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
LEICHTE STABILISIERTE KARDANISCHE KAMERANUTZLAST FÜR KLEINE LUFTFAHRZEUGE
CHARGE UTILE DE CAMÉRA À CARDAN STABILISÉE LÉGÈRE POUR PETITS VÉHICULES AÉRIENS
2025-03-26
Patent
Electronic Resource
English
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