Engine failure treating method for unmanned aerial vehicle
A fault handling method and engine technology, which is applied to aircraft landers, electrical program control, etc., can solve problems such as poor autonomous control capabilities, unmanned aerial vehicles cannot troubleshoot, and fatal engine failures, etc., to achieve fast response, high success rate, The effect of high reliability
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[0032] In order to solve the problem that the UAV aircraft engine is stopped in the air, out of control and unable to stop for protection, the UAV engine failure processing method of the present invention includes a control computer system with data acquisition and signal processing, and in the control computer Configure system fault automatic diagnosis module and fault handling logic program module. The program module used for engine speed monitoring and UAV emergency recovery by using functional devices such as parachute control and buffer airbag / bracket is based on the engine fault automatic diagnosis and fault handling control logic program module of the control computer system. It mainly includes:
[0033] (1) "Signal Acquisition Program Module" for extracting engine speed sensor signal (including: components such as "Optical Interval", "A / D Acquisition", "Event Manager Capture");
[0034] (2) Real-time monitoring of ignition device voltage and frequency program modules ...
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