One-rocket multi-satellite layout method and system based on separation safety design

The invention relates to a one-rocket multi-satellite layout method and system based on separation safety design, and the method comprises the steps: obtaining the orbit injection attitude deviation at a satellite-rocket separation moment, and setting an initial separation state; setting mass center coordinates of M groups of satellites relative to a rocket body and separation energy of the satellites in an initial separation state, and completing population initialization; establishing a fitness function by taking the minimum far-field distance of the two satellites from the half period to the five periods after separation and the sum of the attitude angular velocities of the satellites after separation as optimization indexes; calculating a fitness function value of each particle; updating an individual extreme value and a global extreme value; updating the particle speed and the particle position; and when a preset ending condition is met, outputting a one-rocket multi-satellite layout optimization result.