arXiv · 2605.29412
Real-Time Retargeting Using Controllability Boundary for Chandrayaan-3 Lunar Landing
Abstract
This paper presents the real-time retargeting guidance policy developed for the Chandrayaan-3 lunar landing mission. The baseline guidance generates approximate fuel-optimal descent trajectories, while a high-level policy enables safe retargeting to alternate sites when the nominal site becomes infeasible. The retargeting strategy leverages a convex representation of the controllability boundary, allowing rapid feasibility checks and real-time target updates. To the best of the authors knowledge, this represents the first application of a data-driven retargeting framework in an operational lunar landing mission. Pre-flight simulations and Chandrayaan-3 flight results validate the effectiveness of the proposed approach.
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Suraj Kumar, Debjyoti Chakrabarti, Aditya Rallapalli, Bharat Kumar GVP, Ashok Kumar Kakula. 2026-05-28. Real-Time Retargeting Using Controllability Boundary for Chandrayaan-3 Lunar Landing. https://arxiv.org/abs/2605.29412
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