Construction method of aero-engine control model and prediction method of dynamic parameters

The invention relates to an aero-engine control model construction method and a dynamic parameter prediction method. The construction method of the aero-engine control model comprises the steps of obtaining training sample data of a to-be-constructed control model; the to-be-constructed control model comprises a to-be-constructed steady-state model, a to-be-constructed dynamic characteristic model, a to-be-constructed transfer function and a to-be-constructed reverse normalization model; respectively training a to-be-constructed steady-state model, a to-be-constructed dynamic feature model and a to-be-constructed anti-normalization model by utilizing the training sample data to obtain a steady-state model, a dynamic feature model and an anti-normalization model; constructing a to-be-constructed transfer function by using the steady-state model and the dynamic characteristic model to obtain the transfer function; and constructing an aero-engine control model based on the steady-state model, the dynamic charact