TY  - BOOK
ED  - Sands, Timothy
AB  - 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 meant for basic scientifically inclined readers, and commences with a chapter on the basics of spaceflight and leverages this remediation to reveal very advanced topics to new spaceflight enthusiasts. The topics learned from reading this text will prepare students and faculties to investigate interesting spaceflight problems in an era where cube satellites have made such investigations attainable by even small universities. It is the fondest hope of the editor and authors that readers enjoy this book.
DO  - https://doi.org/10.5772/intechopen.77574
KW  - Science
KW  - Mechanics
KW  - Aerodynamics
L1  - https://library.oapen.org/bitstream/id/971a4c26-9c07-4ed0-b550-527fdcefbf9d/external_content.pdf
LA  - English
LK  - https://library.oapen.org/handle/20.500.12657/44001
PB  - InTechOpen
PY  - 2020
SN  - 9781839685163
TI  - Advances in Spacecraft Attitude Controlnull
ER  - 
