Optimal attitude tracking control for an unmanned aerial quadrotor under lumped disturbances

The robust control problem in attitude tracking of an unmanned aerial vehicle quadrotor is a challenging task due to strong parametric uncertainties, large nonlinearities and high couplings in flight dynamics. In this paper, a continuous nonsingular fast terminal sliding mode controller based on lin...

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Veröffentlicht in:	International journal of micro air vehicles Jg. 12
Hauptverfasser:	Ding, Li, Li, Yangmin
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	London, England SAGE Publications 2020 Sage Publications Ltd
Schlagworte:	Adaptive algorithms Adaptive control Aerodynamics Attitude control Control methods Controllers Couplings Disturbances Optimization Robust control Sliding mode control State observers Tracking control Uncertainty Unmanned aerial vehicles Unmanned helicopters terminal sliding mode attitude tracking control fruit fly optimization algorithm linear extended state observer Quadrotor
ISSN:	1756-8293, 1756-8307
Online-Zugang:	Volltext
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