The invention discloses an optimization design method of a
skin conformal antenna under fatigue reliability constraint. The method comprises the following steps: firstly, analyzing a
skin conformal antenna structure and a
service load thereof, identifying a main failure mode of the
skin conformal antenna structure, representing and quantifying multi-source uncertainty such as a service environment, a
composite material layering structure and material performance, establishing a performance
simulation analysis model under multi-
physics field
coupling, and simulating performance response of the model under the action of multi-
physics field
coupling; the method comprises the following steps: firstly, simulating a skin conformal antenna, then, constructing a
performance prediction model based on
deep learning on the basis of a
simulation result, then, establishing a skin conformal antenna integrated optimization design model under fatigue reliability constraint, finally, solving an
optimal design variable by utilizing an intelligent optimization
algorithm, and carrying out multi-
physics field performance analysis on an optimized structure to verify an optimization effect. According to the method, key
technical support is provided for aircraft design optimization and
collaborative design of an electromagnetic and
structural system, and reliable operation and high performance of the aircraft under complex working conditions can be ensured.