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    • 73. 发明公开
    • Aircraft control apparatus and aircraft control system
    • Flugzeugsteuerungsvorrichtung und Flugzeugsteuerungssystem
    • EP2595023A3
    • 2015-03-18
    • EP12192728.9
    • 2012-11-15
    • Nabtesco CorporationBAE Systems Controls Inc.
    • Fukui, AtsushiMori, AtsushiBessette, StevenEllsworth, GaryGianisis, Dino
    • G05D1/00B64C13/50
    • G06F17/00B64C13/503G05D1/0077
    • A plurality of control channels each include a power supply, an interface that receives a manipulation signal, an arithmetic processing portion that calculates and generates an operation command signal for actuators based on the manipulation signal, and a signal determination unit that determines a control signal for finally controlling the operation of the actuators and outputs the control signal. The arithmetic processing portions respectively provided in the plurality of control channels have designs different from one another. Each of the signal determination units determines the control signal by receiving a first operation command signal generated by the arithmetic processing portion of the control channel in which that signal determination unit is provided, and a second operation command signal generated in the arithmetic processing portion of another of the control channels, and comparing the first operation command signal and the second operation command signal, and outputs the control signal.
    • 多个控制通道各自包括电源,接收操作信号的接口,运算处理部分,其基于操作信号计算并产生用于致动器的操作命令信号;以及信号确定单元,其确定用于 最后控制执行器的运行并输出控制信号。 分别设置在多个控制通道中的算术处理部分具有彼此不同的设计。 每个信号确定单元通过接收由其中提供该信号确定单元的控制信道的运算处理部分产生的第一操作命令信号和在另一个的算术处理部分中生成的第二操作命令信号来确定控制信号 并且比较第一操作命令信号和第二操作命令信号,并输出控制信号。
    • 74. 发明授权
    • Ground fault detection system and method
    • 接地故障检测系统和方法
    • EP1336528B1
    • 2015-01-28
    • EP03003775.8
    • 2003-02-19
    • BAE Systems Controls Inc.
    • Roden, Garey GeorgeCarruthers, Peter Alexander
    • B60L3/00
    • G01R31/025B60L3/0061B60L3/0069B60L3/04B60L2200/26B60W10/08B60W20/00
    • An AC ground fault detector system for sensing an AC signal indicative of an unintended electrical path between a load driven by a power source and a reference potential comprises a first power conductor coupled to a first terminal of the power source and a second power conductor coupled to a second terminal of the power source. A switching mechanism coupled to the first and second power conductors is operative for alternately connecting a phase of the load with the first and second power conductors according to a predetermined switching rate, whereby, during normal operation, voltages developed at the first power conductor and second power conductor are substantially constant with respect to a reference potential. In the event of an occurrence of the unintended electrical path of at least one phase of the load with the reference potential, time varying voltages are developed at the first power conductor and second power conductor associated with the switching rate. A detector is coupled at an input port to the first power conductor for receiving the voltage or current signal on the first power conductor. The detector includes a processing circuit for processing the received signal and comparing with a threshold value, and an output port for generating an output signal based on said comparison; whereby the occurrence of the unintended electrical path between the load and reference potential causes a change in the voltage or current signal on the first power conductor of sufficient magnitude relative to the threshold value for detection by the detector such that the output signal of the detector is indicative of a detected fault.