Health management method and system for general aircraft
A health management system and technology of health management, applied in the field of health management methods and systems of general aircraft
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[0050] Preferred embodiments of the present invention are described below with reference to the accompanying drawings. Those skilled in the art should understand that these embodiments are only used to explain the technical principles of the present invention, and are not intended to limit the protection scope of the present invention. For example
[0051] See attached figure 1 , figure 1 It exemplarily shows the main steps of a health management method for a general-purpose aircraft, such as figure 1 As shown, the health management method for general-purpose aircraft provided in this embodiment mainly includes the following steps:
[0052] Step S101: Obtain preset state parameters of key subsystems of the general-purpose aircraft in real time.
[0053] Specifically, key subsystems may include engine subsystems, flight control subsystems, and so on. State parameters of the engine subsystem may include engine speed, engine exhaust temperature, engine vibration, fuel flow, ...
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