Yıl: 2019 Cilt: 0 Sayı: 15 Sayfa Aralığı: 132 - 142 Metin Dili: İngilizce DOI: 10.31590/ejosat.507222 İndeks Tarihi: 23-09-2020

Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions

Öz:
In this paper, a four-rotor unmanned aerial vehicle was modeled, a control system was designed and performance evaluations weremade. For the control system, a separate mathematical model of the unmanned aerial vehicle longitudinal, lateral and vertical take-offand landing operations is omitted and is expressed as a state space model. The mathematical model of the wind disturbances that willaffect the unmanned aerial vehicle during the flight was created and the situation was added to the space model. Proportional IntegralDerivative (PID) control algorithm was used as the control. Unmanned aerial vehicle modeling was done in Solidworks andsimulations were done in Matlab / Simulink program.
Anahtar Kelime:

Belge Türü: Makale Makale Türü: Araştırma Makalesi Erişim Türü: Erişime Açık
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APA KOSE O, OKTAY T (2019). Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. , 132 - 142. 10.31590/ejosat.507222
Chicago KOSE OGUZ,OKTAY TUGRUL Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. (2019): 132 - 142. 10.31590/ejosat.507222
MLA KOSE OGUZ,OKTAY TUGRUL Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. , 2019, ss.132 - 142. 10.31590/ejosat.507222
AMA KOSE O,OKTAY T Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. . 2019; 132 - 142. 10.31590/ejosat.507222
Vancouver KOSE O,OKTAY T Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. . 2019; 132 - 142. 10.31590/ejosat.507222
IEEE KOSE O,OKTAY T "Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions." , ss.132 - 142, 2019. 10.31590/ejosat.507222
ISNAD KOSE, OGUZ - OKTAY, TUGRUL. "Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions". (2019), 132-142. https://doi.org/10.31590/ejosat.507222
APA KOSE O, OKTAY T (2019). Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. Avrupa Bilim ve Teknoloji Dergisi, 0(15), 132 - 142. 10.31590/ejosat.507222
Chicago KOSE OGUZ,OKTAY TUGRUL Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. Avrupa Bilim ve Teknoloji Dergisi 0, no.15 (2019): 132 - 142. 10.31590/ejosat.507222
MLA KOSE OGUZ,OKTAY TUGRUL Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. Avrupa Bilim ve Teknoloji Dergisi, vol.0, no.15, 2019, ss.132 - 142. 10.31590/ejosat.507222
AMA KOSE O,OKTAY T Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. Avrupa Bilim ve Teknoloji Dergisi. 2019; 0(15): 132 - 142. 10.31590/ejosat.507222
Vancouver KOSE O,OKTAY T Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions. Avrupa Bilim ve Teknoloji Dergisi. 2019; 0(15): 132 - 142. 10.31590/ejosat.507222
IEEE KOSE O,OKTAY T "Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions." Avrupa Bilim ve Teknoloji Dergisi, 0, ss.132 - 142, 2019. 10.31590/ejosat.507222
ISNAD KOSE, OGUZ - OKTAY, TUGRUL. "Dynamic Modeling and Simulation of Quadrotor for Different Flight Conditions". Avrupa Bilim ve Teknoloji Dergisi 15 (2019), 132-142. https://doi.org/10.31590/ejosat.507222