DocumentCode
3451114
Title
Geomagnetic Surface Navigation Using Adaptive EKF
Author
Mu, Hua ; Wu, Meiping ; Hu, Xiaoping ; Ma, Hongxu
Author_Institution
Nat. Univ. of Defense Technol., Changsha
fYear
2007
fDate
23-25 May 2007
Firstpage
2821
Lastpage
2825
Abstract
In need of accurate and covert positioning, a geomagnetic surface navigation system is investigated in the paper. The Earth anomaly magnetic field intensity is selected as the reference to bound the INS (inertial navigation system) errors. Using stochastic linearization technique, we have proposed an EKF (extended Kalman filtering) algorithm which is adaptive in two aspects: linearization region size determination and linearization noise variance estimation. Simulation results show that the proposed algorithm can achieve high positioning accuracy with moderate initial position errors and has great robustness with respect to the velocity errors, attitude errors and the geomagnetic map quality. The geomagnetic navigation system can be extended to air and underwater applications.
Keywords
adaptive Kalman filters; geomagnetism; inertial navigation; linearisation techniques; magnetic field measurement; stochastic processes; Earth anomaly magnetic field intensity; adaptive EKF; attitude errors; covert positioning; extended Kalman filtering; geomagnetic map quality; geomagnetic surface navigation; inertial navigation system; linearization noise variance estimation; linearization region size determination; stochastic linearization techniques; velocity errors; Adaptive filters; Earth; Filtering; Geomagnetism; Inertial navigation; Kalman filters; Linearization techniques; Magnetic fields; Magnetic separation; Stochastic resonance;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics and Applications, 2007. ICIEA 2007. 2nd IEEE Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4244-0737-8
Electronic_ISBN
978-1-4244-0737-8
Type
conf
DOI
10.1109/ICIEA.2007.4318926
Filename
4318926
Link To Document