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Precision Landing Options in Unmanned Aerial Vehicles

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26220%2F18%3APU128253" target="_blank" >RIV/00216305:26220/18:PU128253 - isvavai.cz</a>

  • Result on the web

    <a href="https://ieeexplore.ieee.org/abstract/document/8388325/" target="_blank" >https://ieeexplore.ieee.org/abstract/document/8388325/</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1109/IIPHDW.2018.8388325" target="_blank" >10.1109/IIPHDW.2018.8388325</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Precision Landing Options in Unmanned Aerial Vehicles

  • Original language description

    This paper presents a precision landing system for unmanned aerial vehicles (UAVs). When designing the solution, we paid special attention to the required accuracy of the various sensors. The system comprises a highly accurate flight controller and a visual sensor for object detection. The platform is constructed to integrate into various types of unmanned aerial vehicles. The method for the visual tracking of the landing platform via an optical camera enables us to increase the landing reliability. The precise position of the unmanned aerial vehicle at landing is provided by an image analysis where the specially designed landing platform is detected. All calculations for precision landing guidance are performed directly on board. An infrared (IR) camera is used as the main sensor for monitoring the IR light beam. This aircraft guidance technique does not necessitate data transfer to and from the landing station. The proposed system can be a suitable solution to replace more complex and expensive systems, such as RTK GPS (Real-Time Kinematic Global Positioning System). A hexacopter drone was used for the test flights, and the results obtained were then subjected to comparison. The navigation to the location was first tested by a GPS sensor only; subsequent tests flights, however, already relied on a visual sensor. All of the precision landing options eventually yielded the required quality.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20201 - Electrical and electronic engineering

Result continuities

  • Project

    Result was created during the realization of more than one project. More information in the Projects tab.

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Others

  • Publication year

    2018

  • Confidentiality

    S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Data specific for result type

  • Article name in the collection

    2018 International Interdisciplinary PhD Workshop (IIPhDW)

  • ISBN

    978-1-5386-6143-7

  • ISSN

  • e-ISSN

  • Number of pages

    3

  • Pages from-to

    58-60

  • Publisher name

    IEEE

  • Place of publication

    Świnoujście, Poland

  • Event location

    Swinouscie

  • Event date

    May 9, 2018

  • Type of event by nationality

    EUR - Evropská akce

  • UT code for WoS article