Control of hybrid aerial vehicle motion in transitional regimes
S. A. Belokon1, D. S. Derishev2, Yu. N. Zolotukhin1, A. A. Nesterov1, M. N. Filippov1
1Institute of Automation and Electrometry, Siberian Branch, Russian Academy of Sciences, Novosibirsk, Russia
2Novosibirsk Research Institute of Aviation Technology and Production Engineering, Novosibirsk, Russia
Keywords: гибридный летательный аппарат, управление в переходных режимах, безразмерные аэродинамические коэффициенты, hybrid aerial vehicle, control in transitional regimes, dimensionless aerodynamic coefficients
Abstract
Results of studying the system used to control the flight of a hybrid aerial vehicle prototype in transitional regimes are presented. The hybrid vehicle is equipped with a quadrotor and main propulsion units. The control system developed in the study includes subsystems for attitude stabilization, vertical takeoff, hovering, and landing, as well as a control subsystem operating in transitional regimes from quadrotor to aircraft modes and back.
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