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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 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.

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Series Title
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Call Number
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Publisher
London : .,
Collation
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Language
English
ISBN/ISSN
9781789848021
Classification
NONE
Content Type
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Media Type
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Carrier Type
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Edition
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Subject(s)
Science
Specific Detail Info
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Statement of Responsibility
Other Information
Cataloger
Jemadi
Source
https://openresearchlibrary.org/content/0595a702-1d4a-4a0c-82da-e870ad268ef4
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