Sign inGet started
Paper · arXiv

Saturation-Aware Robust Trajectory Optimization for Reusable Launch Vehicles via Differentiable Physics

The high-angle-of-attack flip maneuver of reusable launch vehicles presents significant challenges for robust trajectory optimization due to the combined effects of highly nonlinear dynamics, aerodynamic uncertainties, and actuator saturation. This paper presents a differentiable physics framework for saturation-aware robust trajectory optimization. At its core, a Differentiable Particle Tube Control (DPTC) scheme is developed to optimize uncertainty evolution through an ensemble-based distribution shaping strategy. State uncertainty is represented by a Lagrangian particle ensemble, while hard actuator projection operators are embedded directly into the computational graph, enabling the j...

AuthorsLiwei Chen, Tong Qin
Primary categorycs.RO
Published2 July 2026
Last updated at source2 July 2026
cs.ROcs.LGphysics.app-ph
Embed this entry
<iframe src="https://silytics.si/embed/item/71d5c2fd-9b6d-4f5b-ad83-0096c88a7ba1" width="420" height="190" style="border:0" loading="lazy" title="Silytics entry"></iframe>

Free, no tracking. More about feeds and embeds.

Silytics shows public metadata from arXiv and links to the original. Information may be incomplete or out of date. Last refreshed 17 October 2026. Licenses and terms of the original apply to the work itself. Not financial, legal or professional advice.