Mathematical Modelling And Simulation of Quadrotor
Journal Title: IOSR Journals (IOSR Journal of Electrical and Electronics Engineering) - Year 2017, Vol 12, Issue 6
Abstract
Nowadays unmanned aerial vehicles are being used surveilance, search and rescue, damage assesment alongwith areas where dangereous for people to work. In this work, 4-rotor unmanned aerial vehicle design, altitude and orientation controls of unmanned aerial vehicle are aimed. Quadrotor’s mathematical model is mostly focused in this work. Quadrotor has 6 degrees of freedom. Inertial Measurement Unit will be composed for flight stability. Quadrotor’s altitude, speed, direction and position datas will be chased and evaluated by the Inertial Measurement Unit. There will be a Quadrotor’s central microcontroller which will manage all the components that necessary for flight. This microcontroller will use the data coming from Inertial Measurement Unit and user inorder to control motor speed. The Quadrotor of mathematical model were obtained using Newton-Euler equation. The PID controller is designed to control the model. The performance of controllers and the model was investigated by using Matlab Simulink program.
Authors and Affiliations
İrfan Ökten, Mehmet Çınar
Keywords
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- EP ID EP388456
- DOI 10.9790/1676-1206021118.
- Views 153
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