Spacecraft Dynamics and Control Book
Score: 5
From 2 Ratings

Spacecraft Dynamics and Control


  • Author : Marcel J. Sidi
  • Publisher : Cambridge University Press
  • Release Date : 1997
  • Genre: Technology & Engineering
  • Pages : 409
  • ISBN 10 : 0521787807

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Spacecraft Dynamics and Control Excerpt :

This 1997 book explains basic theory of spacecraft dynamics and control and the practical aspects of controlling a satellite.

Spacecraft Dynamics and Control Book

Spacecraft Dynamics and Control


  • Author : Enrico Canuto
  • Publisher : Butterworth-Heinemann
  • Release Date : 2018-03-08
  • Genre: Technology & Engineering
  • Pages : 790
  • ISBN 10 : 9780081017951

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Spacecraft Dynamics and Control Excerpt :

Spacecraft Dynamics and Control: The Embedded Model Control Approach provides a uniform and systematic way of approaching space engineering control problems from the standpoint of model-based control, using state-space equations as the key paradigm for simulation, design and implementation. The book introduces the Embedded Model Control methodology for the design and implementation of attitude and orbit control systems. The logic architecture is organized around the embedded model of the spacecraft and its surrounding environment. The model is compelled to include disturbance dynamics as a repository of the uncertainty that the control law must reject to meet attitude and orbit requirements within the uncertainty class. The source of the real-time uncertainty estimation/prediction is the model error signal, as it encodes the residual discrepancies between spacecraft measurements and model output. The embedded model and the uncertainty estimation feedback (noise estimator in the book) constitute the state predictor feeding the control law. Asymptotic pole placement (exploiting the asymptotes of closed-loop transfer functions) is the way to design and tune feedback loops around the embedded model (state predictor, control law, reference generator). The design versus the uncertainty class is driven by analytic stability and performance inequalities. The method is applied to several attitude and orbit control problems. The book begins with an extensive introduction to attitude geometry and algebra and ends with the core themes: state-space dynamics and Embedded Model Control. Fundamentals of orbit, attitude and environment dynamics are treated giving emphasis to state-space formulation, disturbance dynamics, state feedback and prediction, closed-loop stability. Sensors and actuators are treated giving emphasis to their dynamics and modelling of measurement errors. Numerical tables are included and their data employed for numerical simulations. Orbit and attitude control

Spacecraft Dynamics and Control Book

Spacecraft Dynamics and Control


  • Author : Anton H. de Ruiter
  • Publisher : John Wiley & Sons
  • Release Date : 2012-12-05
  • Genre: Technology & Engineering
  • Pages : 592
  • ISBN 10 : 9781118403327

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Spacecraft Dynamics and Control Excerpt :

Provides the basics of spacecraft orbital dynamics plusattitude dynamics and control, using vectrix notation Spacecraft Dynamics and Control: An Introductionpresents the fundamentals of classical control in the context ofspacecraft attitude control. This approach is particularlybeneficial for the training of students in both of the subjects ofclassical control as well as its application to spacecraft attitudecontrol. By using a physical system (a spacecraft) that the readercan visualize (rather than arbitrary transfer functions), it iseasier to grasp the motivation for why topics in control theory areimportant, as well as the theory behind them. The entiretreatment of both orbital and attitude dynamics makes use ofvectrix notation, which is a tool that allows the user to writedown any vector equation of motion without consideration of areference frame. This is particularly suited to the treatment ofmultiple reference frames. Vectrix notation also makes a very cleardistinction between a physical vector and its coordinaterepresentation in a reference frame. This is very important inspacecraft dynamics and control problems, where often multiplecoordinate representations are used (in different reference frames)for the same physical vector. Provides an accessible, practical aid for teaching andself-study with a layout enabling a fundamental understanding ofthe subject Fills a gap in the existing literature by providing ananalytical toolbox offering the reader a lasting, rigorousmethodology for approaching vector mechanics, a key element vitalto new graduates and practicing engineers alike Delivers an outstanding resource for aerospace engineeringstudents, and all those involved in the technical aspects of designand engineering in the space sector Contains numerous illustrations to accompany the written text.Problems are included to apply and extend the material in eachchapter Essential reading for graduate level aerospace engineeringstudents, aerospace professionals, res

