Conference_Location
Istanbul, Turkey
Print_ISBN
0-7803-8142-4
Type
conf
DOI
10.1109/RAST.2003.1303978
Filename
1303978
Link To Document