An asymmetrically variable wingtip anhedral angles morphing aircraft based on incremental sliding mode control: Improving lateral maneuver capability
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics ; 38 , 1 ; 103166
01.01.2025
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Low-induced-resistance helicopter rotor wing with sweepback anhedral wingtip
Europäisches Patentamt | 2015
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