A control system for a component of a rescue hoist attached to an aircraft is disclosed. In various embodiments, the control system includes a first bus extending between a control module of the rescue hoist and a control input device; a second bus 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
03.01.2023
Patent
Elektronische Ressource
Englisch
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