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We provide the code repository for our paper This repository includes the necessary code to replicate our experiments and utilize our DRL model for spacecraft trajectory planning. By accessing the repository, researchers and practitioners can benefit from our approach to efficiently transfer spacecraft to GEO using low-thrust propulsion systems.
Solve low-thrust interplanetary trajectory optimization problem using Particle Swarm Optimizer. Coded by Matlab. Deflecting Potentially Hazardous Asteroids to maximize the closest-approach distance between the Earth