Finite-Time Control Design for a Coaxial Tilt-Rotor UAV

Coaxial tilt-rotor (CTR) unmanned aerial vehicle (UAV) is a system with the specific configuration of two CTR modules and a rear-rotor module. The CTRUAV is a typical strongly coupled, nonlinear, and underactuated system whose control performance is always adversely affected by various disturbances....

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Veröffentlicht in:	IEEE transactions on industrial electronics (1982) Jg. 71; H. 12; S. 16132 - 16142
Hauptverfasser:	Lv, Zongyang, Zhao, Qing, Sun, Xi-Ming, Wu, Yuhu
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.12.2024 The Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Schlagworte:	Attitude control Autonomous aerial vehicles Coaxial tilt-rotor (CTR) Configuration management control allocation law Control systems finite-time control Flight control Flight tests Force Modules Multivariable control Nonlinear control Parameter robustness Resource management Robust control Rotors Torque Transient performance Transmission line matrix methods unmanned aerial vehicle (UAV) Unmanned aerial vehicles
ISSN:	0278-0046, 1557-9948
Online-Zugang:	Volltext
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