General model and control of an n rotor helicopter

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The purpose of this study was to create a dynamic, nonlinear mathematical model ofa multirotor that would be valid for different numbers of rotors. Furthermore, a set of SingleInput Single Output (SISO) controllers were implemented for attitude control. Both model andcontrollers were tested experimentally on a quadcopter. Using the combined model andcontrollers, simple system simulation and control is possible, by replacing the physical valuesfor the individual systems.
Original languageEnglish
Article number052004
Book seriesJournal of Physics: Conference Series (Online)
Number of pages12
Publication statusPublished - 2015
Event11th European Workshop on Advanced Control and Diagnosis - HTW Berlin, University of Applied Sciences, Berlin, Germany
Duration: 13 Nov 201414 Nov 2014


Conference11th European Workshop on Advanced Control and Diagnosis
LocationHTW Berlin, University of Applied Sciences

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