Flight control system sensor hybrid redundancy method based on analytic reconstructed signal
A technology for reconstructing signals and flight control systems, applied in the field of aircraft control, can solve the problems of increasing the take-off weight of the aircraft and the development cost, so as to reduce the hardware redundancy configuration, improve the redundancy level, improve the redundancy level and fault/work horizontal effect
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[0038] The present invention will be described in further detail below with reference to the drawings and embodiments.
[0039] The present invention provides a sensor hybrid redundancy method of a flight control system based on analytically reconstructed signals, such as figure 2 with image 3 As shown, when the sensor system has no fault sensors, the monitoring voting system (including the comparator and the voting device) directly outputs the sensor status and voting results; for the triple redundancy sensor system, when a sensor failure occurs, the monitoring voting system can achieve Sensor fault isolation. When the triple redundancy sensor has a secondary fault, the voting result of the monitoring voting system is 1:1. At this time, the fault sensor cannot be identified only by the original monitoring voting system. Therefore, the mixed redundancy provided by the present invention is adopted. The method uses analytical reconstruction signals to form a three-redundancy syste...
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