Fundamentals of Spacecraft Attitude Determination and Control (Record no. 54811)
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000 -LEADER | |
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fixed length control field | 03487nam a22005415i 4500 |
001 - CONTROL NUMBER | |
control field | 978-1-4939-0802-8 |
005 - DATE AND TIME OF LATEST TRANSACTION | |
control field | 20200421111658.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
fixed length control field | 140531s2014 xxu| s |||| 0|eng d |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
ISBN | 9781493908028 |
-- | 978-1-4939-0802-8 |
082 04 - CLASSIFICATION NUMBER | |
Call Number | 629.1 |
100 1# - AUTHOR NAME | |
Author | Markley, F. Landis. |
245 10 - TITLE STATEMENT | |
Title | Fundamentals of Spacecraft Attitude Determination and Control |
300 ## - PHYSICAL DESCRIPTION | |
Number of Pages | XV, 486 p. 96 illus., 4 illus. in color. |
490 1# - SERIES STATEMENT | |
Series statement | Space Technology Library ; |
505 0# - FORMATTED CONTENTS NOTE | |
Remark 2 | 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. |
520 ## - SUMMARY, ETC. | |
Summary, etc | 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. |
700 1# - AUTHOR 2 | |
Author 2 | Crassidis, John L. |
856 40 - ELECTRONIC LOCATION AND ACCESS | |
Uniform Resource Identifier | http://dx.doi.org/10.1007/978-1-4939-0802-8 |
942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
Koha item type | eBooks |
264 #1 - | |
-- | New York, NY : |
-- | Springer New York : |
-- | Imprint: Springer, |
-- | 2014. |
336 ## - | |
-- | text |
-- | txt |
-- | rdacontent |
337 ## - | |
-- | computer |
-- | c |
-- | rdamedia |
338 ## - | |
-- | online resource |
-- | cr |
-- | rdacarrier |
347 ## - | |
-- | text file |
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-- | rda |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Engineering. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Dynamics. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Ergodic theory. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Aerospace engineering. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Astronautics. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Control engineering. |
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Engineering. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Aerospace Technology and Astronautics. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Dynamical Systems and Ergodic Theory. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Control. |
912 ## - | |
-- | ZDB-2-ENG |
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