The invention provides an inter-
satellite link
configuration optimization design method based on an NSGA-II
algorithm, and belongs to the technical field of inter-
satellite links of
satellite navigation systems. The method comprises the following steps: determining the number N of decision variables influencing the inter-satellite link configuration; initializing a
population, constraining the initialized
population, and establishing an inter-satellite link; according to a designed inter-satellite link configuration, a multi-objective optimization function is constructed by taking an inter-satellite link configuration weighted average WAPDOP, a total communication routing number TCR and variances VTHL of all satellite hardware loads as optimization objectives; and optimizing the inter-satellite
link design configuration according to the multi-objective optimization function. According to the method, the performance of the inter-satellite
link design configuration is evaluated by constructing the inter-satellite link network type observation structure, the
load capacity and the communication efficiency condition model, and the performance of the
system is effectively improved, so that the autonomous navigation task is better completed, and the problem that the existing inter-satellite link configuration of the Beidou
system cannot be optimal is solved.