Method and device for integrating multiple upper computers in aeroengine control system
An aero-engine and control system technology, applied in geometric CAD, design optimization/simulation, special data processing applications, etc., can solve the problems of confusion of the upper computer, different versions, and increased labor maintenance costs, so as to solve the problem of confusion in use and avoid The effect of controlling risk
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[0043] Specific embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings. It should be understood that the specific embodiments described here are only used to illustrate and explain the present invention, and are not intended to limit the present invention.
[0044] As a first aspect of the present invention, a method for integrating various upper computers in an aeroengine control system is provided, wherein, such as figure 1 As shown, the aero-engine control system includes a control device and various host computers connected to the control device, each of which is used to send control commands to the control device, and the control commands sent by the various host computers are different from each other. Similarly, each host computer includes configuration information, and the integration method includes:
[0045] S110. Obtain the configuration information of each upper computer, and form the configuration info...
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