Synthesis of quadcopter’s controller in an example of loop manoeuver

• Autorzy: Gudzenko, Oleksandr
• Języki publikacji: EN

Abstrakty

EN

This paper presents a method of synthesis of feedback controller based on the method of inverse dynamics, and applies this method for loop manoeuver. The motivation was to test the quadcopter’s behaviour during a flight on a complex trajectory. In the paper was used developed by the author a model taking into account asymmetric construction of quadcopter.

• Czasopismo: Zeszyty Naukowe. Elektryka / Politechnika Opolska
• Rocznik: 2015
• Tom: z. 71
• Strony: 25--27
• Opis fizyczny: Bibliogr. 3 poz., rys.

Twórcy

autor

Gudzenko, Oleksandr

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

Bibliografia

• [1] ZHAO W., HIONG GO T.: Quadcopter formation flight control combining MPC and robust feedback linearization. Journal of the Franklin Institute. Vol. 351, Issue 3, March 2014, pp. 1335–1355.
• [2] LUUKKONEN T.: Modelling and Control of Quadcopter. School of Science, Espoo, August 22, 2011, p. 26, http://sal.aalto.fi/publications/pdf-files/eluu11_public.pdf
• [3] DIKMEN I.C., ARISOY A., TEMELTAS H.: Attitude control of a quadrotor. 4th International Conference on Recent Advances in Space Technologies, 2009, pp. 722–727.