Spacecraft Modeling Attitude Determination And Control

Author : Yaguang Yang
Publisher : CRC Press
Page : 159 pages
File Size : 55,6 Mb
Release : 2019-02-06
Category : Science
ISBN : 9780429822131

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Spacecraft Modeling, Attitude Determination, and Control by Yaguang Yang Pdf

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.

Author : J.R. Wertz
Publisher : Springer Science & Business Media
Page : 877 pages
File Size : 52,9 Mb
Release : 2012-12-06
Category : Technology & Engineering
ISBN : 9789400999077

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Spacecraft Attitude Determination and Control by J.R. Wertz Pdf

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.

Author : F. Landis Markley,John L. Crassidis
Publisher : Springer
Page : 486 pages
File Size : 45,9 Mb
Release : 2014-05-31
Category : Technology & Engineering
ISBN : 9781493908028

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Fundamentals of Spacecraft Attitude Determination and Control by F. Landis Markley,John L. Crassidis Pdf

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.

Author : Marcel J. Sidi
Publisher : Cambridge University Press
Page : 434 pages
File Size : 41,7 Mb
Release : 1997
Category : Science
ISBN : 0521787807

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Spacecraft Dynamics and Control by Marcel J. Sidi Pdf

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

Author : Computer Sciences Corporation. Attitude Systems Operation
Publisher : Unknown
Page : 858 pages
File Size : 47,8 Mb
Release : 1978
Category : Space vehicles
ISBN : OCLC:17564560

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Spacecraft Attitude Determination and Control by Computer Sciences Corporation. Attitude Systems Operation Pdf

Author : Enrico Canuto,Carlo Novara,Donato Carlucci,Carlos Perez Montenegro,Luca Massotti
Publisher : Butterworth-Heinemann
Page : 790 pages
File Size : 41,9 Mb
Release : 2018-03-08
Category : Technology & Engineering
ISBN : 9780081017951

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Spacecraft Dynamics and Control by Enrico Canuto,Carlo Novara,Donato Carlucci,Carlos Perez Montenegro,Luca Massotti Pdf

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 problems of the European GOCE mission are the inspiration of numerical exercises and simulations. The suite of the attitude control modes of a GOCE-like mission is designed and simulated around the so-called mission state predictor. Solved and unsolved exercises are included within the text - and not separated at the end of chapters - for better understanding, training and application. Simulated results and their graphical plots are developed through MATLAB/Simulink code.

Author : Bong Wie
Publisher : AIAA
Page : 692 pages
File Size : 44,9 Mb
Release : 1998
Category : Mathematics
ISBN : 1563472619

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Space Vehicle Dynamics and Control by Bong Wie Pdf

A textbook that incorporates the latest methods used for the analysis of spacecraft orbital, attitude, and structural dynamics and control. Spacecraft dynamics is treated as a dynamic system with emphasis on practical applications, typical examples of which are the analysis and redesign of the pointing control system of the Hubble Space Telescope and the analysis of an active vibrations control for the COFS (Control of Flexible Structures) Mast Flight System. In addition to the three subjects mentioned above, dynamic systems modeling, analysis, and control are also discussed. Annotation copyrighted by Book News, Inc., Portland, OR

Author : Mohammed Chessab Mahdi
Publisher : Cambridge Scholars Publishing
Page : 190 pages
File Size : 48,6 Mb
Release : 2018-11-14
Category : Technology & Engineering
ISBN : 9781527521636

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Attitude Stabilization for CubeSat by Mohammed Chessab Mahdi Pdf

This book explores CubeSat technology, and develops a nonlinear mathematical model of a spacecraft with the assumption that the satellite is a rigid body. It places emphasis on the CubeSat subsystem, orbit dynamics and perturbations, the satellite attitude dynamic and modeling, and components of attitude determination and the control subsystem. The book focuses on the attitude stabilization methods of spacecraft, and presents gravity gradient stabilization, aerodynamic stabilization, and permanent magnets stabilization as passive stabilization methods, and spin stabilization and three axis stabilization as active stabilization methods. It also discusses the need to develop a control system design, and describes the design of three controller configurations, namely the Proportional–Integral–Derivative Controller (PID), the Linear Quadratic Regulator (LQR), and the Fuzzy Logic Controller (FLC) and how they can be used to design the attitude control of CubeSat three-axis stabilization. Furthermore, it presents the design of a suitable attitude stabilization system by combining gravity gradient stabilization with magnetic torquing, and the design of magnetic coils which can be added in order to improve the accuracy of attitude stabilization. The book then investigates, simulates, and compares possible controller configurations that can be used to control the currents of magnetic coils when magnetic coils behave as the actuator of the system.

