The invention discloses a different-
orbit inter-
satellite communication link beam
pointing error calculation method, which relates to the technical field of communication, introduces high-order perturbation modeling, solar
radiation pressure, earth tidal effect and moon gravitational perturbation items, effectively simulates
orbit change of a
satellite disturbed by external
gravitational force for a long time, reduces the accumulation effect of errors, and improves the accuracy of beam
pointing error calculation. In long-time or high-
orbit satellite communication, pointing errors caused by simplified perturbation can be effectively reduced,
relative motion models of two different-orbit satellites are combined, orbit change of a single satellite is integrated, change of relative speed is taken into calculation, wave beam pointing can be dynamically adjusted when the relative position and the speed of the satellites change, and the method is suitable for large-scale popularization and application. Errors caused by relative movement are reduced, meanwhile, a
coupling model of
frequency deviation and beam pointing angle deviation is constructed, the influence of the
Doppler effect on beam pointing is predicted and corrected in real time, the beam pointing is dynamically adjusted through
coupling correction, communication signals are kept on the optimal transmission path, and
frequency deviation is avoided.