A vertical take-off and landing (VTOL) aircraft is provided and includes a fuselage, wings extending outwardly from the fuselage to define a wing plane and a prop-rotor operably disposed to generate thrust, a flight computer and controllable surfaces disposed on at least one of the fuselage, the wings and the prop-rotor. The controllable surfaces are controllable by the flight computer to position the wing plane in accordance with a predominant local wind direction.
HOVER ATTITUDE TRIM FOR VEHICLE
2017-04-06
Patent
Electronic Resource
English
Modelling and robust attitude trajectory tracking control of 3-DOF four rotor hover vehicle
Emerald Group Publishing | 2017
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