The invention provides a
satellite tracking method, which relates to the field of electromagnetic wave
beam tracking, and is used for realizing the rapid tracking and pointing of satellites. The method comprises the steps that the
directivity factor function of the antenna is obtained; the Jacobi matrix of the
directivity factor function which is used for determining the angle compensation direction of the antenna is obtained; the angle of
deviation matrix of the antenna, relative to the
satellite can be obtained through scanning, and the angle of
deviation matrix is used for providing a
function model to obtain the compensation angle; the compensation angle is obtained based on the
directivity factor function, the angle of
deviation matrix, and the Jacobi matrix, and the compensation angle is used for guiding the antenna to move at the next time; the compensation angle can be dynamically obtained during the aligning process, the antenna is continuously adjusted based on the compensation angle to scan, track and align the
satellite. The invention is advantageous in that the
satellite tracking errors can be rapidly converged through collecting wave beam signals having quite a few orquite
low frequency, and the satellite aligning with high precision can be realized.