DocumentCode
3705010
Title
Integration of inertial and satellite navigation systems using corrective circuits for UAV
Author
V.M. Vasyliev;V.O. Rogozhyn;B.I Dolintse
Author_Institution
Institute of Air Navigation, National Aviation University, Kyiv, Ukraine
fYear
2015
Firstpage
193
Lastpage
197
Abstract
The scheme of integration of inertial and satellite navigation systems with corrective circuits for low-cost unmanned aerial vehicles is proposed. Based on derived mathematical model describing the errors of navigation parameters evaluation in the integrated inertial-satellite navigation system the study of system accuracy in static and dynamic operation mode has been done.
Keywords
"Satellite navigation systems","Mathematical model","Unmanned aerial vehicles","Steady-state","Conferences","Radio navigation"
Publisher
ieee
Conference_Titel
Actual Problems of Unmanned Aerial Vehicles Developments (APUAVD), 2015 IEEE International Conference
Print_ISBN
978-1-4673-6566-6
Type
conf
DOI
10.1109/APUAVD.2015.7346597
Filename
7346597
Link To Document