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1. A Rotor Control Assembly for an aerial vehicle capable of vertical takeoff and landing in rotor-wing mode, rotor-wing vertical flight operations, and horizontal flight operations in fixed-wing mode, wherein the aerial vehicle comprises a wing having a wingtip, the rotor control assembly comprising a Power Section having: a lower drive gear; a hollow drive shaft axially mounted to the center of said lower drive gear, said drive shaft rotatably mounted in said wingtip; an electric motor and associated controls to power said drive gear; an electric slip ring operably mounted within said drive shaft to provide power and signal paths to and from electric actuators within a plurality of rotoron blades; an upper guide gear; a hollow guide shaft axially mounted to the center of the guide gear and concentrically mounted onto said drive shaft; an electric motor and associated controls to power said guide gear; a device to latch and hold said drive gear in place; a device to latch and hold said guide gear in place; two spring-loaded coupler locks, wherein each of said spring-loaded coupler locks directly engages with said drive gear and said guide gear to couple said drive gear and said guide gear together as a single unit when operating the rotoron blades as rotors during rotor-wing flight operations and when operating the rotoron blades as extended ailerons during fixed-wing flight operations, and to decouple said drive gear and said guide gears during a process in which said aerial vehicle transitions from a vertical flight configuration to a horizontal flight configuration; an electric actuator for each of said spring-loaded coupler locks; and a gear cover providing protection for said drive gear and said guide gear.
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