Attitude Control of Multicopter
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26220%2F12%3APU100859" target="_blank" >RIV/00216305:26220/12:PU100859 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Attitude Control of Multicopter
Original language description
This article deals with the problem of attitude control of multicopters. At first the basic properties of multicopters are described. Regarding the attitude control, representation of attitude and computation of errors using rotation matrices are mentioned. Since the dynamics of rotation motion of multicopter around each axis is similar and almost independent to each other, the attitude control is split to three independent control loops. Then the construction of simplified model of multicopter with onedegree of rotation freedom is described. Also the dynamics of thrusts of propellers are taken into account in the model. Finally one of the possible controller designs is described and for reference the results of controller with parameters tuned usingMATLAB tool are shown.
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JB - Sensors, detecting elements, measurement and regulation
OECD FORD branch
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Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
ElectroScope - http://www.electroscope.zcu.cz
ISSN
1802-4564
e-ISSN
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Volume of the periodical
2012
Issue of the periodical within the volume
5
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
5
Pages from-to
1-5
UT code for WoS article
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EID of the result in the Scopus database
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