Контакты/Проезд  Доставка и Оплата Помощь/Возврат
История
  +7(495) 980-12-10
  пн-пт: 10-18 сб,вс: 11-18
  shop@logobook.ru
   
    Поиск книг                    Поиск по списку ISBN Расширенный поиск    
Найти
  Зарубежные издательства Российские издательства  
Авторы | Каталог книг | Издательства | Новинки | Учебная литература | Акции | Хиты | |
 

Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters, Wang Jie, Li Dong-Xu


Варианты приобретения
Цена: 18167.00р.
Кол-во:
Наличие: Поставка под заказ.  Есть в наличии на складе поставщика.
Склад Америка: Есть  
При оформлении заказа до: 2025-09-15
Ориентировочная дата поставки: Октябрь
При условии наличия книги у поставщика.

Добавить в корзину
в Мои желания

Автор: Wang Jie, Li Dong-Xu
Название:  Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters
ISBN: 9789811650963
Издательство: Springer
Классификация:




ISBN-10: 9811650969
Обложка/Формат: Hardcover
Страницы: 158
Вес: 0.45 кг.
Дата издания: 20.10.2021
Серия: Springerbriefs in law
Язык: English
Издание: 1st ed. 2022
Иллюстрации: 50 tables, color; 108 illustrations, color; 51 illustrations, black and white; ix, 185 p. 159 illus., 108 illus. in color.
Размер: 23.39 x 15.60 x 1.27 cm
Читательская аудитория: Professional & vocational
Подзаголовок: Proceedings of the ahfe 2021 virtual conferences on design for inclusion, affective and pleasurable design, interdisciplinary practice in industrial design, kansei engineering, and human factors for apparel and textile engineering, july 25-29, 2021,
Ссылка на Издательство: Link
Рейтинг:
Поставляется из: Германии
Описание: This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters.


Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion

Автор: Ye Yan; Xu Huang; Yueneng Yang
Название: Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion
ISBN: 9811026025 ISBN-13(EAN): 9789811026027
Издательство: Springer
Рейтинг:
Цена: 12157.00 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.

Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion

Автор: Yan Ye, Huang Xu, Yang Yueneng
Название: Dynamics and Control of Lorentz-Augmented Spacecraft Relative Motion
ISBN: 9811096651 ISBN-13(EAN): 9789811096655
Издательство: Springer
Рейтинг:
Цена: 6986.00 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.

Spacecraft Dynamics and Control

Автор: Xie Yongchun, Lei Yongjun, Guo Jianxin
Название: Spacecraft Dynamics and Control
ISBN: 9813364475 ISBN-13(EAN): 9789813364479
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.

Spacecraft Dynamics and Control

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.

Spacecraft Thermal Control Handbook. Fundamental Technologies V.1

Автор: Gilmore D. G.
Название: Spacecraft Thermal Control Handbook. Fundamental Technologies V.1
ISBN: 188498911X ISBN-13(EAN): 9781884989117
Издательство: AIAA
Рейтинг:
Цена: 13622.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: A thorough, technical survey of the various technologies used to achieve thermal control of all types of spacecraft, as well as the design and analysis methods used by thermal engineers.

Spacecraft Momentum Control Systems

Автор: Frederick A. Leve; Brian J. Hamilton; Mason A. Pec
Название: Spacecraft Momentum Control Systems
ISBN: 3319361740 ISBN-13(EAN): 9783319361741
Издательство: Springer
Рейтинг:
Цена: 13059.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: The goal of this book is to serve both as a practical technical reference and a resource for gaining a fuller understanding of the state of the art of spacecraft momentum control systems, specifically looking at control moment gyroscopes (CMGs).

Fundamentals of Spacecraft Attitude Determination and Control

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.

Guidance and Control Technology of Spacecraft on Elliptical Orbit

Автор: Liu
Название: Guidance and Control Technology of Spacecraft on Elliptical Orbit
ISBN: 9811079587 ISBN-13(EAN): 9789811079580
Издательство: Springer
Рейтинг:
Цена: 16769.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: It comprehensively covers the key technologies of guidance, navigation and control (GNC) system design for spacecraft in elliptical orbits, including the orbit design, formation configuration design and maintenance, autonomous navigation technology and relative navigation technology, as well as autonomous rendezvous technology.

