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
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;
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
DOI :
10.1109/ICCASM.2010.5619184