This book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers. After an introduction on the kinematics of the flexible and agile space vehicles, the modern architecture and functions of an AOC system are described and the main AOC modes reviewed with possible design solutions and examples. The dynamics of the flexible body in space are then considered using an original Lagrangian approach suitable for the control applications of large space flexible structures. Subsequent chapters address optimal control theory, attitude control methods, and orbit control applications, including the optimal orbital transfer with finite and infinite thrust. The theory is integrated with a description of current propulsion systems, with the focus especially on the new electric propulsion systems and state of the art sensors and actuators.
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Specifications
Book Details
Title
Flexible Spacecraft Dynamics, Control and Guidance
Imprint
Springer International Publishing AG
Product Form
Paperback
Publisher
Springer International Publishing AG
Genre
Technology & Engineering
ISBN13
9783319368771
Book Category
Higher Education and Professional Books
BISAC Subject Heading
TEC002000
Book Subcategory
Electronics and Communications Engineering Books
ISBN10
9783319368771
Language
English
Dimensions
Height
235 mm
Length
155 mm
Weight
5854 gr
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