Conceptual

Compositional Diffusion Models for Spacecraft Powered-Descent Trajectory Generation

A generative approach to spacecraft trajectory design that models the space of feasible 6-degree-of-freedom powered-descent trajectories as a probability density learned by a diffusion model, then composes separate densities for distinct constraints and design specifications. Composition lets the model adapt to new, out-of-distribution problem variations in a few-shot manner and produce dynamically feasible initial guesses for downstream guidance, including inference-time minimum-fuel landing-site selection.