Fault Tolerant Attitude Control Of Spacecraft

Author : Qinglei Hu,Bing Xiao,Bo Li,Youmin Zhang
Publisher : Elsevier
Page : 306 pages
File Size : 51,7 Mb
Release : 2021-06-09
Category : Technology & Engineering
ISBN : 9780323901246

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Fault-Tolerant Attitude Control of Spacecraft by Qinglei Hu,Bing Xiao,Bo Li,Youmin Zhang Pdf

Fault-Tolerant Attitude Control of Spacecraft presents the fundamentals of spacecraft fault-tolerant attitude control systems, along with the most recent research and advanced, nonlinear control techniques. This book gives researchers a self-contained guide to the complex tasks of envisaging, designing, implementing and experimenting by presenting designs for integrated modeling, dynamics, fault-tolerant attitude control, and fault reconstruction for spacecraft. Specifically, the book gives a full literature review and presents preliminaries and mathematical models, robust fault-tolerant attitude control, fault-tolerant attitude control with actuator saturation, velocity-free fault tolerant attitude control, finite-time fault-tolerant attitude tracking control, and active fault-tolerant attitude contour. Finally, the book looks at the future of this interesting topic, offering readers a one-stop solution for those working on fault-tolerant attitude control for spacecraft. Presents the fundamentals of fault-tolerant attitude control systems for spacecraft in one practical solution Gives the latest research and thinking on nonlinear attitude control, fault tolerant control, and reliable attitude control Brings together concepts in fault control theory, fault diagnosis, and attitude control for spacecraft Covers advances in theory, technological aspects, and applications in spacecraft Presents detailed numerical and simulation results to assist engineers Offers a clear, systematic reference on fault-tolerant control and attitude control for spacecraft

Author : Qinglei Hu,Bing Xiao,Bo Li,Youmin Zhang
Publisher : Elsevier
Page : 304 pages
File Size : 42,5 Mb
Release : 2021-06-18
Category : Technology & Engineering
ISBN : 9780323898638

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Fault-Tolerant Attitude Control of Spacecraft by Qinglei Hu,Bing Xiao,Bo Li,Youmin Zhang Pdf

Fault-Tolerant Attitude Control of Spacecraft presents the fundamentals of spacecraft fault-tolerant attitude control systems, along with the most recent research and advanced, nonlinear control techniques. This book gives researchers a self-contained guide to the complex tasks of envisaging, designing, implementing and experimenting by presenting designs for integrated modeling, dynamics, fault-tolerant attitude control, and fault reconstruction for spacecraft. Specifically, the book gives a full literature review and presents preliminaries and mathematical models, robust fault-tolerant attitude control, fault-tolerant attitude control with actuator saturation, velocity-free fault tolerant attitude control, finite-time fault-tolerant attitude tracking control, and active fault-tolerant attitude contour. Finally, the book looks at the future of this interesting topic, offering readers a one-stop solution for those working on fault-tolerant attitude control for spacecraft. Presents the fundamentals of fault-tolerant attitude control systems for spacecraft in one practical solution Gives the latest research and thinking on nonlinear attitude control, fault tolerant control, and reliable attitude control Brings together concepts in fault control theory, fault diagnosis, and attitude control for spacecraft Covers advances in theory, technological aspects, and applications in spacecraft Presents detailed numerical and simulation results to assist engineers Offers a clear, systematic reference on fault-tolerant control and attitude control for spacecraft

Author : Qinglei Hu,Bo Li,Bing Xiao,Youmin Zhang
Publisher : Springer Nature
Page : 221 pages
File Size : 44,5 Mb
Release : 2021-03-13
Category : Technology & Engineering
ISBN : 9789811604393

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Control Allocation for Spacecraft Under Actuator Faults by Qinglei Hu,Bo Li,Bing Xiao,Youmin Zhang Pdf

This book provides a systematical and comprehensive description of some facets of modeling, designing, analyzing and exploring the control allocation and fault-tolerant control problems for over-actuated spacecraft attitude control system under actuator failures, system uncertainties and disturbances. The book intends to provide a unified platform for understanding and applicability of the fault-tolerant attitude control and control allocation for different purposes in aerospace engineering and some related fields. And it is particularly suited for readers who are interested to learn solutions in spacecraft attitude control system design and related engineering applications.

