Autonomous Guidance for Cislunar Orbit Transfers via Reinforcement Learning

This paper investigates the use of reinforcement learning for the optimal guidance of a spacecraft during a time-free low-thrust transfer between two libration point orbits in the cislunar environment. To this aim, a deep neural network is trained via Proximal Policy Optimization to map any spacecraft state to the optimal control action. A general-purpose reward is used to guide the network toward a fuel-optimal control law regardless of the specific orbits considered, and without the use of any ad-hoc reward shaping technique. Eventually, the learned control policies are compared with the optimal solutions provided by a direct method in two different mission scenarios, and Monte Carlo simulations are used to assess the policies robustness to navigation uncertainties