CPC B64C 27/26 (2013.01) [B64C 29/02 (2013.01); B64C 39/02 (2013.01); B64C 39/024 (2013.01); B64D 27/06 (2013.01); B64U 30/10 (2023.01); B64U 30/20 (2023.01); B64U 50/13 (2023.01); B64U 70/80 (2023.01)] | 20 Claims |
1. A vertical takeoff and landing (VTOL) aircraft comprising:
a top port motor, a bottom port motor, a top starboard motor, and a bottom starboard motor, wherein the top and bottom starboard motors are angled away from each other within a first plane generally perpendicular to a plane of a wing, and wherein the top and bottom port motors are angled away from each other within a second plane generally perpendicular to the plane of the wing; and
a processor having addressable memory, the processor configured to:
control thrust to each of the top port motor, the bottom port motor, the top starboard motor, and the bottom starboard motor.
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