Experiment of the State Variable Feedback for a Quadrotor

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This work is the design of the robust attitude stabilization of a quadrotor. The dynamics model of the quadrotor is normally non-linear and it is difficult to obtain an accurate dynamic model. The linearized model is obtained based on data from experiments. The Multiple Input Multiple Output (MIMO) state variable feedback control is implemented to stabilize the system. The dynamic model based on approximated torques (roll, pitch, and yaw) as inputs and the dynamic model based on rotational speeds of the four rotors are used for design the controller. The experimental results from both dynamic model has very similar characteristic and perform much better than the conventional controller.

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267-272

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August 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] UAVs. New world vista: Air and space for 21st century. Human systems and biotechnology systems, 7. 0: 17-18, (1997).

Google Scholar

[2] Pero Castillo, Rogelio Lozano and Alejandro E. Dzul (2005). Modelling and Control of Mini-Flying, ISBN: 185233957, Springer-Verlag London.

Google Scholar

[3] S. Bouabdallah, Design and control of quadrotors with application to autonomous flying, Ph.D. dissertation, EPFL, (2006).

Google Scholar

[4] Thorhallur Tomas Buchholz and Dagur Gretarsson (2009). Construction of a Four Rotor Helicopter Control System, Master's Thesis, Technical University of Denmark.

Google Scholar

[5] Viboon Sangveraphunsiri. Control of Dynamic System, 3rd Edition, Chulapress, Bangkok, (2013).

Google Scholar

[6] Roman Czyba, Attitude Stabilization of an Indoor Quadrotor, EMAV, (2009).

Google Scholar

[7] Sang-hyun Lee, Seung Hoon Kang and Youdan Kim, Trajectory Tracking Control of Quadrotor UAV, in International Conference on Control, Autonomous and Systems, (KINTEX, Gyeonggi-do, Korea), Oct. 26-29, (2011).

Google Scholar