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eess.SY2026
Real-Time Retargeting Using Controllability Boundary for Chandrayaan-3 Lunar Landing
Suraj Kumar, Debjyoti Chakrabarti, Aditya Rallapalli +2
This paper presents the real-time retargeting guidance policy developed for the Chandrayaan-3 lunar landing mission. The baseline guidance generates approximate fuel-optimal descen…
eess.SY2026
Decoupled Thrust-Axis Attitude Control Using Quaternions for Chandrayaan-3 Lunar Landing Mission
Aditya Rallapalli, Suraj Kumar, Rijesh M P +2
Chandrayaan-3 mission achieved a historic milestone with its successful soft landing near the lunar south pole, highlighting the critical role of the navigation, guidance, and cont…