The invention relates to the technical field of
optical imaging, in particular to an aerodynamic
optical aberration calculation method, which comprises the following steps of: firstly, dividing an external flow field for an aircraft model carrying an
optical imaging system, and setting a speed variable condition, a plurality of
flight height sampling points and a corresponding state boundary condition of the aircraft model; according to the Reynolds number and the
viscosity interference parameter under each state boundary condition, dividing the
flight height sampling points into two types of calculation aberration and prediction aberration; for a predicted aberration sampling point, randomly selecting one as a reference point, calculating the pneumatic
optical aberration of the predicted aberration sampling point, and predicting the pneumatic optical aberrations of other predicted sampling points based on the pneumatic
optical aberration of the reference point; for aberration calculation sampling points, the corresponding pneumatic optical aberration is solved by directly calculating external flow field
density distribution and conversion
refractive index distribution of the aberration calculation sampling points. According to the invention, through one-time pneumatic optical transmission aberration calculation, different flight heights are expanded, and the demand for large-scale calculation resources and the time required for evaluation are significantly reduced.