Vertical take=off and landing aircraft

摘要

The aircraft has no movable parts for steering the aircraft in two directions, the pilot controlling the aircraft in these directions using body-weight control. The aircraft fuselage has an initial vertical position with movement into an approximately horizontal position as the speed increases, additional motors reducing the swaying caused by the contra-rotating propellers. High energy batteries can be used to power electric drives for intermittent ON/OFF switching of each propeller driven by two motors with different power outputs.