Aeronautics and astronautics
Aircraft, heavier-than-air
Helicopter or auto-rotating wing sustained, i.e., gyroplanes
Inventor
active
Aerodynamic surface load sensing
Automatic approach to hover system
Helicopter pitch rate feedback bias for pitch axis maneuvering s
Variable incidence helicopter stabilator and fail safe actuator
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Profile ID: LFUS-PAI-P-16040