| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide an aircraft control apparatus for which the redundancy that allows the operation of a device installed in an aircraft to be safely continued can be ensured and whose configuration can be simplified with a reduced number of arithmetic processing portions. <P>SOLUTION: A plurality of control channels 13 each include a power supply 14, an interface 16 that receives a manipulation signal, an arithmetic processing portion 17 that calculates and generates an operation command signal for actuators based on the manipulation signal, and a signal determination unit 18 that determines a control signal for finally controlling the operation of the actuators and outputs the control signal. The arithmetic processing portions 17 respectively provided in the plurality of control channels 13 have designs different from one another. Each of the signal determination units 18 determines the control signal by receiving a first operation command signal generated by the arithmetic processing portion 17 of the control channel 13 in which that signal determination unit 18 is provided, and a second operation command signal generated in the arithmetic processing portion 17 of another of the control channels 13, and comparing the first operation command signal and the second operation command signal, and outputs the control signal. <P>COPYRIGHT: (C)2013,JPO&INPIT |
