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.
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"It is of exceptional quality in both the range of subjects covered and the detail of that coverage. ... this book has a lot to offer to those of us involved in the developments and data processing for such projects, describing in detail external forces as well as the effects of non-rigidity. ... this is a very worthwhile volume, highly recommended for anyone involved in astronomical or other satellite projects." (Floor van Leeuwen, The Observatory, Vol. 135 (1246), June, 2015)
"This is an excellent book. Markley ... and Crassidis (Univ. of Buffalo) have succeeded in creating a work that is a good textbook for both upper-level undergraduate and graduate students as well as practitioners. ... book ends with several appendixes that further support the rest of the book and also provide novice practitioners with a good resource to help them understand the more technical and complicated material. ... Summing Up: Highly recommended. Aerospace engineering collections serving upper-division undergraduates through professionals/practitioners." (D. B. Spencer, Choice, Vol. 52 (7), March, 2015)