Loading method of C-PML boundary conditions during time-domain airborne electromagnetic numerical simulation
A technology of aeronautical electromagnetic and numerical simulation, applied in the direction of electrical digital data processing, special data processing applications, instruments, etc., can solve problems that do not involve processing methods, reduce calculation time, etc.
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[0067] see figure 1 , a method for loading C-PML boundary conditions in time-domain airborne electromagnetic numerical simulation, including:
[0068] 1), using the divergence equation As the governing equation of the vertical component of the magnetic field, under quasi-static conditions, the passive Maxwell curl equation is used as the governing equation of other electromagnetic field components. Combined with non-uniform Yee grid and DuFort-Frankel method to construct an explicit difference scheme, the number of grids is 107× 107×53, the number of grids in the x and y directions is 107, the number of grids in the z direction is 53, the minimum and maximum grid steps are 10m and 120m respectively, and the other 5 sides of the calculation area are the outermost Layer 8 meshes loaded with C-PML layers.
[0069] 2) Set parameters such as conductivity, magnetic permeability, and C-PML coefficient in the entire calculation area. The model in the calculation example is a unifor...
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