Spacecraft Dynamics And Control

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Author: Anton H. de Ruiter
Publisher: John Wiley & Sons
ISBN: 1118403320
Size: 45.38 MB
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Spacecraft Dynamics And Control by Anton H. de Ruiter


Original Title: Spacecraft Dynamics And Control

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 application to spacecraft attitude control. By using a physical system (a spacecraft) that the reader can visualize (rather than arbitrary transfer functions), it is easier to grasp the motivation for why topics in control theory are important, as well as the theory behind them. The entire treatment of both orbital and attitude dynamics makes use of vectrix notation, which is a tool that allows the user to write down any vector equation of motion without consideration of a reference frame. This is particularly suited to the treatment of multiple reference frames. Vectrix notation also makes a very clear distinction between a physical vector and its coordinate representation in a reference frame. This is very important in spacecraft dynamics and control problems, where often multiple coordinate representations are used (in different reference frames) for the same physical vector. Provides an accessible, practical aid for teaching and self-study with a layout enabling a fundamental understanding of the subject Fills a gap in the existing literature by providing an analytical toolbox offering the reader a lasting, rigorous methodology for approaching vector mechanics, a key element vital to new graduates and practicing engineers alike Delivers an outstanding resource for aerospace engineering students, and all those involved in the technical aspects of design and engineering in the space sector Contains numerous illustrations to accompany the written text. Problems are included to apply and extend the material in each chapter Essential reading for graduate level aerospace engineering students, aerospace professionals, researchers and engineers.

Fundamental Spacecraft Dynamics And Control

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Author: Weiduo Hu
Publisher: John Wiley & Sons
ISBN: 1118753534
Size: 80.95 MB
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Fundamental Spacecraft Dynamics And Control by Weiduo Hu


Original Title: Fundamental Spacecraft Dynamics And Control

An extensive text reference includes around an asteroid - a new and important topic * Covers the most updated contents in spacecraft dynamics and control, both in theory and application * Introduces the application to motion around asteroids - a new and important topic * Written by a very experienced researcher in this area

Flexible Spacecraft Dynamics Control And Guidance

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Author: Leonardo Mazzini
Publisher: Springer
ISBN: 3319255401
Size: 48.82 MB
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Flexible Spacecraft Dynamics Control And Guidance by Leonardo Mazzini


Original Title: Flexible Spacecraft Dynamics Control And Guidance

This book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers. After an introduction on the kinematics of the flexible and agile space vehicles, the modern architecture and functions of an AOC system are described and the main AOC modes reviewed with possible design solutions and examples. The dynamics of the flexible body in space are then considered using an original Lagrangian approach suitable for the control applications of large space flexible structures. Subsequent chapters address optimal control theory, attitude control methods, and orbit control applications, including the optimal orbital transfer with finite and infinite thrust. The theory is integrated with a description of current propulsion systems, with the focus especially on the new electric propulsion systems and state of the art sensors and actuators.

Space Vehicle Dynamics And Control

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Author: Bong Wie
Publisher: AIAA
ISBN: 9781563472619
Size: 66.77 MB
Format: PDF
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Space Vehicle Dynamics And Control by Bong Wie


Original Title: Space Vehicle Dynamics And Control

"Space Vehicle Dynamics and Control provides a solid foundation in dynamic modeling, analysis, and control of space vehicles. More than 200 figures, photographs, and tables are featured in detailed sections covering the fundamentals of controlling orbital, attitude, and structural motions of space vehicles. The textbook highlights a range of orbital maneuvering and control problems: orbital transfer, rendezvous, and halo orbit determination and control. Rotational maneuvering and attitude control problems of space vehicles under the influence of reaction jet firings, internal energy dissipation, or momentum transfer via reaction wheels and control moment gyros are treated in detail. The textbook also highlights the analysis and design of attitude control systems in the presence of structural flexibility and/or propellant sloshing. At the end of each chapter, Dr. Wie includes a helpful list of references for graduate students and working professionals studying spacecraft dynamics and control. A bibliography of more than 350 additional references in the field of spacecraft guidance, control, and dynamics is also provided at the end of the book. This text requires a thorough knowledge of vector and matrix algebra, calculus, ordinary differential equations, engineering mechanics, and linear system dynamics and control. The first two chapters provide a summary of such necessary background material. Since some problems may require the use of software for the analysis, control design, and numerical simulation, readers should have access to computational software (i.e., MATLAB) on a personal computer.