Author : Chingiz Hajiyev,Halil Ersin Soken
Publisher : CRC Press
Page : 305 pages
File Size : 45,8 Mb
Release : 2020-12-23
Category : Technology & Engineering
ISBN : 9781351248815

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Fault Tolerant Attitude Estimation for Small Satellites by Chingiz Hajiyev,Halil Ersin Soken Pdf

Small satellites use commercial off-the-shelf sensors and actuators for attitude determination and control (ADC) to reduce the cost. These sensors and actuators are usually not as robust as the available, more expensive, space-proven equipment. As a result, the ADC system of small satellites is more vulnerable to any fault compared to a system for larger competitors. This book aims to present useful solutions for fault tolerance in ADC systems of small satellites. The contents of the book can be divided into two categories: fault tolerant attitude filtering algorithms for small satellites and sensor calibration methods to compensate the sensor errors. MATLAB® will be used to demonstrate simulations. Presents fault tolerant attitude estimation algorithms for small satellites with an emphasis on algorithms’ practicability and applicability Incorporates fundamental knowledge about the attitude determination methods at large Discusses comprehensive information about attitude sensors for small satellites Reviews calibration algorithms for small satellite magnetometers with simulated examples Supports theory with MATLAB simulation results which can be easily understood by individuals without a comprehensive background in this field Covers up-to-date discussions for small satellite attitude systems design Dr. Chingiz Hajiyev is a professor at the Faculty of Aeronautics and Astronautics, Istanbul Technical University (Istanbul, Turkey). Dr. Halil Ersin Soken is an assistant professor at the Aerospace Engineering Department, Middle East Technical University (Ankara, Turkey).

Author : Chingiz Hajiyev,Halil Ersin Soken
Publisher : CRC Press
Page : 330 pages
File Size : 52,9 Mb
Release : 2020-12-22
Category : Technology & Engineering
ISBN : 9781351248822

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Fault Tolerant Attitude Estimation for Small Satellites by Chingiz Hajiyev,Halil Ersin Soken Pdf

Small satellites use commercial off-the-shelf sensors and actuators for attitude determination and control (ADC) to reduce the cost. These sensors and actuators are usually not as robust as the available, more expensive, space-proven equipment. As a result, the ADC system of small satellites is more vulnerable to any fault compared to a system for larger competitors. This book aims to present useful solutions for fault tolerance in ADC systems of small satellites. The contents of the book can be divided into two categories: fault tolerant attitude filtering algorithms for small satellites and sensor calibration methods to compensate the sensor errors. MATLAB® will be used to demonstrate simulations. Presents fault tolerant attitude estimation algorithms for small satellites with an emphasis on algorithms’ practicability and applicability Incorporates fundamental knowledge about the attitude determination methods at large Discusses comprehensive information about attitude sensors for small satellites Reviews calibration algorithms for small satellite magnetometers with simulated examples Supports theory with MATLAB simulation results which can be easily understood by individuals without a comprehensive background in this field Covers up-to-date discussions for small satellite attitude systems design Dr. Chingiz Hajiyev is a professor at the Faculty of Aeronautics and Astronautics, Istanbul Technical University (Istanbul, Turkey). Dr. Halil Ersin Soken is an assistant professor at the Aerospace Engineering Department, Middle East Technical University (Ankara, Turkey).

