Fundamentals of spacecraft attitude determination and control /
نام عام مواد
[Book]
نام نخستين پديدآور
F. Landis Markley, John L. Crassidis
مشخصات ظاهری
نام خاص و کميت اثر
1 online resource (xv, 486 pages) :
ساير جزييات
illustrations (some color)
فروست
عنوان فروست
Space Technology Library
یادداشتهای مربوط به کتابنامه ، واژه نامه و نمایه های داخل اثر
متن يادداشت
Includes bibliographical references and index
یادداشتهای مربوط به مندرجات
متن يادداشت
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
بدون عنوان
0
یادداشتهای مربوط به خلاصه یا چکیده
متن يادداشت
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
ویراست دیگر از اثر در قالب دیگر رسانه
شماره استاندارد بين المللي کتاب و موسيقي
9781493908011
موضوع (اسم عام یاعبارت اسمی عام)
موضوع مستند نشده
Space vehicles-- Attitude control systems
مقوله موضوعی
موضوع مستند نشده
TEC002000
موضوع مستند نشده
TRP
موضوع مستند نشده
TTDS
رده بندی کنگره
شماره رده
TL3260
نام شخص به منزله سر شناسه - (مسئولیت معنوی درجه اول )