• 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