This invention discloses a method for generating and evaluating Doppler
simulation data for low-Earth
orbit (LEO) satellites. By employing source-end discrete-
time gating, the
system is forced to directly block output when the
time deviation exceeds 1 ms, fundamentally severing the error
coupling path and ensuring the purity of the output data. In the inertial frame velocity synthesis, an explicit Earth rotation-related velocity correction term is introduced, enabling even stationary receivers to accurately reflect their motion in inertial space. An elevation-angle-weighted
noise model is used to accurately simulate the physical phenomenon of sharp link deterioration in LEO satellites at low elevation angles, realistically reflecting the tracking and loss-of-lock behavior of receivers in complex geometric environments. Terminal physical consistency
verification is introduced. By comparing the distance change rate calculated in the velocity domain with the distance rate of the
position domain derivative in real time, a rigorous closed-loop feedback mechanism is constructed, which can automatically identify and eliminate abnormal data caused by
ephemeris jumps or numerical divergences, significantly improving the
engineering confidence of the
simulation data.