dLITE: Differentiable Lighting-Informed Trajectory Evaluation for On-Orbit Inspection
Jack Naylor, Raghav Mishra, Nicholas H. Barbara, Donald G. Dansereau

TL;DR
This paper introduces $ extbackslash$partialLITE, a novel differentiable simulation pipeline for optimizing spacecraft inspection trajectories in orbit, significantly enhancing data quality through automatic, data-driven planning methods.
Contribution
It presents the first end-to-end differentiable pipeline for on-orbit inspection planning, enabling automatic trajectory optimization based on visual data quality.
Findings
Automated trajectory design improves inspection data quality.
Differentiable simulation enables end-to-end optimization.
Trajectory optimization outperforms traditional planning methods.
Abstract
Visual inspection of space-borne assets is of increasing interest to spacecraft operators looking to plan maintenance, characterise damage, and extend the life of high-value satellites in orbit. The environment of Low Earth Orbit (LEO) presents unique challenges when planning inspection operations that maximise visibility, information, and data quality. Specular reflection of sunlight from spacecraft bodies, self-shadowing, and dynamic lighting in LEO significantly impact the quality of data captured throughout an orbit. This is exacerbated by the relative motion between spacecraft, which introduces variable imaging distances and attitudes during inspection. Planning inspection trajectories with the aide of simulation is a common approach. However, the ability to design and optimise an inspection trajectory specifically to improve the resulting image quality in proximity operations…
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Taxonomy
TopicsSpace Satellite Systems and Control · Spacecraft Dynamics and Control · Spacecraft Design and Technology
