Momentum Space Analysis for Mixed Skew Angle Arrays

This report explores non-redundant constant-speed single-gimballed control moment gyroscope mechanics for spacecraft maneuvers. A 3/4 control moment gyroscope pyramid design was examined. This report focuses on maximum available momentum for mixed skew angle configurations. A method to maximize off-...

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Detalles Bibliográficos

Autor principal:	Lewis, Zachary A.
Formato:	Capítulo de libro
Lenguaje:	inglés
Publicado:	IntechOpen 2020
Materias:	Physical Sciences, Engineering and Technology
Acceso en línea:	https://www.intechopen.com/chapters/67815
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!