A vertical takeoff and landing aircraft capable of six degree-of-freedom motion where lift, pitch, and roll are provided by multirotors oriented vertically, lateral translation is provided by a cyclorotor oriented vertically, and yaw is provided by a combination of the cyclorotor and the multirotors. The invention includes a frame, which supports the multirotors and cyclorotors. The frame also supports a payload and battery which are positioned at the extreme ends of the frame. The aircraft is capable of hovering precisely to position a payload close to or touching a target surface in the air.
Multirotor Vertical Takeoff And Landing Aircraft With Cyclorotor For Lateral Control
17.02.2022
Patent
Elektronische Ressource
Englisch
Multirotor vertical takeoff and landing aircraft with cyclorotor for lateral control
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