经对某航空发动机电子综合调节器燃油通道动态过程参数模型辨识的实例，验证了该算法精确快速。
Through the analysis of a system identification example of X aero-engine EEC (engine electronic controller) , the result shows this.
如果空气渗入通道堵塞时，在发动机熄火后，会导致浮子室中的燃油流。
If air-bleed passages become plugged, they may cause the float bowl to be emptied after the engine shuts off.
由于需要采集多个柴油机的燃油消耗参数，在硬件设计中采用模拟开关对采集通道进行切换。
Furthermore, the selection of the fuel consumption sensor, the frequency collection circuit, the simulation processing circuit, A/D transmitter, memory circuit, SCM, etc was introduced.
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