Spacecraft Dynamics and Control Book

Spacecraft Dynamics and Control


  • Author : Yongchun Xie
  • Publisher : Springer Nature
  • Release Date : 2021-07-13
  • Genre: Technology & Engineering
  • Pages : 422
  • ISBN 10 : 9789813364486

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Spacecraft Dynamics and Control Excerpt :

This book presents up-to-date concepts and design methods relating to space dynamics and control, including spacecraft attitude control, orbit control, and guidance, navigation, and control (GNC), summarizing the research advances in control theory and methods and engineering practice from Beijing Institute of Control Engineering over the years. The control schemes and systems based on these achievements have been successfully applied to remote sensing satellites, communication satellites, navigation satellites, new technology test satellites, Shenzhou manned spacecraft, Tianzhou freight spacecraft, Tiangong 1/2 space laboratories, Chang'e lunar explorers, and many other missions. Further, the research serves as a guide for follow-up engineering developments in manned lunar engineering, deep space exploration, and on-orbit service missions.

Flexible Spacecraft Dynamics  Control and Guidance Book
Score: 5
From 2 Ratings

Flexible Spacecraft Dynamics Control and Guidance


  • Author : Leonardo Mazzini
  • Publisher : Springer
  • Release Date : 2015-10-27
  • Genre: Technology & Engineering
  • Pages : 363
  • ISBN 10 : 9783319255408

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Flexible Spacecraft Dynamics Control and Guidance Excerpt :

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.

Fundamental Spacecraft Dynamics and Control Book

Fundamental Spacecraft Dynamics and Control


  • Author : Weiduo Hu
  • Publisher : John Wiley & Sons
  • Release Date : 2015-09-03
  • Genre: Technology & Engineering
  • Pages : 300
  • ISBN 10 : 9781118754351

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Fundamental Spacecraft Dynamics and Control Excerpt :

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

Modern Spacecraft Dynamics and Control Book

Modern Spacecraft Dynamics and Control


  • Author : Marshall H. Kaplan
  • Publisher : Courier Dover Publications
  • Release Date : 2020-11-18
  • Genre: Technology & Engineering
  • Pages : 432
  • ISBN 10 : 9780486819181

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Modern Spacecraft Dynamics and Control Excerpt :

Topics include orbital and attitude maneuvers, orbit establishment and orbit transfer, plane rotation, interplanetary transfer and hyperbolic passage, lunar transfer, reorientation with constant momentum, attitude determination, more. Answers to selected exercises. 1976 edition.

Space Vehicle Dynamics and Control Book

Space Vehicle Dynamics and Control


  • Author : Bong Wie
  • Publisher : AIAA
  • Release Date : 1998
  • Genre: Science
  • Pages : 661
  • ISBN 10 : 1563472619

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Space Vehicle Dynamics and Control Excerpt :

"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 Attitude Determination and Control Book

Spacecraft Attitude Determination and Control


  • Author : J.R. Wertz
  • Publisher : Springer Science & Business Media
  • Release Date : 2012-12-06
  • Genre: Technology & Engineering
  • Pages : 858
  • ISBN 10 : 9789400999077

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Spacecraft Attitude Determination and Control Excerpt :

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.

Spacecraft Attitude Dynamics Book

Spacecraft Attitude Dynamics


  • Author : Peter C. Hughes
  • Publisher : Courier Corporation
  • Release Date : 2012-05-23
  • Genre: Science
  • Pages : 592
  • ISBN 10 : 9780486140131

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Spacecraft Attitude Dynamics Excerpt :

Comprehensive coverage includes environmental torques, energy dissipation, motion equations for four archetypical systems, orientation parameters, illustrations of key concepts with on-orbit flight data, and typical engineering hardware. 1986 edition.

