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Spacecraft Formation Flying, Alfriend, Kyle T.


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Цена: 110040.00T
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Автор: Alfriend, Kyle T.
Название:  Spacecraft Formation Flying
ISBN: 9780750685337
Издательство: Elsevier Science
Классификация:
ISBN-10: 0750685336
Обложка/Формат: Hardback
Страницы: 402
Вес: 0.75 кг.
Дата издания: 13.11.2009
Язык: English
Размер: 236 x 158 x 28
Читательская аудитория: Professional & vocational
Основная тема: Auto & aero eng
Подзаголовок: Dynamics, control and navigation
Ссылка на Издательство: Link
Рейтинг:
Поставляется из: Европейский союз
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.

Soyuz / A Universal Spacecraft

Автор: Hall Rex, Shayler David
Название: Soyuz / A Universal Spacecraft
ISBN: 1852336579 ISBN-13(EAN): 9781852336578
Издательство: Springer
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Цена: 46570.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Rex Hall and Dave Shayler provide a unique history of the Soyuz spacecraft programme from conception, through development to its use, detailed in the only English language book available on this topic. Planned for publication in 2003, it will celebrate 40 years since the original concept of the Soyuz craft.

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: 130430.00 T
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.

Spacecraft Thermal Control Technologies

Автор: Miao Jianyin, Zhong Qi, Zhao Qiwei
Название: Spacecraft Thermal Control Technologies
ISBN: 9811549834 ISBN-13(EAN): 9789811549830
Издательство: Springer
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Цена: 204970.00 T
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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.

Ionospheric Multi-Spacecraft Analysis Tools: Approaches for Deriving Ionospheric Parameters

Автор: Dunlop Malcolm Wray, Lьhr Hermann
Название: Ionospheric Multi-Spacecraft Analysis Tools: Approaches for Deriving Ionospheric Parameters
ISBN: 3030267342 ISBN-13(EAN): 9783030267346
Издательство: Springer
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Цена: 46570.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
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.

Deciphering Spacecraft Systems and Orbital Calculations

Автор: Tabor Jean
Название: Deciphering Spacecraft Systems and Orbital Calculations
ISBN: 1632401355 ISBN-13(EAN): 9781632401359
Издательство: Неизвестно
Цена: 128690.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.

Principles of spacecraft control

Автор: Fichter, Walter Geshnizjani, Ramin T.
Название: Principles of spacecraft control
ISBN: 3031047796 ISBN-13(EAN): 9783031047794
Издательство: Springer
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Цена: 46570.00 T
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.

Fundamental spacecraft dynamics and control

Автор: Hu, Weiduo,
Название: Fundamental spacecraft dynamics and control
ISBN: 1118753534 ISBN-13(EAN): 9781118753538
Издательство: Wiley
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Цена: 110830.00 T
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

Spacecraft Dynamics and Control

Автор: Canuto, Enrico
Название: Spacecraft Dynamics and Control
ISBN: 0081007000 ISBN-13(EAN): 9780081007006
Издательство: Elsevier Science
Рейтинг:
Цена: 133620.00 T
Наличие на складе: Поставка под заказ.
Описание:

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

Space Invaders

Автор: Michel van Pelt
Название: Space Invaders
ISBN: 1489990127 ISBN-13(EAN): 9781489990129
Издательство: Springer
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Цена: 21380.00 T
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Описание: Focusing on future modern spacecraft, Michel van Pelt explains the exciting life of unmanned space explorers, making the technology, design, development, operation and results of modern space probe missions understandable by lay readers.

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: 111790.00 T
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.

Planetary Spacecraft Navigation

Автор: James Miller
Название: Planetary Spacecraft Navigation
ISBN: 3030076784 ISBN-13(EAN): 9783030076788
Издательство: Springer
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Цена: 83850.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This textbook introduces the theories and practical procedures used in planetary spacecraft navigation. Written by a former member of NASA's Jet Propulsion Laboratory (JPL) navigation team, it delves into the mathematics behind modern digital navigation programs, as well as the numerous technological resources used by JPL as a key player in the field. In addition, the text offers an analysis of navigation theory application in recent missions, with the goal of showing students the relationship between navigation theory and the real-world orchestration of mission operations.


A Design for a Reusable Water-Based Spacecraft Known as the Spacecoach

Автор: Brian McConnell; Alexander Tolley
Название: A Design for a Reusable Water-Based Spacecraft Known as the Spacecoach
ISBN: 3319226762 ISBN-13(EAN): 9783319226767
Издательство: Springer
Рейтинг:
Цена: 60940.00 T
Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Based on components already in existence, this manual details a reference design for an interplanetary spacecraft that is simple, durable, fully reusable and comprised mostly of water.


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