arxiv
PublishedMay 29, 2026 at 4:00 AM
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Real-Time Retargeting Using Controllability Boundary for Chandrayaan-3 Lunar Landing
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arXiv:2605.29412v1 Announce Type: cross 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
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Originally published on arxiv ↗