Trajectory of flybys of multiple irregular satellites of Jupiter with Galilean moon gravity assist using beam search

Using the algorithms and programs involved in the paper, the touring orbits of multiple irregular Jovian satellites are optimized to obtain trajectory information. The program runs in a Matlab environment and the data is opened using Matlab. The data includes the optimal trajectories corresponding to different initial orbit periods, and the impact of different proportions of branches retained at each level on the results.