Dynamic modeling and displacement control for differential flatness of quadrotor UAV slung-load system

In this paper, the quantitative simulation studies of a quadrotor unmanned aerial vehicles (Q-UAVs) carrying a payload are designed and holding a robust position and attitude tracking control problem of a Q-UAVs subject to system nonlinearities, input coupling, aerodynamic uncertainties and external...

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Veröffentlicht in:	International journal of dynamics and control Jg. 11; H. 2; S. 637 - 655
Hauptverfasser:	Roy, Kumud Ranjan, Waghmare, Laxman M., Patre, Balasaheb M.
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Berlin/Heidelberg Springer Berlin Heidelberg 01.04.2023 Springer Nature B.V
Schlagworte:	Aircraft Attitude control Closed loop systems Complexity Control Control algorithms Control and Systems Theory Controllers Design Displacement Disturbance observers Dynamic inversion Dynamic models Dynamical Systems Engineering Helicopters Mathematical models Nonlinear dynamics Nonlinearity Systems stability Tracking control Unmanned aerial vehicles Unmanned helicopters Vehicles Vibration Robust nonlinear dynamic inversion design Slung payload Disturbance observer Differential flatness Unmanned aerial vehicle
ISSN:	2195-268X, 2195-2698
Online-Zugang:	Volltext
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