An aircraft power generation control device
A technology for power generation control and aircraft, which is applied in the fuel control of turbine/propulsion device, charging system, engine components, etc. It can solve the problem of reducing the control accuracy of the system, unable to automatically correct the PID controller, and difficult to meet the high control accuracy of aircraft. requirements, etc., to achieve the effect of strong adaptive ability and good dynamic and static characteristics
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[0021] In order to better understand the present invention, the present invention will be described in more detail below in conjunction with the accompanying drawings and specific embodiments. In the following description, when detailed descriptions of existing prior art may obscure the subject matter of the present invention, such descriptions will be omitted here.
[0022] figure 1 It is a structural block diagram of a specific embodiment of the aircraft power generation control device of the present invention
[0023] In this example, if figure 1 As shown, the aircraft power generation control device includes an input module 1, an output module 2, and a core processing module 3. The input module 1 sends the collected operating parameters of the aircraft generator set to the core processing module 3, and the core processing module 3 according to The operating parameters output the control quantity to the corresponding actuator to perform the corresponding operation.
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