Spacecraft Dynamics And Control

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Author: Enrico Canuto
Publisher: Butterworth-Heinemann
ISBN: 0081017952
Size: 32.71 MB
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Spacecraft Dynamics And Control by Enrico Canuto


Original Title: Spacecraft Dynamics And Control

Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform way of approaching space engineering control problems from the standpoint of model-based control, using state equations as the key dynamic model for simulation, design and implementation. The book introduces model-based control design methodology for spacecraft attitude and orbit control. It then covers model-based estimation and control algorithm design, using spacecraft and environment dynamics as the core of the implemented control algorithms—referred to as the embedded (or internal) model. The book also presents two appendices, in which the state equation machinery is fully exploited and introduced. Embedded model and noise estimators constitute a closed‐loop state predictor to be stabilized by the estimator gains. Kalman filter optimization may be adopted under certain restricted assumptions. This book is indispensable for researchers and practitioners in the field of control engineering, aerospace engineering, mechanical engineering and applied mathematics. Includes exercises within the text—not separated at the end of the chapter—for better understanding, training and application Provides a uniform way of approaching space engineering control problems from the standpoint of model-based control Presents method for including environment perturbations in the control unit embedded model and for estimating perturbation derivatives in presence of measurement noise MATLAB Simulink code available for modeling, simulating and analyzing multidomain dynamic systems

Spacecraft Attitude Determination And Control

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Author: James R. Wertz
Publisher: Springer Science & Business Media
ISBN: 9400999070
Size: 34.74 MB
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Spacecraft Attitude Determination And Control by James R. Wertz


Original Title: Spacecraft Attitude Determination And Control

Roger D. Werking Head, Attitude Determination and Control Section National Aeronautics and Space Administration/ Goddard Space Flight Center Extensiye work has been done for many years in the areas of attitude determination, attitude prediction, and attitude control. During this time, it has been difficult to obtain reference material that provided a comprehensive overview of attitude support activities. This lack of reference material has made it difficult for those not intimately involved in attitude functions to become acquainted with the ideas and activities which are essential to understanding the various aspects of spacecraft attitude support. As a result, I felt the need for a document which could be used by a variety of persons to obtain an understanding of the work which has been done in support of spacecraft attitude objectives. It is believed that this book, prepared by the Computer Sciences Corporation under the able direction of Dr. James Wertz, provides this type of reference. 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 how it is determined, but who have neither the time nor the resources to pursue the varied literature on this subject; and a tool for encouraging those who could expand this discipline to do so, because much remains to be done to satisfy future needs.

Dynamics And Control Of Lorentz Augmented Spacecraft Relative Motion

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Author: Ye Yan
Publisher: Springer
ISBN: 9811026033
Size: 50.50 MB
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Dynamics And Control Of Lorentz Augmented Spacecraft Relative Motion by Ye Yan


Original Title: Dynamics And Control Of Lorentz Augmented Spacecraft Relative Motion

This book develops a dynamical model of the orbital motion of Lorentz spacecraft in both unperturbed and J2-perturbed environments. It explicitly discusses three kinds of typical space missions involving relative orbital control: spacecraft hovering, rendezvous, and formation flying. Subsequently, it puts forward designs for both open-loop and closed-loop control schemes propelled or augmented by the geomagnetic Lorentz force. These control schemes are entirely novel and represent a significantly departure from previous approaches.

Spacecraft Attitude Dynamics And Control

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Author: Vladimir A. Chobotov
Publisher: Krieger Publishing Company
ISBN: 9780894640698
Size: 31.72 MB
Format: PDF, Mobi
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Spacecraft Attitude Dynamics And Control by Vladimir A. Chobotov


Original Title: Spacecraft Attitude Dynamics And Control

Presented here are the basic concepts, methods, and mathematical developments which are necessary to understand spacecraft attitude dynamics and control. This book is a comprehensive and self-contained treatment with emphasis on the practical aspects of the subject. It is a "road map" to the field of spacecraft dynamics and control, which contains all essential elements of kinematics, rigid body dynamics, linear control theory, environmental effects, and the theory of the stability of motion, all in a single volume. The book is based on the author's more than forty years of industrial and teaching experience and can be used as a textbook in aerospace engineering courses at either the senior or the first-year graduate school level.The Spacecraft Attitude Dynamics, 2008 Reprint with Corrections, Supplement and CD-ROM augments the original material published in 1991 by correcting errors and presenting a Supplement that reviews recent trends in dynamics and control of small satellite systems and tethers in space. Also, included is a CD-ROM the objective of which is to provide view points and guidelines for solving selected problems in the text. Spinners and a menu are employed to enhance the learning experience by providing numerical results for ranges of input parameters to selected problems. Moreover, a faculty CD-ROM is also available that presents complete solutions to the problems of interest.

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