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