Synthesis of control for the implementation Of the quadcopter aggressive maneuvers

• Autorzy: Gudzenko, O.
• Języki publikacji: EN

Abstrakty

EN

This paper describes a problem of quadcopter’s control for an implementation of “eight-shape” aggressive maneuver. The maneuver was realized with use linear-quadratic regulator, inverse dynamics control and full state feedback. In this paper these methods are compared in area of the control accuracy and energy consumption. Obtained results allow us to make recommendations for the application of considered methods. The research will help designers to correctly calculate quadcopter’s opportunities to implement aggressive maneuvers. The developed software package allows us to demonstrate the movement of quadcopter in flight.

• Czasopismo: Zeszyty Naukowe. Elektryka / Politechnika Opolska
• Rocznik: 2016
• Tom: z. 72
• Strony: 23--26
• Opis fizyczny: Bibliogr. 4 poz., rys.

Twórcy

autor

Gudzenko, O.

• Faculty of Electrical Engineering, Automatic Control and Informatics Institute of Electromechanical Systems and Industrial Electronics

Bibliografia

• [1] ZHAOA W., GO T.H.: Quadcopter formation flight control combining MPC and robust feedback linearization, Journal of the Franklin Institute, Volume 351, Issue 3, March 2014, pp 1335–1355. DOI: 10.1016/j.jfranklin.2013.10.021
• [2] DIKMEN İ.C., ARISOY A., TEMELTAŞ H.: Attitude Control of a Quadrotor, Recent Advances in Space Technologies, Istanbul, 2009, pp 722–727. DOI: 10.1109/RAST.2009.5158286
• [3] DONG W., GU G.Y., ZHU X., DING H.: Solving the Boundary Value Problem of an Under-Actuated Quadrotor with Subspace Stabilization Approach, Journal of Intelligent and Robotic Systems, Volume 80, Issue 2, November 2015, pp 299–311. DOI: 10.1007/s10846-014-0161-3
• [4] GUDZENKO O.: Synthesis of quadcopter’s controller in an example of loop maneuver, IX Środowiskowe Warsztaty Doktorantów Politechniki Opolskiej, seria Elektryka, nr 355/2015, s. 25–27, Opole-Pokrzywna 201