DocumentCode
3592980
Title
Error analysis of pseudo single point position date range on account of kailman filtering
Author
He, Hong ; Zhang, Shipu ; Liu, Hao ; Zhang, Dajian ; Hou, Mingfeng ; Wang, Kexi
Author_Institution
Tianjin Key Lab. for Control Theor. & Applic. in Complicated Syst., Tianjin Univ. of Technol., Tianjin, China
Volume
1
fYear
2010
Abstract
GPS with a global, all-weather, continuous real-time three-dimensional navigation and positioning capabilities, has a broad application value and development potential. GPS receiver with C / A code has advantage of cheap, small, easy to carry, from the results of position by C / A code GPS receiver outputting, researching the C / A code GPS receiver static positioning accuracy, has important practical value.. Kalman filtering is a linear unbiased minimum variance estimation theory pushdown obtained a recursive filtering method, which introduces the concept of the state space, using the system state transition equation of state of the previous one moment of valuation and the current moment observed value estimated that the new state of Recursive valuation. Experiments show that the Kalman filter introduced into the positioning data as a post-processing tool, which greatly improves the positioning accuracy.
Keywords
Global Positioning System; Kalman filters; error analysis; recursive filters; state-space methods; GPS; Kalman filtering; error analysis; minimum variance estimation theory; pseudo single point position date range; recursive filtering; system state transition; Accuracy; Artificial neural networks; Filtering; Global Positioning System; C/A code; GPS position; Kalman filtering;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Application and System Modeling (ICCASM), 2010 International Conference on
Print_ISBN
978-1-4244-7235-2
Electronic_ISBN
978-1-4244-7237-6
Type
conf
DOI
10.1109/ICCASM.2010.5619184
Filename
5619184
Link To Document