Author: Publisher:
ISBN: 9780877035879
Category :
Languages : en
Pages :
Book Description
Dynamics and Control of Space Systems DyCoSS2012
Author: Spacecraft Modeling, Attitude Determination, and Control
Author: Yaguang YangPublisher: CRC Press
ISBN: 0429822146
Category : Science
Languages : en
Pages : 328
Book Description
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.
Hamiltonian Perturbation Solutions for Spacecraft Orbit Prediction
Author: MartÃn LaraPublisher: Walter de Gruyter GmbH & Co KG
ISBN: 3110667320
Category : Science
Languages : en
Pages : 315
Book Description
"Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems are discussed according to the Lie transforms method, which is the de facto standard in analytical orbital motion calculations"--Print version, page 4 of cover.
Spacecraft Dynamics and Control
Author: Anton H. de RuiterPublisher: John Wiley & Sons
ISBN: 1118403320
Category : Technology & Engineering
Languages : en
Pages : 562
Book 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 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.
Fundamentals of Dynamics and Control of Space Systems
Author: Krishna KumarPublisher: CreateSpace
ISBN: 9781470162412
Category :
Languages : en
Pages : 362
Book Description
This book is an outcome of the lectures delivered by the author for engineering students at Kyushu University, Japan, Korea Advanced Institute of Science and Technology, South Korea, and Ryerson University, Canada. The text started when the author was at Kyushu University, Japan. The author has been doing research on the subject of "Dynamics and Control of Space Systems" for the last fifteen years. During the course of research and teaching this subject, the author realized that there is an earnest need of a text which may provide basic understanding of inherent complexity in modelling space systems including environmental forces and torques. This text fulfils this goal through a step by step approach that explains each concept in a simple way with mathematical details and simple notations. This textbook is written for engineers and students pursuing study or research on the dynamics and control of space systems. The author has used all contents of this textbook in a core course on Space Systems (one semester, four hours a week). This text assumes that the reader is well acquainted with elementary calculus and linear algebra. Enough care has been taken so that the reader may attempt different types of problems. Each concept has been discussed with sufficient mathematical background supported by examples. A complete set of problems has been added to the end of every chapter. A "Solution Manual" accompanying this book provides a solution to most of the these exercise problems. In addition, a "Laboratory Manual" with this textbook provides the practical aspects of designing space systems with a focus on the construction of a Can-sized satellite. During the course of writing I have received several suggestions and comments from my colleagues and students. I especially thank my students Aradhana Choudhuri, Mike Alger, Geoffrey McVittie, Mike Tai, Kamran Shahid, Antonio Mauro, and Tarunkumar Patel who have gone through previous drafts of this book, and provided me with valuable suggestions. Finally, I express my sincere appreciation to my parents, my wife, Annu, and children, Diksha and Saurabh for their support and patience, without which it would have been impossible to complete this book. This textbook is dedicated to my parents and family for their inspiration and support. In writing this textbook, I have tried my best to provide the best relevant materials on the subject. I encourage and welcome all comments and suggestions to make this book more relevant to the contents of your course or research study. Please address your comments to [email protected].
Solution Manual
Author: Krishna KumarPublisher: Createspace Independent Publishing Platform
ISBN: 9781470166854
Category :
Languages : en
Pages : 0
Book Description
This Solution Manual is prepared to accompany and supplement the author's text ``Fundamentals of Dynamics and Control of Space Systems'' by K. D. Kumar. It contains detailed solutions for most problems in the textbook.
Spacecraft Dynamics and Control
Author: Yongchun XiePublisher: Springer
ISBN: 9789813364479
Category : Technology & Engineering
Languages : en
Pages : 422
Book Description
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
Author: Leonardo MazziniPublisher: Springer
ISBN: 9783319368771
Category : Technology & Engineering
Languages : en
Pages : 363
Book Description
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.
Dynamics and Control of Autonomous Space Vehicles and Robotics
Author: Ranjan VepaPublisher: Cambridge University Press
ISBN: 1108626580
Category : Technology & Engineering
Languages : en
Pages :
Book Description
Presenting the established principles underpinning space robotics (conservation of momentum and energy, stability) with a thorough and modern approach, chapters build from general physical foundations through an extensive treatment of kinematics of multi-body systems, and then to conservation principles in dynamics. The latter part of the book focuses on real-life applications related to space systems. Drawing upon years of practical experience and using numerous solved examples, illustrative applications and MATLAB, the author includes: an explanation of basic space mechanics and the dynamics of space vehicles; a rigorous treatment of conservation and variational principles in dynamics and in control theory that can be applied to a range of space vehicles and robotic systems; and a systematic presentation of the application of dynamics and control theory to real spacecraft systems.
Author: Jianke Xu