Introduction to Spacecraft Thermal Design, Eric A. Silk
Автор: J. Jaap Wijker Название: Mechanical Vibrations in Spacecraft Design ISBN: 3642073549 ISBN-13(EAN): 9783642073540 Издательство: Springer Рейтинг: Цена: 18284.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Автор: J. Jaap Wijker Название: Random Vibrations in Spacecraft Structures Design ISBN: 9400736797 ISBN-13(EAN): 9789400736795 Издательство: Springer Рейтинг: Цена: 19589.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This book examines low and high frequency mechanical, acoustic random vibrations. The theory of random vibration is strongly related to the design of spacecraft structures and is illustrated with simple and more difficult worked examples.
Автор: James Miller Название: Planetary Spacecraft Navigation ISBN: 3030076784 ISBN-13(EAN): 9783030076788 Издательство: Springer Рейтинг: Цена: 12577.00 р. 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.
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.
Описание: This book collects selected papers from the 27th Conference of Spacecraft TT&C Technology in China held in Guangzhou on November 9-12, 2014. To meet requirements of new space endeavors, especially China`s deep-space programs, China`s spacecraft TT&C systems shall "go farther, measure more accurately and control better with higher efficacy".
Автор: Conway Название: Spacecraft Trajectory Optimization ISBN: 1107653827 ISBN-13(EAN): 9781107653825 Издательство: Cambridge Academ Рейтинг: Цена: 6018.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Dedicated to space trajectory optimization, this volume includes a variety of both analytical and numerical approaches to trajectory optimization. The authors, all experts and active researchers in their areas of specialization, have written chapters with palpable enthusiasm and relevance to contemporary problems.
Автор: F. Landis Markley; John L. Crassidis Название: Fundamentals of Spacecraft Attitude Determination and Control ISBN: 1493908014 ISBN-13(EAN): 9781493908011 Издательство: Springer Рейтинг: Цена: 12577.00 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: Canuto, Enrico Название: Spacecraft Dynamics and Control ISBN: 0081007000 ISBN-13(EAN): 9780081007006 Издательство: Elsevier Science Рейтинг: Цена: 20043.00 р. 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
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.
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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