CPC G08G 5/0034 (2013.01) [B64C 25/10 (2013.01); B64C 25/32 (2013.01); B64U 50/19 (2023.01); B64U 60/40 (2023.01); B64U 60/50 (2023.01); G08G 5/0069 (2013.01); B64C 2025/325 (2013.01); B64U 10/17 (2023.01); B64U 30/40 (2023.01); B64U 2101/30 (2023.01); B64U 2101/64 (2023.01); B64U 2201/10 (2023.01)] | 20 Claims |
1. An unmanned helicopter platform comprising:
a fuselage housing flight control electronics;
a tail coupled with the fuselage, the tail including a tail rotor and a tail rotor motor, wherein the tail is removably coupled to the fuselage, wherein the fuselage includes a fuselage coupling section and the tail includes a tail coupling section configured to mate with the fuselage coupling section, the tail coupling section and the fuselage coupling section providing a mechanical connection, a data connection and a power connection between the fuselage and the tail; and
a main rotor assembly coupled with the fuselage and the flight control electronics, the main rotor assembly including a main rotor having an axis of rotation and a main rotor motor.
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