Modelling, attitude controller design and flight experiments of a novel micro-ducted-fan aircraft
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DOI: 10.1177/1687814018765569
Abstract: This research concerns a novel micro-ducted-fan aircraft. A structured attitude controller is designed for a novel unmanned aerial vehicle in the presence of strong state coupling and system perturbation. The novel unmanned aerial vehicle is… read more here.
Keywords: aircraft; novel micro; micro ducted; controller ... See more keywords