CPC G08G 5/0034 (2013.01) [B64C 25/10 (2013.01); B64C 25/32 (2013.01); B64C 39/024 (2013.01); G08G 5/0069 (2013.01); B64C 2025/325 (2013.01); B64U 10/10 (2023.01); B64U 30/20 (2023.01); B64U 50/13 (2023.01); B64U 50/19 (2023.01); B64U 2101/00 (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;
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; and
a payload rail coupled with and extending along the fuselage, the payload rail allowing mechanical connection of a plurality of payloads to the fuselage, the payload rail allowing positioning of the plurality of payloads connected to the payload rail such that a center of gravity of the plurality of payloads is able to be aligned with the axis of rotation of the main rotor.
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