Modelling of Unmanned Aerial Vehicle – Tricopter

• Autorzy: Źrebiec J.

Identyfikatory

DOI

10.7494/automat.2016.20.1.7

Warianty tytułu

PL

Modelowanie bezzałogowego statku latającego typu tricopter

• Języki publikacji: EN

Abstrakty

EN

This paper presents detailed models of small aerial unmanned vehicle’s subsystems like propeller, BLDC motor or Li–poly batery. Furthermore, more accurate dynamic model of Tricopter is described. This, multi–system model can be used to synthesize pecise controller which may have the advantage in hazardous situations.

PL

W niniejszym artykule zaprezentowano modele poszczególnych podsystemów wchodzących w skład bezzałogowych statków latających. Opisano między innymi zespół napędowy składający się z silnika bezszczotkowego (BLDC) i śmigła oraz akumulator litowo-polimerowy. Dodatkowo zaproponowano dokładniejszy model dynamiki lotu tricoptera. Przytoczone modele można wykorzystać do syntezy bardziej optymalnego regulatora, który może mieć przewagę w krytycznych sytuacjach.

Słowa kluczowe

EN

UAV modelling; flight dynamics; tricopter; BLDC

PL

dynamika lotu; BLDC; modelowanie UAV; tricopter; bezzałogowy statek latający

• Wydawca: Wydawnictwa AGH
• Czasopismo: Automatyka / Automatics
• Rocznik: 2016
• Tom: Vol. 20, no. 1
• Strony: 7--25
• Opis fizyczny: Bibliogr. 21 poz., rys., tab.

Twórcy

autor

Źrebiec J.

• AGH University of Science and Technology, Department of Automatics and Biomedical Engineering, Krakow, Poland

Bibliografia

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• [20] Źrebiec J., Modelling and control of Tricopter – an Unmanned Aerial Vehicle , Master of science thesis, AGH, Kraków 2015.
• [21] Źrebiec J., Włodarz R., Laboratory model of Tricopter , Bachelors thesis, AGH, Kraków 2013, p. 16

Uwagi

PL

Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).