The invention discloses a
time domain integral equation method for analyzing the electromagnetic scattering characteristic of a hypersonic flight object. The
time domain integral equation method comprises that a
time domain volume-surface integral equation is established; according to the structural scattering characteristic, the total
electric field on the stimulated object is equal to the sum of an incident
electric field and a scattered
electric field, and the incident electric field is stimulated; the integral equation is discretized, tests in space and time are carried out, and a time domain matrix equation is established; the relationship between the
dielectric flux density and the electric
field intensity of
plasma is established; and the time domain matrix equation is solved, and the electromagnetic scattering characteristic of a mixed object in
broadband is analyzed. According to the invention, only the
object model needs to be discretized, by means of a
free space green function and a
recursive convolution method, a mixed object containing heterogeneous
plasma medium and
metal can be analyzed, the calculating precision is high, and the number of unknowns is relatively small; at the same time, a time domain method is employed for solution, the electromagnetic scattering characteristic of each frequency point in
broadband can be calculated for one step, compared with a
frequency domain method that frequency sweep operation is needed, the time domain integral equation method is advantaged in that the solving time is reduced.