Spacecraft Formation Flying Book

Spacecraft Formation Flying


  • Author : Kyle Alfriend
  • Publisher : Elsevier
  • Release Date : 2009-11-16
  • Genre: Technology & Engineering
  • Pages : 402
  • ISBN 10 : 0080559654

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Spacecraft Formation Flying Excerpt :

Space agencies are now realizing that much of what has previously been achieved using hugely complex and costly single platform projects—large unmanned and manned satellites (including the present International Space Station)—can be replaced by a number of smaller satellites networked together. The key challenge of this approach, namely ensuring the proper formation flying of multiple craft, is the topic of this second volume in Elsevier’s Astrodynamics Series, Spacecraft Formation Flying: Dynamics, control and navigation. In this unique text, authors Alfriend et al. provide a coherent discussion of spacecraft relative motion, both in the unperturbed and perturbed settings, explain the main control approaches for regulating relative satellite dynamics, using both impulsive and continuous maneuvers, and present the main constituents required for relative navigation. The early chapters provide a foundation upon which later discussions are built, making this a complete, standalone offering. Intended for graduate students, professors and academic researchers in the fields of aerospace and mechanical engineering, mathematics, astronomy and astrophysics, Spacecraft Formation Flying is a technical yet accessible, forward-thinking guide to this critical area of astrodynamics. The first book dedicated to spacecraft formation flying, written by leading researchers and professors in the field Develops the theory from an astrodynamical viewpoint, emphasizing modeling, control and navigation of formation flying satellites on Earth orbits Examples used to illustrate the main developments, with a sample simulation of a formation flying mission included to illustrate high fidelity modeling, control and relative navigation

Rigid Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time Varying Parameters Book

Rigid Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time Varying Parameters


  • Author : Jie Wang
  • Publisher : Springer Nature
  • Release Date : 2021-09-15
  • Genre: Technology & Engineering
  • Pages : 185
  • ISBN 10 : 9789811650970

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Rigid Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time Varying Parameters Excerpt :

This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft.

Spacecraft Attitude Dynamics and Control Book

Spacecraft Attitude Dynamics and Control


  • Author : Vladimir A. Chobotov
  • Publisher : Orbit Book Company
  • Release Date : 1991
  • Genre: Science
  • Pages : 140
  • ISBN 10 : UOM:39015024967401

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Spacecraft Attitude Dynamics and Control Excerpt :

Written for aerospace engineering courses of senior undergraduate or graduate level, this work presents basic concepts, methods and mathematical developments in spacecraft attitude dynamics and control. Topics covered include rigid body dynamics, environmental effects and linear control theory.

Fundamentals of Spacecraft Attitude Determination and Control Book

Fundamentals of Spacecraft Attitude Determination and Control


  • Author : F. Landis Markley
  • Publisher : Springer
  • Release Date : 2014-05-31
  • Genre: Technology & Engineering
  • Pages : 486
  • ISBN 10 : 9781493908028

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Fundamentals of Spacecraft Attitude Determination and Control Excerpt :

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.

Spacecraft Modeling  Attitude Determination  and Control Book

Spacecraft Modeling Attitude Determination and Control


  • Author : Yaguang Yang
  • Publisher : CRC Press
  • Release Date : 2019-02-06
  • Genre: Technology & Engineering
  • Pages : 328
  • ISBN 10 : 9780429822131

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Spacecraft Modeling Attitude Determination and Control Excerpt :

This book discusses all spacecraft attitude control-related topics: spacecraft (including attitude measurements, actuator, and disturbance torques), modeling, spacecraft attitude determination and estimation, and spacecraft attitude controls. Unlike other books addressing these topics, this book focuses on quaternion-based methods because of its many merits. The book lays a brief, but necessary background on rotation sequence representations and frequently used reference frames that form the foundation of spacecraft attitude description. It then discusses the fundamentals of attitude determination using vector measurements, various efficient (including very recently developed) attitude determination algorithms, and the instruments and methods of popular vector measurements. With available attitude measurements, attitude control designs for inertial point and nadir pointing are presented in terms of required torques which are independent of actuators in use. Given the required control torques, some actuators are not able to generate the accurate control torques, therefore, spacecraft attitude control design methods with achievable torques for these actuators (for example, magnetic torque bars and control moment gyros) are provided. Some rigorous controllability results are provided. The book also includes attitude control in some special maneuvers, such as orbital-raising, docking and rendezvous, that are normally not discussed in similar books. Almost all design methods are based on state-spaced modern control approaches, such as linear quadratic optimal control, robust pole assignment control, model predictive control, and gain scheduling control. Applications of these methods to spacecraft attitude control problems are provided. Appendices are provided for readers who are not familiar with these topics.