Author : Chuang Liu,Xiaokui Yue,Keke Shi,Zhaowei Sun
Publisher : Elsevier
Page : 386 pages
File Size : 52,5 Mb
Release : 2022-01-31
Category : Science
ISBN : 9780323990066

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Spacecraft Attitude Control by Chuang Liu,Xiaokui Yue,Keke Shi,Zhaowei Sun Pdf

Spacecraft Attitude Control: A Linear Matrix Inequality Approach solves problemsfor spacecraft attitude control systems using convex optimization and, specifi cally,through a linear matrix inequality (LMI) approach. High-precision pointing and improvedrobustness in the face of external disturbances and other uncertainties are requirementsfor the current generation of spacecraft. This book presents an LMI approach to spacecraftattitude control and shows that all uncertainties in the maneuvering process can besolved numerically. It explains how a model-like state space can be developed through amathematical presentation of attitude control systems, allowing the controller in question tobe applied universally. The authors describe a wide variety of novel and robust controllers,applicable both to spacecraft attitude control and easily extendable to second-ordersystems. Spacecraft Attitude Control provides its readers with an accessible introductionto spacecraft attitude control and robust systems, giving an extensive survey of currentresearch and helping researchers improve robust control performance. Considers the control requirements of modern spacecraft Presents rigid and flexible spacecraft control systems with inherent uncertainties mathematically, leading to a model-like state space Develops a variety of novel and robust controllers directly applicable to spacecraft control as well as extendable to other second-order systems Includes a systematic survey of recent research in spacecraft attitude control

Author : Wenchuan Cai
Publisher : Unknown
Page : 230 pages
File Size : 48,5 Mb
Release : 2010
Category : Adaptive control systems
ISBN : OCLC:748588626

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Robust Adaptive and Fault-tolerant Control for Attitude Tracking of Spacecraft by Wenchuan Cai Pdf

Explores an indirect (non-regressor based) adaptive and robust algorithm to deal with the effects of system uncertainties, unexpected disturbances, subsystem failures, and limited resources. Develops a robust adaptive attitude control scheme, based on the indirect adaptive algorithm, which was verified to be robust against external disturbances and adaptive to unknown and time-varying mass/inertia properties, and to tolerate limited thrusts. Designs three robust adaptive and fault-tolerant attitude control laws to accommodate actuator failures by extending the idea of the robust adaptive control method.

Author : Yuanqing Xia,Jinhui Zhang,Kunfeng Lu,Ning Zhou
Publisher : Springer
Page : 400 pages
File Size : 52,9 Mb
Release : 2018-07-02
Category : Technology & Engineering
ISBN : 9789811313738

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Finite Time and Cooperative Control of Flight Vehicles by Yuanqing Xia,Jinhui Zhang,Kunfeng Lu,Ning Zhou Pdf

This book focuses on the finite-time control of attitude stabilization, attitude tracking for individual spacecraft, and finite-time control of attitude synchronization. It discusses formation reconfiguration for multiple spacecraft in complex networks, and provides a new fast nonsingular terminal sliding mode surface (FNTSMS). Further, it presents newly designed controllers and several control laws to enhance the performance of spacecraft systems and meet related demands, such as strong disturbance rejection and high-precision control. As such, the book establishes a fundamental framework for these topics, while also highlighting the importance of integrated analysis. It is a useful resource for all researchers and students who are interested in this field, as well as engineers whose work involves designing flight vehicles.

Author : Mufeed Mahmoud,Jin Jiang,Youmin Zhang
Publisher : Springer Science & Business Media
Page : 238 pages
File Size : 47,9 Mb
Release : 2003-02-13
Category : Technology & Engineering
ISBN : 9783540003182

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Active Fault Tolerant Control Systems by Mufeed Mahmoud,Jin Jiang,Youmin Zhang Pdf

Modern technological systems rely on sophisticated control functions to meet increased performance requirements. For such systems, Fault Tolerant Control Systems (FTCS) need to be developed. Active FTCS are dependent on a Fault Detection and Identification (FDI) process to monitor system performance and to detect and isolate faults in the systems. The main objective of this book is to study and to validate some important issues in real-time Active FTCS by means of theoretical analysis and simulation. Several models are presented to achieve this objective, taking into consideration practical aspects of the system to be controlled, performance deterioration in FDI algorithms, and limitations in reconfigurable control laws.

