Автор: You Rui, Gao Wenjun, Wu Chunbang Название: Technologies for Spacecraft Antenna Engineering Design ISBN: 9811558329 ISBN-13(EAN): 9789811558320 Издательство: Springer Рейтинг: Цена: 25155.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Overview.- Spacecraft TT&C Antenna.- Spacecraft DTA.- Spacecraft GNSS Antenna.- Intersatellite Link Antenna.- Communication Satellite Payload Antenna.- Microwave Remote Sensing Satellite Payload Antenna.- Low Frequency Antenna and Small Satellite Antenna.- Reliability Design of Spacecraft Antenn.- Spacecraft Antenna Test Technology.- Design Case of Typical Spacecraft Antenna System.- Overview of New Technology of Spacecraft Antenna.
Описание: Spacecraft TT&C and Information Transmission Theory and Technologies introduces the basic theory of spacecraft TT&C (telemetry, track and command) and information transmission.
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
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.
Описание: This book introduces readers to the fundamentals of estimation and dynamical system theory, and their applications in the field of multi-source information fused autonomous navigation for spacecraft.
Автор: Maxwell Noton Название: Spacecraft Navigation and Guidance ISBN: 1447115856 ISBN-13(EAN): 9781447115854 Издательство: Springer Рейтинг: Цена: 15672.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: The analysis and computational techniques associated with the navigation and guidance of spacecraft are now in a mature state of development. Attention is paid to all phases of a space mission including launch and re-entry, and whether culminating in an earth satellite or a deep space mission to planets or primitive bodies.
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: NASA, George Marshall Space Flight Center, Nasa Manned Spacecraft Center Название: Saturn V Flight Manual Sa 503 ISBN: 1780398476 ISBN-13(EAN): 9781780398471 Издательство: Неизвестно Цена: 3304.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: From the foreword: "This manual was prepared to provide the astronaut with a single source reference as to the characteristics and functions of the SA-S03 launch vehicle and the AS-S03 manned flight mission. The manual provides general mission and performance data, emergency detection system information, a description of each stage and the IU, and a general discussion of ground support facilities, equipment, and mission control. A bibliography identifies additional references". This important historical reprint is profusely illustrated throughout, and a great addition to the book collections of all space flight enthusiasts.
Автор: Leonardo Mazzini Название: Flexible Spacecraft Dynamics, Control and Guidance ISBN: 331936877X ISBN-13(EAN): 9783319368771 Издательство: Springer Рейтинг: Цена: 18284.00 р. 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.
