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Published in 2024 at "Robotica"
DOI: 10.1017/s0263574724000523
Abstract: Abstract In this paper, an $\textrm{H}_{{\infty }}$ dynamic output feedback controller is experimentally implemented for the position regulation of a fully actuated tilted-rotor octocopter unmanned aerial vehicle (UAV) to improve wind disturbance rejection during station-keeping.…
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Keywords:
wind disturbance;
textrm infty;
fully actuated;
frequency dependent ... See more keywords