Advances in Spacecraft Attitude Control

Spacecraft attitude maneuvers comply with Euler's moment equations, a set of three nonlinear, coupled differential equations. Nonlinearities complicate the mathematical treatment of the seemingly simple action of rotating, and these complications lead to a robust lineage of research. This book is me...

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Detalles Bibliográficos
Autor principal: Timothy Sands
Formato: Libro
Publicado: IntechOpen 2020
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Acceso en línea:Ver este registro en EBSCOhost