发明名称 ABNORMAL AIRCRAFT RESPONSE MONITOR
摘要 An aircraft flight control system includes at least two flight control computers at least one of which is utilized at any one time to control aircraft flight, each of the at least two flight control computers having at least two processors, each processor being responsive to an aircraft input signal indicative of at least one of a plurality of aircraft flight parameters and being responsive to control laws to provide a control output command signal indicative of a desired control of an aircraft flight control surface. Also, at least one of the at least two processors for each of the at least two flight control computers comprises an abnormal response monitor that is responsive to at least one aircraft input signal indicative of at least one of a plurality of aircraft flight parameters to determine whether the control output command signal is within an acceptable value.
申请公布号 US2016202701(A1) 申请公布日期 2016.07.14
申请号 US201414912748 申请日期 2014.08.18
申请人 Bombardier Inc. 发明人 BURTE Gregory
分类号 G05D1/00;B64C13/50 主分类号 G05D1/00
代理机构 代理人
主权项 1. A flight control system for an aircraft, comprising: at least two flight control computers at least one of which is utilized at any one time to control flight of the aircraft, each of the at least two flight control computers having at least two processors, each of the at least two processors being responsive to an aircraft input signal indicative of at least one of a plurality of aircraft flight parameters and being responsive to control laws to provide a control output command signal indicative of a desired control of a flight control surface of an aircraft; and wherein at least one of the at least two processors for each of the at least two flight control computers comprises an abnormal response monitor that is responsive to the aircraft input signal indicative of at least one of a plurality of aircraft flight parameters to determine whether the control output command signal is within an acceptable value.
地址 Dorval CA