Author : F. Landis Markley,John L. Crassidis
Publisher : Springer
Page : 486 pages
File Size : 42,9 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 : Hanspeter Schaub,John L. Junkins
Publisher : AIAA
Page : 744 pages
File Size : 55,7 Mb
Release : 2003
Category : Celestial mechanics
ISBN : 1600860273

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Analytical Mechanics of Space Systems by Hanspeter Schaub,John L. Junkins Pdf

Author : Kyle Alfriend,Srinivas Rao Vadali,Pini Gurfil,Jonathan How,Louis Breger
Publisher : Elsevier
Page : 402 pages
File Size : 47,5 Mb
Release : 2009-11-16
Category : Technology & Engineering
ISBN : 0080559654

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Spacecraft Formation Flying by Kyle Alfriend,Srinivas Rao Vadali,Pini Gurfil,Jonathan How,Louis Breger Pdf

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

Author : Dong Ye,You Li,Yan Xiao
Publisher : Academic Press
Page : 280 pages
File Size : 42,8 Mb
Release : 2022-08-02
Category : Technology & Engineering
ISBN : 9780323954563

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Fast Satellite Attitude Maneuver and Control by Dong Ye,You Li,Yan Xiao Pdf

Fast Satellite Attitude Maneuver and Control introduces the concept of agile satellites and corresponding fast maneuver attitude control systems, systematically and comprehensively presenting recent research results of fast maneuver attitude control for agile satellites by using advanced nonlinear control techniques. This reference book focuses on modeling and attitude control, considering different actuator combinations, actuator installation deviation, actuator fault, and flexible appendage coupling effect for agile satellites. The book provides a unified platform for understanding and applicability of agile satellites fast maneuverer and stabilization control for different purposes. It will be an excellent resource for researchers working on spacecraft design, nonlinear control systems, vehicle systems and complex control systems. Unifies existing and emerging concepts concerning nonlinear control theory, fault tolerant, and attitude control for agile satellites Provides a series of the latest results, including, but not limited to, fast maneuverer and stabilization control, hybrid actuator control, nonlinear attitude control, fault tolerant control, and active vibration suppression towards agile satellites Comprehensively captures recent advances of theory, technological aspects and applications of fast maneuverer and stabilization control in agile satellites Addresses research problems in each chapter, along with numerical and simulation results that reflect engineering practice and demonstrate the focus of developed analysis and synthesis approaches Contains comprehensive, up-to-date references, which play an indicative role for further study

Author : Liang Yan,Haibin Duan,Xiang Yu
Publisher : Springer Nature
Page : 5416 pages
File Size : 46,9 Mb
Release : 2021-11-12
Category : Technology & Engineering
ISBN : 9789811581557

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Advances in Guidance, Navigation and Control by Liang Yan,Haibin Duan,Xiang Yu Pdf

This book features the latest theoretical results and techniques in the field of guidance, navigation, and control (GNC) of vehicles and aircraft. It covers a range of topics, including, but not limited to, intelligent computing communication and control; new methods of navigation, estimation, and tracking; control of multiple moving objects; manned and autonomous unmanned systems; guidance, navigation, and control of miniature aircraft; and sensor systems for guidance, navigation, and control. Presenting recent advances in the form of illustrations, tables, and text, it also provides detailed information of a number of the studies, to offer readers insights for their own research. In addition, the book addresses fundamental concepts and studies in the development of GNC, making it a valuable resource for both beginners and researchers wanting to further their understanding of guidance, navigation, and control.

Author : J.R. Wertz
Publisher : Springer Science & Business Media
Page : 877 pages
File Size : 52,5 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.