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Device for Measuring Multicopters Performance Parameters

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21260%2F21%3A00352625" target="_blank" >RIV/68407700:21260/21:00352625 - isvavai.cz</a>

  • Result on the web

    <a href="https://doi.org/10.1109/ICMT52455.2021.9502763" target="_blank" >https://doi.org/10.1109/ICMT52455.2021.9502763</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1109/ICMT52455.2021.9502763" target="_blank" >10.1109/ICMT52455.2021.9502763</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Device for Measuring Multicopters Performance Parameters

  • Original language description

    New requirements for classifying unmanned aerial vehicles are forcing institutions as well as manufacturers to devise established procedures and methodologies for testing vehicles. A new possibility of dynamic testing of performance parameters of multicopters is offered in addition to conventional software modeling of flight characteristics and static tests in wind tunnels. This alternative is currently hampered by the problem of flight data collection. This work deals with the design of a complex measuring device specially designed for the testing of the flight characteristics of unmanned aerial vehicles. The proposed modular device provides the user with a flight record containing time-synchronized data showing the linear and angular accelerations achieved by the vehicle during flight, three-axis roll, flight altitude, magnetic course, multicopter speeds, and revolutions of each power unit separately. This work further defines the conditions imposed on the type of tested multicopter (load capacity) and the subsequent need for its balancing. The output of this work is to support the experimental research of dynamic quantification of multicopter performance properties during flight.

  • Czech name

  • Czech description

Classification

  • Type

    D - Article in proceedings

  • CEP classification

  • OECD FORD branch

    20304 - Aerospace engineering

Result continuities

  • Project

  • Continuities

    S - Specificky vyzkum na vysokych skolach

Others

  • Publication year

    2021

  • Confidentiality

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

Data specific for result type

  • Article name in the collection

    2021 International Conference on Military Technologies (ICMT)

  • ISBN

    978-1-6654-3724-0

  • ISSN

  • e-ISSN

  • Number of pages

    7

  • Pages from-to

  • Publisher name

    IEEE Czechoslovakia Section

  • Place of publication

    Praha

  • Event location

    Brno

  • Event date

    Jun 8, 2021

  • Type of event by nationality

    WRD - Celosvětová akce

  • UT code for WoS article