A method (400) for an airborne payload system (100) includes receiving (410), from a sensor (140) on a payload line (130), information about the payload line (130), wherein the payload line (130) comprises a first end (130a) wound about a main reel (210) of a winch system (120) and a second end (130b) configured to couple to a payload (160). The method further includes providing instructions (420), based on the received information, to the unmanned aircraft (110) and the winch system (120) in order to control a position of the second end (130b) of the payload line (130).
AIRBORNE PAYLOAD CONTROL SYSTEM
LUFTGESTÜTZTES NUTZLASTSTEUERUNGSSYSTEM
SYSTÈME DE COMMANDE DE CHARGE UTILE EMBARQUÉE
2021-01-27
Patent
Elektronische Ressource
Englisch