Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters, Wang
Автор: de Ruiter Название: Spacecraft Dynamics and Control - An Introduction ISBN: 1118342364 ISBN-13(EAN): 9781118342367 Издательство: Wiley Рейтинг: Цена: 28956.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: 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.
Автор: Alfriend, Kyle T. Название: Spacecraft Formation Flying ISBN: 0750685336 ISBN-13(EAN): 9780750685337 Издательство: Elsevier Science Рейтинг: Цена: 16506.00 р. Наличие на складе: Поставка под заказ.
Описание: Provides a discussion of spacecraft relative motion, both in the unperturbed and perturbed settings. This title explains the main control approaches for regulating relative satellite dynamics, using both impulsive and continuous maneuvers, and present the main constituents required for relative navigation.
Автор: Daniel Choukroun; Yaakov Oshman; Julie Thienel; Mo Название: Advances in Estimation, Navigation, and Spacecraft Control ISBN: 3662447843 ISBN-13(EAN): 9783662447840 Издательство: Springer Рейтинг: Цена: 36570.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Estimation, - Navigation.- Spacecraft Guidance, Navigation and Control
Автор: Fichter, Walter Geshnizjani, Ramin T. Название: Principles of spacecraft control ISBN: 3031047796 ISBN-13(EAN): 9783031047794 Издательство: Springer Рейтинг: Цена: 6986.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: The objective of this textbook is to provide the mathematical models and algorithms needed to develop a thorough understanding of all control system functions of a rigid body spacecraft. Relatively simple, but practically applicable algorithms are presented rather than recent advances. We try to avoid detailed and specialized issues that are of less importance for the fundamental understanding, such as detailed environment models, etc. Furthermore, control problems that can be cast in standard formulations and solved with existing methods are not treated here. Instead, we intend to provide an understanding of the principles, put them in an engineering context, and try to give all explanations as concise as possible. Besides conventional three-axis attitude control systems, the following topics are treated in this book:• Control of agile rotation maneuvers using control moment gyros • Precise pointing control with error classes for pointing instruments • Control systems with accelerometers and free-flying test masses, which provide low-disturbance or disturbance-free environments We believe that these topics are of considerable relevance for the design of future spacecraft control systems, especially in the field of science and Earth observation missions.
Автор: F. Landis Markley; John L. Crassidis Название: Fundamentals of Spacecraft Attitude Determination and Control ISBN: 1493955691 ISBN-13(EAN): 9781493955695 Издательство: Springer Рейтинг: Цена: 10447.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion.
Автор: Hu, Weiduo, Название: Fundamental spacecraft dynamics and control ISBN: 1118753534 ISBN-13(EAN): 9781118753538 Издательство: Wiley Рейтинг: Цена: 16624.00 р. Наличие на складе: Поставка под заказ.
Описание: 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 applicationIntroduces the application to motion around asteroids - a new and important topicWritten by a very experienced researcher in this area
Описание: The immediate need for this volume was motivated by the ongoing ESA Swarm satellite mission, but the tools that are described are general and can be used for any future ionospheric multi-satellite mission with comparable instrumentation.
Автор: Hu Qinglei, Li Bo, Xiao Bing Название: Control Allocation for Spacecraft Under Actuator Faults ISBN: 981160438X ISBN-13(EAN): 9789811604386 Издательство: Springer Цена: 19564.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: 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.
Описание: 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.
Автор: Xie Название: Spacecraft Dynamics and Control ISBN: 9813364505 ISBN-13(EAN): 9789813364509 Издательство: Springer Рейтинг: Цена: 16769.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: 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.
