Finite-time Convergence Control For A Quadrotor Unmanned Aerial Vehicle With A Slung load

This work investigates the control technique for a quadrotor unmanned aerial vehicle with a slung load. By taking the advantage of the cascade property, a new hierarchical control scheme is designed that divides the control problem into three parts. For the attitude motion control of the quadrotor,...

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Veröffentlicht in:	IEEE transactions on industrial informatics Jg. 20; H. 1; S. 1 - 9
Hauptverfasser:	Yang, Sen, Xian, Bin, Cai, Jiaming, Wang, Guangyi
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Piscataway IEEE 01.01.2024 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Attitude control Autonomous aerial vehicles Closed loops Control design Control theory Convergence Feedback control finite-time convergence Motion control Nonlinear control Quadrotors Sliding mode control slung load Stability analysis Trajectory UAV Unmanned aerial vehicles Unmanned helicopters
ISSN:	1551-3203, 1941-0050
Online-Zugang:	Volltext
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