Design and flight tests of a holonomic quadrotor UAV with sub-rotor control surfaces
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Tarih
2013
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info:eu-repo/semantics/closedAccess
Özet
In this work, a quadrotor helicopter UAV with sub-rotor control surfaces for non-inclined horizontal motion is designed. Dynamic model of the air vehicle and an eight output PID control system is designed for controlling both the rotor speeds and control surface angles. The performance of this control system on the air vehicle is presented through simulation results with severe wind conditions and initial flight test results acquired from the prototype. © 2013 IEEE.
Açıklama
2013 10th IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013 -- 4 August 2013 through 7 August 2013 -- Takamastu -- 100781
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Kaynak
2013 IEEE International Conference on Mechatronics and Automation, IEEE ICMA 2013
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