Abstract
This article focuses on the problem of computing a control law for a particular class of tail-sitter aircraft able to switch their flight configuration from hover to level flight and vice-versa. We address the problem of steering a ducted-fan UAV along a given path (path following problem) so as to meet spatial constraints. One possible scenario is the situation where a vehicle is required to execute collision-free maneuvers under strict spatial limitations and arrive at his final destination while pointing with a camera to a moving target. Path following control in 3D builds on a nonlinear control strategy that is first derived at the kinematic level using the Special Orthogonal Group (SO(3)) theory. © 2011 IEEE.
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CITATION STYLE
Cichella, V., Naldi, R., Dobrokhodov, V., Kaminer, I., & Marconi, L. (2011). On 3D path following control of a ducted-fan UAV on SO(3). In Proceedings of the IEEE Conference on Decision and Control (pp. 3578–3583). Institute of Electrical and Electronics Engineers Inc. https://doi.org/10.1109/CDC.2011.6161419
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