Conceptual Design and Control of Twin-Propeller Tail-Sitter mini-UAV: Conceptual Study of V-TS mini-UAV
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F70883521%3A28140%2F19%3A63523624" target="_blank" >RIV/70883521:28140/19:63523624 - isvavai.cz</a>
Result on the web
<a href="https://link.springer.com/article/10.1007%2Fs13272-019-00388-z" target="_blank" >https://link.springer.com/article/10.1007%2Fs13272-019-00388-z</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1007/s13272-019-00388-z" target="_blank" >10.1007/s13272-019-00388-z</a>
Alternative languages
Result language
angličtina
Original language name
Conceptual Design and Control of Twin-Propeller Tail-Sitter mini-UAV: Conceptual Study of V-TS mini-UAV
Original language description
This paper describes progress made on the design and analysis of a twin-propeller tail-sitter mini-UAV (named V-TS). Since the V-TS mini-UAV is a combination of airplanes and copters, high energy efficiency during the forward flight and VTOL capability in the hover flight are achieved. However, this configuration also brings new challenges and difficulties, especially in the case of control. Free software which was used in the design process is presented and described. AVIGLE Demonstrator is analyzed in SU2 to verify correct settings of the aerodynamic analysis. Furthermore, 3D model of the V-TS mini-UAV with the Y-tail configuration and its basic geometrical parameters are shown. The results prove that it is aerodynamically efficient for our purpose. In addition, probably all control modes, transitional flight phases, and difficulties which appear in the control of the twin-propeller tail-sitter mini-UAV are defined and solutions are proposed. The transitional flight phases are determined as a combination of the control modes and sub-modes.
Czech name
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Czech description
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Classification
Type
J<sub>SC</sub> - Article in a specialist periodical, which is included in the SCOPUS database
CEP classification
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OECD FORD branch
20304 - Aerospace 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)<br>S - Specificky vyzkum na vysokych skolach
Others
Publication year
2019
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
CEAS Aeronautical Journal
ISSN
1869-5582
e-ISSN
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Volume of the periodical
10
Issue of the periodical within the volume
3
Country of publishing house
CH - SWITZERLAND
Number of pages
18
Pages from-to
937-954
UT code for WoS article
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EID of the result in the Scopus database
2-s2.0-85069953520