Decoupled Thrust-Axis Attitude Control Using Quaternions for Chandrayaan-3 Lunar Landing Mission

Fuente: arXiv
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Bibliographic Details
Main Authors: Rallapalli, Aditya, Kumar, Suraj, P, Rijesh M, Kakula, Ashok Kumar, GVP, Bharat Kumar
Format: Preprint
Published: 2026
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