The control method of a simulated flight support automation system according to the present invention comprises: (a) a first operating mode step of entering a simulated flight mode for preparing for launch, based on input of external power through an integrated electronic device; (b) a second operating mode step of acquiring and displaying a telemetry message based on a launch command being granted via a simulated flight simulator computer; (c) a third operating mode step of automatically storing the obtained telemetry message in a file form based on arrival of the flight time at the scheduled flight time; and (d) a fourth operating mode step of waiting until the external power is again input through the integrated electronic device, based on the external power being inputted through the integrated electronic device being cut off.
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