Patent attributes
An aircraft capable of vertical takeoff and landing (VTOL) including one or more propulsion systems gyroscopically mounted (i.e. rotatable about x- and y-axes) to a rigid airframe is disclosed. Each “wing” includes a propulsion system mounted to an axle that is rotatably attached to a wing mount, which in turn is pivotably mounted to the exterior of the airframe. The propulsion systems are electronically grouped according to their position relative to the airframe, such that one controller can control all the propulsion systems on the right or left side of the aircraft, resulting in control logic that is far more intuitive and convenient than that taught in the prior art. A method of operating an aircraft utilizing this improved control logic is also disclosed.
