DocumentCode :
731558
Title :
Improvement of altitude precision in indoor and urban canyon navigation for small flying vehicles
Author :
Petritoli, Enrico ; Leccese, Fabio
Author_Institution :
Sci. Dept., Univ. degli Studi “Roma Tre”, Rome, Italy
fYear :
2015
fDate :
4-5 June 2015
Firstpage :
56
Lastpage :
60
Abstract :
Because of integrating measurements, the Inertial Navigation System (INS) for UAVs or small planes has the great drawback to increase the uncertainty for those entities, as acceleration and angular velocity that are function of time. For this reason, it generally employs GPS in order to correct and calibrate itself. When GPS is not available, typically in environments such as urban canyons or indoor navigation, is necessary to measure the altitude using stored map terrain profile and a LiDAR altimeter: weighting these data through a least square method, we can obtain the altitude of the vehicle non affected by local discontinuities of the ground.
Keywords :
Global Positioning System; aircraft navigation; autonomous aerial vehicles; height measurement; indoor navigation; inertial navigation; GPS; INS; LiDAR altimeter; UAVs; altitude measurement; altitude precision; angular velocity; indoor canyon navigation; inertial navigation system; least square method; small flying vehicles; stored map terrain profile; urban canyon navigation; Global Positioning System; Laser radar; Least squares approximations; Measurement uncertainty; Sea measurements; Vehicles; Accuracy; Altitude; Error; Improvements; Navigation; UAV;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Metrology for Aerospace (MetroAeroSpace), 2015 IEEE
Conference_Location :
Benevento
Type :
conf
DOI :
10.1109/MetroAeroSpace.2015.7180626
Filename :
7180626
Link To Document :
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