Research on Trajectory Optimization System of Thrust Orbit Transfer Based on Computer Artificial Intelligence

A Gaussian pseudo-spectral method is used to solve an optimal orbital transition problem with a certain force. Firstly, based on the banal perturbation model of the quasi-equinox trajectory element, the objective is to minimize the energy, take the acceleration of a three-part finite thrust engine as the target, and take the acceleration of a three-part finite thrust engine as the target. The multiphase optimization problem is studied by Gaussian pseudospectra method. A new multi-NLP problem based on Gaussian pseudo-spectrum method is proposed and converted into a continuous NLP problem. By comparing with classical homotropy method, the efficiency of the proposed algorithm is proved.