1 edition of Introductory Attitude Dynamics found in the catalog.
Published
1989
by Springer New York in New York, NY
.
Written in English
Edition Notes
| Statement | by F. P. J. Rimrott |
| Series | Mechanical Engineering Series, Mechanical Engineering Series |
| Classifications | |
|---|---|
| LC Classifications | TL1-483 |
| The Physical Object | |
| Format | [electronic resource] / |
| Pagination | 1 online resource (xiii, 383p. 120 illus.) |
| Number of Pages | 383 |
| ID Numbers | |
| Open Library | OL27047135M |
| ISBN 10 | 1461281296, 1461235022 |
| ISBN 10 | 9781461281290, 9781461235026 |
| OCLC/WorldCa | 852789976 |
Attitude control is the process of controlling the orientation of an aerospace vehicle with respect to an inertial frame of reference or another entity such as the celestial sphere, certain fields, and nearby objects, etc.. Controlling vehicle attitude requires sensors to measure vehicle orientation, actuators to apply the torques needed to orient the vehicle to a desired attitude, and. This book can serve as a reference for individuals involved in mission planning, attitude determination, and attitude dynamics; an introductory textbook for stu dents and professionals starting in this field; an information source for experimen ters or others involved in spacecraft-related work who need information on spacecraft orientation and.
Established in , Attitude Dynamics is an information technology company with more than a decade of proven IT experience, world-class credentials and a wide range of technology expertise. As well as a trusted presence in South Africa, Attitude's footprint spans across the rest of Africa and the Middle East. Spacecraft Dynamics and Control: A Practical Engineering Approach - Ebook written by Marcel J. Sidi. Read this book using Google Play Books app on your PC, android, iOS devices. Download for offline reading, highlight, bookmark or take notes while you read Spacecraft Dynamics and Control: A Practical Engineering Approach.
Dynamics Fall Version Lecture L28 - 3D Rigid Body Dynamics: Equations of Motion; Euler’s Equations 3D Rigid Body Dynamics: Euler’s Equations We now turn to the task of deriving the general equations of motion for a three-dimensional rigid body. These equations are referred to as Euler’s Size: KB. It discusses relative motion, entry flight mechanics, low-thrust transfers, rocket propulsion fundamentals, attitude dynamics, and attitude control. The book is filled with illustrated concepts and real-world examples drawn from the space industry. Additionally, the book includes a “computational toolbox” composed of MATLAB M-files for.
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Introductory Attitude Dynamics (Mechanical Engineering Series) [F.P.J. Rimrott] on *FREE* shipping on qualifying offers. From the preface: The present text deals with attitude dynamics and is devoted to satellites of finite size.
It begins with a discussion of the inertia moment tensor. From the preface: "The present text deals with attitude dynamics and is devoted to satellites of finite size.
It begins with a discussion of the inertia moment tensor, Euler's law, Euler's angles, Euler's equations, and Euler's frequencies. After that a thorough treatment of the concept of centre. Additional Physical Format: Online version: Rimrott, F.P.J. (Friedrich Paul Johannes), Introductory attitude dynamics.
New York: Springer-Verlag, © The book deals with the determination of the angular position (altitude) of rotating finite-size solid gyroscopes, such as spacecraft. In addition to the study of rigid body behavior, the book pays particular attention to the behavior of deforming solid bodies and presents significant new results and provides the reader with a thorough understanding of the fundamental aspects of the dynamics.
From the preface: Introductory Attitude Dynamics book present text deals with attitude dynamics and is devoted to satellites of finite size.
It begins with a discussion of the inertia moment tensor, Euler's law, Euler's angles, Euler's equations, and Euler's frequencies. Get this from a library. Introductory Attitude Dynamics.
[F P J Rimrott] -- From the preface: "The present text deals with attitude dynamics and is devoted to satellites of finite size. It begins with a discussion of the inertia moment tensor, Euler's law, Euler's angles.
Introductory Attitude Dynamics (Mechanical Engineering Series) (1st Edition) by F.P.J. Rimrott, Rimroot F. P.J. Hardcover, Pages, Published ISBN / ISBN / Need it Fast. 2 day shipping options: Chesser, HC; FPJ Rimrott. "Attitude Drift of Torquefree Flexible Gyros Using Book Edition: 1st Edition.
