Asynchronous, triple redundant primary flight computers (PFC's) (12, 14, 16) produce output command signals carried over a data bus (18) to control redundant actuators (32, 34, 36) in an aircraft flight control system. To prevent the transmission of a fault and a force fight among the redundant actuators,...http://www.google.es/patents/US5515282?utm_source=gb-gplus-sharePatente US5515282 - Method and apparatus for implementing a databus voter to select flight command signals from one of several redundant asynchronous digital primary flight computers
Method and apparatus for implementing a databus voter to select flight ...
