A gimbal configured to be implemented in an unmanned aerial system. The gimbal includes a payload interface; an end effector; a structure that includes composite skins, an internal structure, and integrated seals; integrated drive components; and at least one computer, where excess heat generated by the at least one computer is disposed of through a heat transfer surface integrated into the composite skin of the gimbal.
LIGHTWEIGHT STABILIZED GIMBAL CAMERA PAYLOAD FOR SMALL AERIAL VEHICLES
2022-11-10
Patent
Electronic Resource
English
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