Guidance and Control Technology of Spacecraft on Elliptical Orbit

Автор: Fucheng Liu; Shan Lu; Yue Sun
Название: Guidance and Control Technology of Spacecraft on Elliptical Orbit
ISBN: 9811340285 ISBN-13(EAN): 9789811340284
Издательство: Springer
Рейтинг:
Цена: 16769.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: This book introduces readers to the navigation, guidance and control technologies involved in single-spacecraft, double-spacecraft, and multiple-spacecraft tasks in elliptical orbits. It comprehensively covers the key technologies of guidance, navigation and control (GNC) system design for spacecraft in elliptical orbits, including the orbit design, formation configuration design and maintenance, autonomous navigation technology and relative navigation technology, as well as autonomous rendezvous technology. The methods that this book introduces are very close to actual practical engineering applications and presented in an accessible style. The book can serve as reference teaching material for senior undergraduates and postgraduates with space navigation related majors, while also providing essential information and guidance for research personnel and engineering technical personnel engaged in the development of GNC systems for spacecraft.

Control and Filtering of Fuzzy Systems with Switched Parameters

Автор: Shanling Dong; Zheng-Guang Wu; Peng Shi
Название: Control and Filtering of Fuzzy Systems with Switched Parameters
ISBN: 3030355659 ISBN-13(EAN): 9783030355654
Издательство: Springer
Рейтинг:
Цена: 13974.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание:

This book presents recent advances in control and filter design for Takagi-Sugeno (T-S) fuzzy systems with switched parameters. Thanks to its powerful ability in transforming complicated nonlinear systems into a set of linear subsystems, the T-S fuzzy model has received considerable attention from those the field of control science and engineering. Typical applications of T-S fuzzy systems include communication networks, and mechanical and power electronics systems. Practical systems often experience abrupt variations in their parameters or structures due to outside disturbances or component failures, and random switching mechanisms have been used to model these stochastic changes, such as the Markov jump principle.
There are three general types of controller/filter for fuzzy Markov jump systems: mode-independent, mode-dependent and asynchronous. Mode-independence does not focus on whether modes are accessible and ignores partially useful mode information, which results in some conservatism. The mode-dependent design approach relies on timely, complete and correct information regarding the mode of the studied plant. Factors like component failures and data dropouts often make it difficult to obtain exact mode messages, which further make the mode-dependent controllers/filters less useful. Recently, to overcome these issues, researchers have focused on asynchronous techniques. Asynchronous modes are accessed by observing the original systems based on certain probabilities. The book investigates the problems associated with controller/filter design for all three types.
It also considers various networked constraints, such as data dropouts and time delays, and analyzes the performances of the systems based on Lyapunov function and matrix inequality techniques, including the stochastic stability, dissipativity, and $H_\infty$. The book not only shows how these approaches solve the control and filtering problems effectively, but also offers potential meaningful research directions and ideas.
Covering a variety of fields, including continuous-time and discrete-time Markov processes, fuzzy systems, robust control, and filter design problems, the book is primarily intended for researchers in system and control theory, and is also a valuable reference resource for graduate and undergraduate students. Further, it provides cases of fuzzy control problems that are of interest to scientists, engineers and researchers in the field of intelligent control. Lastly it is useful for advanced courses focusing on fuzzy modeling, analysis, and control.
Spacecraft Thermal Control Technologies

Автор: Miao Jianyin, Zhong Qi, Zhao Qiwei
Название: Spacecraft Thermal Control Technologies
ISBN: 9811549834 ISBN-13(EAN): 9789811549830
Издательство: Springer
Рейтинг:
Цена: 30745.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание: This book presents fundamental theories, design and testing methodologies, and engineering applications concerning spacecraft thermal control systems, helping readers gain a comprehensive understanding of spacecraft thermal control systems and technologies.

Control Allocation for Spacecraft Under Actuator Faults

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.


ООО "Логосфера " Тел:+7(495) 980-12-10 www.logobook.ru
   В Контакте     В Контакте Мед  Мобильная версия