DocumentCode :
2993248
Title :
Application of Unscented Kalman Filter in GPS /INS
Author :
Zhai Xuhua ; Qi Fengjun ; Zhang Hongtao ; Xu Haifeng
Author_Institution :
Changchun Inst. of Eng. Technol., Changchun, China
fYear :
2012
fDate :
21-23 May 2012
Firstpage :
1
Lastpage :
3
Abstract :
Kalman Filter is an extremely effective and versatile procedure for combining noisy sensor outputs to estimate the state of a system with uncertain dynamics . In this paper, the algorithm of UFK (Unscented Kalman Filter) is developed. By simulated experiment, EKF(Extended Kalman Filter), UKF without and with GPS latency compensation are compared. In result, the UKF algorithm is unbiased and minimum variance. A UKF-based integrated navigation for GPS/INS provides precise position and orientation to the photogrammetric adjustment. In turn, the photogrammetric adjustment provides position updates to the UKF.
Keywords :
Global Positioning System; Kalman filters; inertial navigation; nonlinear filters; state estimation; EKF; GPS latency compensation; GPS/INS; UKF algorithm; UKF-based integrated navigation; extended Kalman filter; noisy sensor output; photogrammetric adjustment; state estimation; uncertain dynamics; unscented Kalman filter; Accuracy; Estimation error; Global Positioning System; Heuristic algorithms; Kalman filters;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Photonics and Optoelectronics (SOPO), 2012 Symposium on
Conference_Location :
Shanghai
ISSN :
2156-8464
Print_ISBN :
978-1-4577-0909-8
Type :
conf
DOI :
10.1109/SOPO.2012.6270470
Filename :
6270470
Link To Document :
بازگشت