DocumentCode :
3372097
Title :
Adaptive extended Kalman filtering applied to low-cost MEMS IMU/GPS integration for UAV
Author :
Wang, Xiaogang ; Guo, Jifeng ; Cui, Naigang
Author_Institution :
Dept. of Astronaut. Eng., Harbin Inst. of Technol., Harbin, China
fYear :
2009
fDate :
9-12 Aug. 2009
Firstpage :
2214
Lastpage :
2218
Abstract :
This paper describes the adaptive extended Kalman filtering which is applied to low-cost MEMS IMU/GPS integration. Unmanned Aerial Vehicles are versatile flying machine capable of handling both military and civilian missions. The availability of low-cost MEMS IMU has made it possible to construct inexpensive, integrated systems for usage in UAV applications. The adaptive extended Kalman filtering is applied to fuse the information from low-cost MEMS IMU and a Global Positioning System receiver. The maximum likelihood estimator of Myers and Tapley which could be used to online estimate the process noise is presented. Finally, the simulation result shows the effectiveness of adaptive extended Kalman filtering.
Keywords :
Global Positioning System; adaptive Kalman filters; inertial navigation; maximum likelihood estimation; nonlinear filters; remotely operated vehicles; space vehicles; Global Positioning System receiver; UAV application; adaptive extended Kalman filtering; low-cost MEMS IMU/GPS integration; maximum likelihood estimator; process noise; unmanned aerial vehicle; versatile flying machine; Adaptive filters; Equations; Filtering; Global Positioning System; Kalman filters; Magnetic sensors; Micromechanical devices; Noise level; Noise measurement; Unmanned aerial vehicles; Adaptive extended Kalman filteing; Low-cost MEMS IMU; UAV;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation, 2009. ICMA 2009. International Conference on
Conference_Location :
Changchun
Print_ISBN :
978-1-4244-2692-8
Electronic_ISBN :
978-1-4244-2693-5
Type :
conf
DOI :
10.1109/ICMA.2009.5246654
Filename :
5246654
Link To Document :
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