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

Fuente: arXiv

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Detalles Bibliográficos
Autores principales:	Rallapalli, Aditya, Kumar, Suraj, P, Rijesh M, Kakula, Ashok Kumar, GVP, Bharat Kumar
Formato:	Preprint
Publicado:	2026
Materias:	Systems and Control Robotics
Acceso en línea:	Acceder al recurso
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!

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