Diffusion Policies for Generative Modeling of Spacecraft Trajectories
Julia Briden, Breanna Johnson, Richard Linares, Abhishek Cauligi
TL;DR
This paper tackles online, constraint-aware trajectory generation for spacecraft, focusing on 6-DoF powered descent. It introduces a compositional diffusion framework that can sample and plan trajectories while integrating diverse constraints and priors at inference time, including multi-landing-site risk maps, via energy-based diffusion and inpainting. The authors train a 6-DoF diffusion model from SCvx-derived data, then demonstrate flexible constraint enforcement through glideslope negation composition, state/control conditioning, and multi-landing-site sampling, achieving feasible trajectories faster and with lower constraint violations than unconstrained baselines. The approach offers a practical, modular toolkit for autonomous space missions, enabling efficient initial guesses and constraint-compliant planning without retraining for each new specification.
Abstract
Machine learning has demonstrated remarkable promise for solving the trajectory generation problem and in paving the way for online use of trajectory optimization for resource-constrained spacecraft. However, a key shortcoming in current machine learning-based methods for trajectory generation is that they require large datasets and even small changes to the original trajectory design requirements necessitate retraining new models to learn the parameter-to-solution mapping. In this work, we leverage compositional diffusion modeling to efficiently adapt out-of-distribution data and problem variations in a few-shot framework for 6 degree-of-freedom (DoF) powered descent trajectory generation. Unlike traditional deep learning methods that can only learn the underlying structure of one specific trajectory optimization problem, diffusion models are a powerful generative modeling framework that represents the solution as a probability density function (PDF) and this allows for the composition of PDFs encompassing a variety of trajectory design specifications and constraints. We demonstrate the capability of compositional diffusion models for inference-time 6 DoF minimum-fuel landing site selection and composable constraint representations. Using these samples as initial guesses for 6 DoF powered descent guidance enables dynamically feasible and computationally efficient trajectory generation.
