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
—