DocumentCode :
1881691
Title :
Robust nonlinear filtering applied to integrated navigation system INS/GNSS under non Gaussian measurement noise effect
Author :
Benzerrouk, Hamza ; Nebylov, Alexander
Author_Institution :
Int. Inst. for Adv. Aerosp. Technol., St.-Petersburg State Univ. of Aerosp. Instrum., St. Petersburg, Russia
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
8
Abstract :
In this paper, robust design of INS/GNSS navigation system is proposed for solving problem of state space models with non Gaussian measurement noise based on parallel non linear filtering. GNSS in this paper is assumed a combination of GPS and GLONASS signals in order to improve and increase accuracy of satellite positioning. Non linear approximation techniques such as Extended Kalman Filter (EKF), Sigma Point Kalman Filter (SPKF) are adapted. Robust navigation system is designed and efficiently estimates state vector of navigation. Three parallel algorithms are simulated and compared through RMSE criteria under several conditions.
Keywords :
Global Positioning System; Kalman filters; nonlinear filters; GLONASS signals; GPS signals; INS/GNSS; extended Kalman filter; integrated navigation system; nonGaussian measurement noise effect; nonlinear approximation techniques; parallel nonlinear filtering; robust nonlinear filtering; satellite positioning; sigma point Kalman filter; state space models; Estimation; Global Navigation Satellite Systems; Kalman filters; Mathematical model; Maximum likelihood detection; Nonlinear filters; Robustness;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187141
Filename :
6187141
Link To Document :
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