Описание: This book develops a dynamical model of the orbital motion of Lorentz spacecraft in both unperturbed and J2-perturbed environments. It explicitly discusses three kinds of typical space missions involving relative orbital control: spacecraft hovering, rendezvous, and formation flying. Subsequently, it puts forward designs for both open-loop and closed-loop control schemes propelled or augmented by the geomagnetic Lorentz force. These control schemes are entirely novel and represent a significantly departure from previous approaches.
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: P.W. Likins; R.E. Roberson; J. Wittenburg Название: Dynamics of Flexible Spacecraft ISBN: 3211811990 ISBN-13(EAN): 9783211811993 Издательство: Springer Рейтинг: Цена: 14365.00 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: 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: Frederick A. Leve; Brian J. Hamilton; Mason A. Pec Название: Spacecraft Momentum Control Systems ISBN: 3319361740 ISBN-13(EAN): 9783319361741 Издательство: Springer Рейтинг: Цена: 13059.00 р. 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).
Описание: 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.
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.
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: 10447.00 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
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: 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.
ООО "Логосфера " Тел:+7(495) 980-12-10 www.logobook.ru
