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
2020-12-10
Patent
Electronic Resource
English
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