Gradient-Informed Monte Carlo Fine-Tuning of Diffusion Models for Low-Thrust Trajectory Design
Jannik Graebner, Ryne Beeson

TL;DR
This paper introduces a gradient-informed Monte Carlo fine-tuning approach for diffusion models to efficiently explore low-thrust spacecraft trajectories, improving convergence and solution diversity in complex mission design landscapes.
Contribution
It extends diffusion model fine-tuning with gradient-informed MCMC methods, notably MALA, to enhance sampling efficiency and solution quality in low-thrust trajectory optimization.
Findings
Gradient-informed MCMC accelerates chain mixing and convergence.
MALA outperforms other algorithms in feasibility and diversity.
Fine-tuning diffusion models reduces the need for extensive data generation.
Abstract
Preliminary mission design of low-thrust spacecraft trajectories in the Circular Restricted Three-Body Problem is a global search characterized by a complex objective landscape and numerous local minima. Formulating the problem as sampling from an unnormalized distribution supported on neighborhoods of locally optimal solutions, provides the opportunity to deploy Markov chain Monte Carlo methods and generative machine learning. In this work, we extend our previous self-supervised diffusion model fine-tuning framework to employ gradient-informed Markov chain Monte Carlo. We compare two algorithms - the Metropolis-Adjusted Langevin Algorithm and Hamiltonian Monte Carlo - both initialized from a distribution learned by a diffusion model. Derivatives of an objective function that balances fuel consumption, time of flight and constraint violations are computed analytically using state…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Space Satellite Systems and Control · Gas Dynamics and Kinetic Theory
