Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/3865
Title: Modeling and Simulation of Quadrotor UAV Using PID Controller
Authors: Karahan, M.
Kasnakoğlu, Coşku
Keywords: Altitude control
Attitude control
Dynamic modeling
Mathematical model
PID controller
Quadcopter
Quadrotor
UAV control
Issue Date: Jun-2019
Publisher: Institute of Electrical and Electronics Engineers Inc.
Source: Karahan, M., Kasnakoglu, C. (2019, June). Modeling and Simulation of Quadrotor UAV Using PID Controller. In 2019 11th International Conference on Electronics, Computers and Artificial Intelligence (ECAI) (pp. 1-4). IEEE.
Abstract: Recent developments in sensor technology, actuators and energy storage devices provides opportunities for development of micro flying robots. This paper provides information about modeling and control of a Quadrotor. Proportional Integral Derivative (PID) controller is designed for altitude and attitude control of Quadrotor. Various simulations were performed and it could be interpreted that the PID controller is capable of tracking the desired reference values. Finally, the last section is devoted for discussing the results of each simulation. © 2019 IEEE.
URI: https://hdl.handle.net/20.500.11851/3865
https://ieeexplore.ieee.org/document/9042043
ISBN: 978-172811624-2
Appears in Collections:Elektrik ve Elektronik Mühendisliği Bölümü / Department of Electrical & Electronics Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection

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