Modern spacecraft guidance, navigation, and control,
Автор: Hall Rex, Shayler David Название: Soyuz / A Universal Spacecraft ISBN: 1852336579 ISBN-13(EAN): 9781852336578 Издательство: Springer Рейтинг: Цена: 6986.00 р. 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: Alfriend, Kyle T. Название: Spacecraft Formation Flying ISBN: 0750685336 ISBN-13(EAN): 9780750685337 Издательство: Elsevier Science Рейтинг: Цена: 16506.00 р. Наличие на складе: Поставка под заказ.
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.
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: Daniel Choukroun; Yaakov Oshman; Julie Thienel; Mo Название: Advances in Estimation, Navigation, and Spacecraft Control ISBN: 3662510049 ISBN-13(EAN): 9783662510049 Издательство: Springer Рейтинг: Цена: 32651.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Estimation, - Navigation.- Spacecraft Guidance, Navigation and Control
Автор: Leonardo Mazzini Название: Flexible Spacecraft Dynamics, Control and Guidance ISBN: 331925538X ISBN-13(EAN): 9783319255385 Издательство: Springer Рейтинг: Цена: 20896.00 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.
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.
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: 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 Название: Fault Tolerant Attitude Control Of Spacecraft ISBN: 0323898637 ISBN-13(EAN): 9780323898638 Издательство: Elsevier Science Рейтинг: Цена: 22738.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание:
Fault-Tolerant Attitude Control of Spacecraft presents the fundamentals of spacecraft fault-tolerant attitude control systems, along with the most recent research and advanced, nonlinear control techniques. This book gives researchers a self-contained guide to the complex tasks of envisaging, designing, implementing and experimenting by presenting designs for integrated modeling, dynamics, fault-tolerant attitude control, and fault reconstruction for spacecraft. Specifically, the book gives a full literature review and presents preliminaries and mathematical models, robust fault-tolerant attitude control, fault-tolerant attitude control with actuator saturation, velocity-free fault tolerant attitude control, finite-time fault-tolerant attitude tracking control, and active fault-tolerant attitude contour.
Finally, the book looks at the future of this interesting topic, offering readers a one-stop solution for those working on fault-tolerant attitude control for spacecraft.
Автор: Botelho Afonso, Parreira Baltazar, Rosa Paulo N. Название: Predictive Control for Spacecraft Rendezvous ISBN: 3030756955 ISBN-13(EAN): 9783030756956 Издательство: Springer Цена: 9083.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Introduction.- Model Predictive Control.- Relative Orbital Mechanics.- Rendezvous With Model Predictive Control.- Conclusions and Future Work.
Автор: Yang, Yaguang Название: Spacecraft Modeling, Attitude Determination, and Control ISBN: 0367780356 ISBN-13(EAN): 9780367780357 Издательство: Taylor&Francis Рейтинг: Цена: 7961.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
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: 36570.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Estimation, - Navigation.- Spacecraft Guidance, Navigation and Control
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