Spacecraft Thermal Control Technologies, Miao Jianyin, Zhong Qi, Zhao Qiwei
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.
Автор: Chen Qi, Liu Zhigang, Zhang Xiaofeng Название: Spacecraft Power System Technologies ISBN: 9811548382 ISBN-13(EAN): 9789811548383 Издательство: Springer Рейтинг: Цена: 25155.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This book provides an introduction to the main design principles, methods, procedures, and development trends in spacecraft power systems. The book`s closing chapters provide essential information on new power systems and technologies, such as space nuclear power, micro- and nano-satellite power systems, and space energy interconnection systems.
Автор: Zhang Hua, Zhang Yuting, Huang Chengbo Название: Spacecraft Electromagnetic Compatibility Technologies ISBN: 9811547815 ISBN-13(EAN): 9789811547812 Издательство: Springer Рейтинг: Цена: 22359.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This book explores key techniques and methods in electromagnetic compatibility management, analysis, design, improvement and test verification for spacecraft.
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: You Rui, Gao Wenjun, Wu Chunbang Название: Technologies for Spacecraft Antenna Engineering Design ISBN: 9811558353 ISBN-13(EAN): 9789811558351 Издательство: Springer 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.
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.
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: 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.
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: Zhang Hua, Zhang Yuting, Huang Chengbo Название: Spacecraft Electromagnetic Compatibility Technologies ISBN: 981154784X ISBN-13(EAN): 9789811547843 Издательство: Springer Цена: 22359.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This book explores key techniques and methods in electromagnetic compatibility management, analysis, design, improvement and test verification for spacecraft.
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: Chen Qi, Liu Zhigang, Zhang Xiaofeng Название: Spacecraft Power System Technologies ISBN: 9811548412 ISBN-13(EAN): 9789811548413 Издательство: Springer Цена: 25155.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This book provides an introduction to the main design principles, methods, procedures, and development trends in spacecraft power systems. The book`s closing chapters provide essential information on new power systems and technologies, such as space nuclear power, micro- and nano-satellite power systems, and space energy interconnection systems.
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