Author : Michael Paluszek
Publisher : Elsevier
Page : 740 pages
File Size : 52,8 Mb
Release : 2023-04-27
Category : Technology & Engineering
ISBN : 9780323985413

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ADCS - Spacecraft Attitude Determination and Control by Michael Paluszek Pdf

ADCS - Spacecraft Attitude Determination and Control provides a complete introduction to spacecraft control. The book covers all elements of attitude control system design, including kinematics, dynamics, orbits, disturbances, actuators, sensors, and mission operations. Essential hardware details are provided for star cameras, reaction wheels, sun sensors, and other key components. The book explores how to design a control system for a spacecraft, control theory, and actuator and sensor details. Examples are drawn from the author’s 40 years of industrial experience with spacecraft such as GGS, GPS IIR, Mars Observer, and commercial communications satellites, and includes historical background and real-life examples. Features critical details on hardware and the space environment Combines theory and ready-to-implement practical algorithms Includes MATLAB code for all examples Provides plots and figures generated with the included code

Author : Daniel Choukroun,Yaakov Oshman,Julie Thienel,Moshe Idan
Publisher : Springer
Page : 545 pages
File Size : 53,9 Mb
Release : 2015-01-02
Category : Technology & Engineering
ISBN : 9783662447857

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Advances in Estimation, Navigation, and Spacecraft Control by Daniel Choukroun,Yaakov Oshman,Julie Thienel,Moshe Idan Pdf

This book presents selected papers of the Itzhack Y. Bar-Itzhack Memorial Sympo- sium on Estimation, Navigation, and Spacecraft Control. Itzhack Y. Bar-Itzhack, professor Emeritus of Aerospace Engineering at the Technion – Israel Institute of Technology, was a prominent and world-renowned member of the applied estimation, navigation, and spacecraft attitude determination communities. He touched the lives of many. He had a love for life, an incredible sense of humor, and wisdom that he shared freely with everyone he met. To honor Professor Bar-Itzhack's memory, as well as his numerous seminal professional achievements, an international symposium was held in Haifa, Israel, on October 14–17, 2012, under the auspices of the Faculty of Aerospace Engineering at the Technion and the Israeli Association for Automatic Control. The book contains 27 selected, revised, and edited contributed chapters written by eminent international experts. The book is organized in three parts: (1) Estimation, (2) Navigation and (3) Spacecraft Guidance, Navigation and Control. The volume was prepared as a reference for research scientists and practicing engineers from academy and industry in the fields of estimation, navigation, and spacecraft GN&C.

Author : William J. Palermo
Publisher : Unknown
Page : 131 pages
File Size : 46,5 Mb
Release : 2001-06-01
Category : Electronic
ISBN : 1423528522

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Angular Rate Estimation for Multi-Body Spacecraft Attitude Control by William J. Palermo Pdf

Spacecraft with high performance attitude control systems requirements have traditionally relied on imperfect mechanical gyroscopes for primary attitude determination. Gyro bias errors are corrected with a Kalman filter algorithm that uses updates from precise attitude sensors like star trackers. Gyroscopes, however, have a tendency to degrade or fail on orbit, becoming a life limiting factor for many satellites. When errors become erratic, pointing accuracy may be lost during short star gaps. Unpredictable gyro degradations have impacted NASA spacecraft missions such as Skylab and Hubble Space Telescope as well as several DoD and ESA satellites. An alternative source of angular rate information is a software implemented real time dynamic model. Inputs to the model from internal sensors and known spacecraft parameters enable the tracking of total system angular momentum from which body rates can be determined. With this technique, the Kalman filter algorithm provides error corrections to the dynamic model. The accuracy of internal sensors and input parameters determine the effectiveness of this angular rate estimation technique. This thesis presents the background for understanding and implementation of this technique into a representative attitude determination system. The system is incorporated into an attitude simulation model developed in SIMULINK to evaluate the effects of dynamic modeling errors and sensor inaccuracies. Results are presented that indicate that real time dynamic modeling is an effective method of angular rate determination for maneuvering multi-body spacecraft attitude control systems.

Author : Marshall H. Kaplan
Publisher : Courier Dover Publications
Page : 433 pages
File Size : 55,9 Mb
Release : 2020-11-18
Category : Technology & Engineering
ISBN : 9780486819181

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Modern Spacecraft Dynamics and Control by Marshall H. Kaplan Pdf

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.

Author : Michael Douglas Griffin
Publisher : AIAA
Page : 700 pages
File Size : 45,7 Mb
Release : 2004
Category : Space vehicles
ISBN : 1600861121

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Space Vehicle Design by Michael Douglas Griffin Pdf

Author : George Meyer
Publisher : Unknown
Page : 58 pages
File Size : 40,8 Mb
Release : 1971
Category : Space vehicles
ISBN : UIUC:30112106585281

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Design and Global Analysis of Spacecraft Attitude Control Systems by George Meyer Pdf

Author : John S. White (writer on artificial satellites.),Fred H. Shigemoto,Kent Bourquin
Publisher : Unknown
Page : 42 pages
File Size : 41,5 Mb
Release : 1961
Category : Artificial satellites
ISBN : UIUC:30112106591255

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Satellite Attitude Control Utilizing the Earth's Magnetic Field by John S. White (writer on artificial satellites.),Fred H. Shigemoto,Kent Bourquin Pdf

The torque developed by the interaction of current-carrying coils with the earth's magnetic field can be used as a means of attitude control. The degree to which the attitude of a vehicle can be maintained utilizing this torque depends on the fluctuations of the magnetic field at the satellite as the satellite orbits about the earth. Due to the nature of the torque developed only two vehicle axes can be c ntinuously controlled simultaneously. With the principle described, either a two- or three-coil system can be used to control vehicle attitude about two axes. Intermittent control about three axes can be obtained. (Author).