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1. 发明申请

US20160202701A1 ABNORMAL AIRCRAFT RESPONSE MONITOR 审中-公开
标题翻译：异常飞机反应监控
公开(公告)号：US20160202701A1
公开(公告)日：2016-07-14
申请号：US14912748
申请日：2014-08-18
申请人： Bombardier Inc.
发明人： Gregory BURTE
IPC分类号： G05D1/00 , B64C13/50
CPC分类号： G05D1/0077 , B64C13/503 , B64C13/505
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.
摘要翻译：飞行器飞行控制系统包括至少两个飞行控制计算机，其中至少一个飞行控制计算机在任何一个时间用于控制飞行器飞行，所述至少两个飞行控制计算机中的每一个具有至少两个处理器，每个处理器响应飞行器输入信号，其指示多个飞行器飞行参数中的至少一个，并响应于控制规律提供指示飞机飞行控制表面的期望控制的控制输出命令信号。此外，用于至少两个飞行控制计算机中的每一个的至少两个处理器中的至少一个包括响应于至少一个飞行器输入信号的异常响应监视器，其指示多个飞行器飞行参数中的至少一个以确定控制输出命令信号是否在可接受的值内。

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