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Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods, Xie Yongchun, Chen Changqing, Liu Tao


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Автор: Xie Yongchun, Chen Changqing, Liu Tao
Название:  Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods
ISBN: 9789811569890
Издательство: Springer
Классификация:

ISBN-10: 9811569894
Обложка/Формат: Hardcover
Страницы: 495
Вес: 0.88 кг.
Дата издания: 17.02.2021
Язык: English
Размер: 23.39 x 15.60 x 2.87 cm
Ссылка на Издательство: Link
Поставляется из: Германии
Описание: This book focuses on the theory and design methods for guidance, navigation, and control (GNC) in the context of spacecraft rendezvous and docking (RVD). Emphasis is placed on the design method of active and passive trajectory protection in different phases of RVD, and on the safety design of the RVD mission as a whole.


Orbital Relative Motion and Terminal Rendezvous: Analytic and Numerical Methods for Spaceflight Guidance Applications

Автор: Kйchichian Jean Albert
Название: Orbital Relative Motion and Terminal Rendezvous: Analytic and Numerical Methods for Spaceflight Guidance Applications
ISBN: 3030646564 ISBN-13(EAN): 9783030646561
Издательство: Springer
Цена: 18167.00 р.
Наличие на складе: Есть у поставщика Поставка под заказ.

Описание:

Chapter 1. The Second-Order Analytic Approximation to the Solution of the Euler-Hill Equations of Relative Motion.- Chapter 2. Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influence of the J2 and J3 Earth Zonal Harmonics, in Rotating and Inertial Cartesian Reference Frames.- Chapter 3. Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influence of the Luni-Solar Gravity, in Rotating and Inertial Cartesian Reference Frames.- Chapter 4. Effect of Luni-Solar Gravity Perturbations on a Near-Circular Orbit: Third-Body Orbit Eccentricity Considerations.- Chapter 5. Effect of Atmospheric Drag Perturbation on Circular Orbits: Atmosphere Rotation Considerations.- Chapter 6. Analytic Solution of Terminal Rendezvous in Near-Circular Orbit Around the Oblate Earth: The Computation of the Starting Guess for Iterations.- Chapter 7. Techniques of Accurate Analytic Terminal Rendezvous in Near-Circular Orbit.- Chapter 8. Coplanar Two-Impulse Rendezvous in General Elliptic Orbit with Drag.- Chapter 9. The Analysis of the Relative Motion in General Elliptic Orbit With Respect to a Dragging and Precessing Coordinate Frame.- Chapter 10. The Algorithm of the Two-Impulse Time-Fixed Noncoplanar Rendezvous with Drag and Oblateness Effects.- Chapter 11. The Analysis and Implementation of In-Plane Stationkeeping of Continuously Perturbed Walker Constellations.- Chapter 12. The Mathematical Models of the Jet Propulsion Laboratory (JPL) Artificial Satellite Analysis Program (ASAP)

Fundamentals of Spacecraft Attitude Determination and Control

Автор: F. Landis Markley; John L. Crassidis
Название: Fundamentals of Spacecraft Attitude Determination and Control
ISBN: 1493908014 ISBN-13(EAN): 9781493908011
Издательство: Springer
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Цена: 12577.00 р.
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Описание: It provides detailed derivations for attitude kinematics and dynamics and provides detailed description of the most widely used attitude parameterization, the quaternion.

Advances in Estimation, Navigation, and Spacecraft Control

Автор: Daniel Choukroun; Yaakov Oshman; Julie Thienel; Mo
Название: Advances in Estimation, Navigation, and Spacecraft Control
ISBN: 3662510049 ISBN-13(EAN): 9783662510049
Издательство: Springer
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Цена: 32651.00 р.
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Описание: Estimation, - Navigation.- Spacecraft Guidance, Navigation and Control

Flexible Spacecraft Dynamics, Control and Guidance

Автор: Leonardo Mazzini
Название: Flexible Spacecraft Dynamics, Control and Guidance
ISBN: 331936877X ISBN-13(EAN): 9783319368771
Издательство: Springer
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Цена: 18284.00 р.
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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.

Spacecraft Autonomous Navigation Technologies Based on Multi-Source Information Fusion

Автор: Wang Dayi, Li Maodeng, Huang Xiangyu
Название: Spacecraft Autonomous Navigation Technologies Based on Multi-Source Information Fusion
ISBN: 9811548811 ISBN-13(EAN): 9789811548819
Издательство: Springer
Цена: 30745.00 р.
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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.

Predictive Control for Spacecraft Rendezvous

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.
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Описание: Introduction.- Model Predictive Control.- Relative Orbital Mechanics.- Rendezvous With Model Predictive Control.- Conclusions and Future Work.

Spacecraft Dynamics and Control

Автор: Canuto, Enrico
Название: Spacecraft Dynamics and Control
ISBN: 0081007000 ISBN-13(EAN): 9780081007006
Издательство: Elsevier Science
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Цена: 20043.00 р.
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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
Control Allocation for Spacecraft Under Actuator Faults

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.
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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.

Spacecraft Navigation and Guidance

Автор: Maxwell Noton
Название: Spacecraft Navigation and Guidance
ISBN: 1447115856 ISBN-13(EAN): 9781447115854
Издательство: Springer
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Цена: 15672.00 р.
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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.

Advances in Estimation, Navigation, and Spacecraft Control

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.
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Описание: Estimation, - Navigation.- Spacecraft Guidance, Navigation and Control

Guidance and Control Technology of Spacecraft on Elliptical Orbit

Автор: Liu
Название: Guidance and Control Technology of Spacecraft on Elliptical Orbit
ISBN: 9811079587 ISBN-13(EAN): 9789811079580
Издательство: Springer
Рейтинг:
Цена: 16769.00 р.
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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.

Guidance and Control Technology of Spacecraft on Elliptical Orbit

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.
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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.


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