DocumentCode :
1795197
Title :
Applications of zero-velocity detector and Kalman filter in zero velocity update for inertial navigation system
Author :
Li Xiaofang ; Mao Yuliang ; Xie Ling ; Chen Jiabin ; Song Chunlei
Author_Institution :
Sch. of Autom., Beijing Inst. of Technol., Beijing, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
1760
Lastpage :
1763
Abstract :
Zero velocity update (ZUPT) is an inexpensive and effective method for error control of inertial navigation system (INS). Detecting the stopping time interval is important for ZUPT methods. The ZUPT method based on Kalman filter has a higher degree of precision compared with the ZUPT method based on curve fitting and the ZUPT method based on maximum likelihood estimation, but the modeling of Kalman filter is critical for the performance of INS. In this paper, three kinds of zero-velocity detectors and a linear discrete Kalman filter model are applied in ZUPT for INS. Simulation results show that the three kinds of zero-velocity detectors are effective, and the ZUPT method based on the linear discrete Kalman filter model makes the positioning accuracy of INS significantly improved.
Keywords :
Kalman filters; curve fitting; inertial navigation; maximum likelihood estimation; satellite navigation; signal detection; ZUPT; curve fitting; error control; inertial navigation system; linear discrete Kalman filter; maximum likelihood estimation; positioning accuracy; time interval; zero-velocity detector; Acceleration; Accelerometers; Detectors; Kalman filters; Mathematical model; Navigation; Noise; Kalman filter; ZUPT; zero-velocity detector;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007449
Filename :
7007449
Link To Document :
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