Introduction to Attitude Dynamics and Control Chris Hall Aerospace and Ocean Engineering [email protected] • Every good dynamics course must begin with a differential equation • For attitude dynamics and control, the equation of choice is • This is the rotational equivalent of.
Introductory Attitude Dynamics (Mechanical Engineering Series) (Reprint Edition) by F.P.J. Rimrott Paperback, Pages, Published ISBN / ISBN / Need it Fast.
2 day shipping optionsBook Edition: Reprint Edition. Introductory Attitude Dynamics. 点击放大图片 出版社: Springer. 作者: From the preface: "The present text deals with Attitude dynamics and is devoted to satellites of finite size. It begins with a discussion of the inertia moment tensor, Euler's law, Euler's angles, Euler's equations, and Euler's frequencies.
The last couple of chapters of this book cover several spacecraft dynamics problems from the Lagrangian and Hamiltonian points of view. Rimrott, Introductory Attitude Dynamics,Springer-Verlag. Similar to Hughes, except uses scalar notation. Includes flexibility effects. Sidi, Spacecraft Dynamics and Control,Cambridge.
Thorough coverage of space flight topics with self-contained chapters serving a variety of courses in orbital mechanics, spacecraft dynamics, and astronautics This concise yet comprehensive book on space flight dynamics addresses all phases of a space mission: getting to space (launch trajectories), satellite motion in space (orbital motion, orbit transfers, attitude dynamics), and returning.
13 Attitude Dynamics J. = ⎛ ⎝ J xx J xy J xz J xy J yy J yz J xz J yz J zz ⎞ ⎠. () The components of the inertia tensor are divided into the moments of inertia, J xx,J yy,J zz,andtheproducts of inertia, J xy,J yz,J that ω is the angular velocity File Size: 1MB.
This book can serve as a reference for individuals involved in mission planning, attitude determination, and attitude dynamics; an introductory textbook for stu dents and professionals starting in this field; an information source for experimen ters or others involved in spacecraft-related work who need information on spacecraft orientation /5(6).
Introduction to Attitude Control. Dynamics is the study of the relationship between motion and the forces affecting motion. The study of the dynamics of objects in interplanetary or interstellar space is called astrodynamics and has two major.
Description. Provides the basics of spacecraft orbital dynamics plus attitude dynamics and control, using vectrix notation. Spacecraft Dynamics and Control: An Introduction presents the fundamentals of classical control in the context of spacecraft attitude control.
This approach is particularly beneficial for the training of students in both of the subjects of classical control as well as its. This book can serve as a reference for individuals involved in mission planning, attitude determination, and attitude dynamics; an introductory textbook for stu dents and professionals starting in this field; an information source for experimen ters or others involved in spacecraft-related work who need information on spacecraft orientation and /5(3).
Abstract. Dynamics is the study of the relationship between motion and the forces affecting motion. The study of the dynamics of objects in interplanetary or interstellar space is called astrodynamics and has two major divisions: celestial mechanics and attitude ial mechanics or orbit dynamics, discussed briefly in Chapter 3, is concerned with the motion of the center of mass of Cited by: Dynamics by Prof.
George Haller. This course reviews momentum and energy principles, and then covers the following topics: Hamilton's principle and Lagrange's equations; three-dimensional kinematics and dynamics of rigid bodies, steady motions and small deviations therefrom, gyroscopic effects, and causes of instability, free and forced vibrations of lumped-parameter and continuous systems.
Space Vehicle Attitude Dynamics and Control. This book shows the similarities within unmanned aerial vehicle and robotic system design, and will serve as a vital resource in the design of new. Introductory Attitude Dynamics From the preface: The present text deals with attitude dynamics and is devoted to satellites of finite size.
It begins with a discussion of the inertia moment tensor, Euler's law, Euler's angles, Euler's equations, and Euler's frequencies.This introductory chapter explains the reasons for adopting the embedded model control methodology in the design of the spacecraft orbit and attitude control algorithms addressed by the book.
Precedence among the book chapters is outlined with the help of a block diagram.I know of no other text that follows the unique and innovative approach of treating introductory spacecraft dynamics and control by means of vectrix calculus. This book can be considered as a prequel to those wishing to study the more advanced graduate-level text of Hughes.” (IEEE Control Systems Magazine, 1 .
