Spacecraft modeling, attitude determination, and control :, Yang, Yaguang,
Новое издание
Автор: Hall Rex, Shayler David Название: Soyuz / A Universal Spacecraft ISBN: 1852336579 ISBN-13(EAN): 9781852336578 Издательство: Springer Рейтинг: 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.
Автор: Conway Название: Spacecraft Trajectory Optimization ISBN: 1107653827 ISBN-13(EAN): 9781107653825 Издательство: Cambridge Academ Рейтинг: Цена: 40120.00 T 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: Paul A. Czysz; Claudio Bruno; Bernd Chudoba Название: Future Spacecraft Propulsion Systems and Integration ISBN: 3662547422 ISBN-13(EAN): 9783662547427 Издательство: Springer Рейтинг: Цена: 186330.00 T Наличие на складе: Невозможна поставка. Описание: The updated and expanded third edition of this book focuses on the multi-disciplinary coupling between flight-vehicle hardware alternatives and enabling propulsion systems. It discusses how to match near-term and far-term aerospace vehicles to missions and provides a comprehensive overview of the subject, directly contributing to the next-generation space infrastructure, from space tourism to space exploration. This holistic treatment defines a mission portfolio addressing near-term to long-term space transportation needs covering sub-orbital, orbital and escape flight profiles. In this context, a vehicle configuration classification is introduced covering alternatives starting from the dawn of space access. A best-practice parametric sizing approach is introduced to correctly design the flight vehicle for the mission. This technique balances required mission with the available vehicle solution space and is an essential capability sought after by technology forecasters and strategic planners alike.
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: 83850.00 T 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: F. Landis Markley; John L. Crassidis Название: Fundamentals of Spacecraft Attitude Determination and Control ISBN: 1493955691 ISBN-13(EAN): 9781493955695 Издательство: Springer Рейтинг: Цена: 69650.00 T 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: 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
Автор: Gilmore D. G. Название: Spacecraft Thermal Control Handbook. Fundamental Technologies V.1 ISBN: 188498911X ISBN-13(EAN): 9781884989117 Издательство: AIAA Рейтинг: Цена: 90810.00 T Наличие на складе: Нет в наличии. 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.
Автор: Leonardo Mazzini Название: Flexible Spacecraft Dynamics, Control and Guidance ISBN: 331936877X ISBN-13(EAN): 9783319368771 Издательство: Springer Рейтинг: Цена: 121890.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers.
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: 243800.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Estimation, - Navigation.- Spacecraft Guidance, Navigation and Control
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: 87060.00 T 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).
Автор: Wertz Название: Spacecraft Attitude Determination and Control ISBN: 9027712042 ISBN-13(EAN): 9789027712042 Издательство: Springer Рейтинг: Цена: 204970.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: A comprehensive presentation of data, theory and practice in attitude analysis. It features discussions of common data anomalies, data validation, attitude hardware and associated mathematical models, and a presentation of geometrical procedures for mission analysis and attitude accuracy studies which can eliminate many complex simulations.
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