Reinforcement Learning for Low-Thrust Trajectory Design of Interplanetary Missions
Alessandro Zavoli, Lorenzo Federici

TL;DR
This paper explores using reinforcement learning, specifically Proximal Policy Optimization, to design robust low-thrust interplanetary trajectories that can handle various disturbances and uncertainties, demonstrated through Earth-Mars mission simulations.
Contribution
It introduces a reinforcement learning framework for robust trajectory design, integrating disturbances and uncertainties into the control policy for interplanetary missions.
Findings
The RL-based guidance law closely matches deterministic optimal solutions.
The approach demonstrates robustness against disturbances in Monte Carlo simulations.
Preliminary results suggest RL can effectively handle uncertainties in space trajectory planning.
Abstract
This paper investigates the use of Reinforcement Learning for the robust design of low-thrust interplanetary trajectories in presence of severe disturbances, modeled alternatively as Gaussian additive process noise, observation noise, control actuation errors on thrust magnitude and direction, and possibly multiple missed thrust events. The optimal control problem is recast as a time-discrete Markov Decision Process to comply with the standard formulation of reinforcement learning. An open-source implementation of the state-of-the-art algorithm Proximal Policy Optimization is adopted to carry out the training process of a deep neural network, used to map the spacecraft (observed) states to the optimal control policy. The resulting Guidance and Control Network provides both a robust nominal trajectory and the associated closed-loop guidance law. Numerical results are presented for a…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Space Satellite Systems and Control · Astro and Planetary Science
MethodsProximal Policy Optimization
