SYNTHESIS OF CONTROL SYSTEM FOR A QUADROCOPTER WITH THE USE OF A SIMPLIFIED MATHEMATICAL MODEL
ITMO University, Saint Petersburg, 197101, Russian Federation; Full Professor, Dean
T. A. Maltseva
ITMO University, Department of Control Systems and Informatics; Student
D. V. Labadin
ITMO University, Department of Control Systems and Informatics; Student
M. O. Surov
St. Petersburg National Research University of Information Technologies, Mechanics and Optics, Department of Control Systems and Informatics;
A. A. Bobtsov
ITMO University, Saint Petersburg, 197101, Russian Federation; Head of the School of Computer Technologies and Control, Professor at the Faculty of Control Systems and Robotics, Head of the Adaptive and Nonlinear Control Systems Lab
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Abstract. An algorithm for synthesis of a control system for a quadrocopter is presented. The algorithm is based on a simplified mathematical model and is easy to realize in contrast to the known algorithms.
Keywords:
quadrocopter, simplified model, multi-rotor aircraft