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Fundamentals of Spacecraft Attitude Determination and Control [[electronic resource] /] / by F. Landis Markley, John L. Crassidis



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Autore: Markley F. Landis Visualizza persona
Titolo: Fundamentals of Spacecraft Attitude Determination and Control [[electronic resource] /] / by F. Landis Markley, John L. Crassidis Visualizza cluster
Pubblicazione: New York, NY : , : Springer New York : , : Imprint : Springer, , 2014
Edizione: 1st ed. 2014.
Descrizione fisica: 1 online resource (XVI, 470 p. 96 illus., 4 illus. in color.)
Disciplina: 629.4742
Soggetto topico: Aerospace engineering
Astronautics
Dynamics
Ergodic theory
Control engineering
Aerospace Technology and Astronautics
Dynamical Systems and Ergodic Theory
Control and Systems Theory
Soggetto genere / forma: Electronic books.
Persona (resp. second.): CrassidisJohn L
Note generali: Bibliographic Level Mode of Issuance: Monograph
Nota di bibliografia: Includes bibliographical references at the end of each chapter and index.
Nota di contenuto: Attitude Determination and Estimation -- Matrices, Vectors, Frames, Transforms -- Rotational Kinematics and Dynamics -- Sensors and Actuators -- Static Attitude Determination Methods -- Filtering for Attitude Determination -- Attitude Control.
Sommario/riassunto: This book explores topics that are central to the field of spacecraft attitude determination and control. The authors provide rigorous theoretical derivations of significant algorithms accompanied by a generous amount of qualitative discussions of the subject matter. The book documents the development of the important concepts and methods in a manner accessible to practicing engineers, graduate-level engineering students and applied mathematicians. It includes detailed examples from actual mission designs to help ease the transition from theory to practice, and also provides prototype algorithms that are readily available on the author’s website. Subject matter includes both theoretical derivations and practical implementation of spacecraft attitude determination and control systems. It provides detailed derivations for attitude kinematics and dynamics, and provides detailed description of the most widely used attitude parameterization, the quaternion. This title also provides a thorough treatise of attitude dynamics including Jacobian elliptical functions. It is the first known book to provide detailed derivations and explanations of state attitude determination, and gives readers real-world examples from actual working spacecraft missions. The subject matter is chosen to fill the void of existing textbooks and treatises, especially in state and dynamics attitude determination. MATLAB code of all examples will be provided through an external website.
Titolo autorizzato: Fundamentals of Spacecraft Attitude Determination and Control  Visualizza cluster
ISBN: 1-4939-0802-2
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910299748103321
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Serie: Space Technology Library ; ; 33