Fundamentals of spacecraft attitude determination and control / F. Landis Markley, John L. Crassidis.
By: Markley, F. Landis [author.].
Contributor(s): Crassidis, John L [author.].
Series: Space technology library: v. 33.Description: xv, 486 pages : illustrations, charts (graphs, tables) ; 24 cm.ISBN: 1493908014; 9781493908011.Subject(s): Space vehicles -- Attitude control systems | Engineering | Engineering | Space vehicles -- Attitude control systemsOnline resources: Full-text onlineItem type | Current location | Call number | Status | Date due | Barcode | Item holds |
---|---|---|---|---|---|---|
Book | Skoltech library Shelves | TL3260 .M37 2014 (Browse shelf) | Available | 2000007708 |
Browsing Skoltech library Shelves , Shelving location: Shelves Close shelf browser
TL1100 Spacecraft power systems / | TL1100 Spacecraft power systems / | TL1489 .H37 2004 Spacecraft--environment interactions / | TL3260 .M37 2014 Fundamentals of spacecraft attitude determination and control / | TN100 .M44 2015 Core analysis: a best practice guide | TN269 .M53 2011 Field geophysics / | TN269 .T44 1989 Applied geophysics / |
Includes bibliographical references (at the end of each chapter) and index.
Introduction -- Matrices, vectors, frames, transforms -- Attitude kinematics and dynamics -- Sensors and actuators -- Static attitude determination methods -- Filtering for attitude estimation and calibration -- Attitude control -- Quaternion identities -- Euler angles -- Orbital dynamics -- Environment models -- Review of control and estimation theory -- Computer software.
"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 alsoprovides 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." --Publisher's Website.
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