A control system for a component of a rescue hoist (210) attached to an aircraft is disclosed. In various embodiments, the control system includes a first bus (270) extending between a control module (252) of the rescue hoist and a control input device (254); a second bus (272) extending between the control module of the rescue hoist and the control input device; and a hardwire extending between the control module of the rescue hoist and the control input device.
DUAL BUS AND HARDWIRE ARCHITECTURE FOR HIGH RELIABILITY CONTROL OF HELICOPTER HOIST
DOPPELBUS- UND KABELVERBINDUNGSARCHITEKTUR ZUR HOCHZUVERLÄSSIGEN STEUERUNG EINES HUBSCHRAUBERZUGS
ARCHITECTURE DE CÂBLAGE ET DE BUS DOUBLE POUR COMMANDE DE TREUIL D'HÉLICOPTÈRE DE HAUTE FIABILITÉ
2025-04-02
Patent
Electronic Resource
English
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