Robust-augmentation nonlinear dynamic inversion control of over-actuated coaxial high-speed helicopter in transition mode
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics ; 37 , 8
01.08.2024
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Coaxial high-speed direct-driven helicopter and flight control mode thereof
Europäisches Patentamt | 2015
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