A redundant ECU controller for aero-engine and its control method
An aero-engine and controller technology, applied in the direction of engine control, machine/engine, mechanical equipment, etc., can solve the problems of engine failure, ECU control failure, low reliability of the controller, etc., to achieve precise control and ensure safety.
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[0028] The present invention will be described in detail below according to the accompanying drawings, which is a preferred embodiment among various implementations of the present invention.
[0029] In a preferred embodiment, a controller with an engine redundant ECU circuit structure is realized by designing redundant input circuits, redundant output circuits, and redundant CPUs of the controller. When one ECU is working normally, the other ECU is in the hot backup state. When the ECU believes that the input signal of a certain channel is unreliable, it can switch to the input signal from another channel; when a certain channel load or drive circuit failure is diagnosed , can be switched to drive the load from another channel; when a CPU fails or is untrustworthy, it can be switched to another CPU to control the engine; therefore, this ECU redundant circuit structure improves the reliability of the controller. The main design idea of the controller is as follows:
[0030]...
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