Dynamics and Design of Space Nets for Orbital Capture, Yang Leping, Zhang Qingbin, Zhen Ming
Автор: Jianping Yuan; Yu Cheng; Jinglang Feng; Chong Sun Название: Low Energy Flight: Orbital Dynamics and Mission Trajectory Design ISBN: 9811361290 ISBN-13(EAN): 9789811361296 Издательство: Springer Рейтинг: Цена: 139750.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание:
The book focuses on the orbital dynamics and mission trajectory (transfer or target trajectory) design of low-energy flight in the context of modern astrodynamics. It investigates various topics that either offer new methods for solving classical problems or address emerging problems that have yet to be studied, including low-thrust transfer trajectory design using the virtual gravity field method; transfer in the three-body system using invariant manifolds; formation flying under space-borne artificial magnetic fields; and the orbital dynamics of highly irregular asteroids. It also features an extensive study of the orbital dynamics in the vicinity of contact binary asteroids, including the 1:1 ground-track resonance, the equilibrium points and their stability, and the third-order analytical solution of orbital motion in the vicinity of the non-collinear equilibrium point.
Given its breadth of coverage, the book offers a valuable reference guide for all engineers and researchers interested in the potential applications of low-energy space missions.
Автор: Leping Yang; Qingbin Zhang; Ming Zhen; Haitao Liu Название: Dynamics and Design of Space Nets for Orbital Capture ISBN: 3662540622 ISBN-13(EAN): 9783662540626 Издательство: Springer Рейтинг: Цена: 111790.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book covers the topics of theoretical principles, dynamics model and algorithm, mission analysis, system design and experimental studies of space nets system, aiming to provide an initial framework in this field and serve as a ready reference for those interested.
Автор: Yu Yang Название: Orbital Dynamics in the Gravitational Field of Small Bodies ISBN: 366257070X ISBN-13(EAN): 9783662570708 Издательство: Springer Рейтинг: Цена: 93160.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This prizewinning PhD thesis presents a general discussion of the orbital motion close to solar system small bodies (SSSBs), which induce non-central asymmetric gravitational fields in their neighborhoods.
Автор: Yang Yu Название: Orbital Dynamics in the Gravitational Field of Small Bodies ISBN: 3662526913 ISBN-13(EAN): 9783662526910 Издательство: Springer Рейтинг: Цена: 95770.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This prizewinning PhD thesis presents a general discussion of the orbital motion close to solar system small bodies (SSSBs), which induce non-central asymmetric gravitational fields in their neighborhoods.
Автор: Chen Lei, Bai Xian-Zong, Liang Yan-Gang Название: Orbital Data Applications for Space Objects: Conjunction Assessment and Situation Analysis ISBN: 9811097526 ISBN-13(EAN): 9789811097522 Издательство: Springer Рейтинг: Цена: 93160.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book introduces readers to the application of orbital data on space objects in the contexts of conjunction assessment and space situation analysis, including theories and methodologies.
Автор: Lei Chen; Xian-Zong Bai; Yan-Gang Liang; Ke-Bo Li Название: Orbital Data Applications for Space Objects ISBN: 9811029628 ISBN-13(EAN): 9789811029622 Издательство: Springer Рейтинг: Цена: 139750.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book introduces readers to the application of orbital data on space objects in the contexts of conjunction assessment and space situation analysis, including theories and methodologies. It addresses the main topics involved in space object conjunction assessment, such as: orbital error analysis of space objects; close approach analysis; the calculation, analysis and application of collision probability; and the comprehensive assessment of collision risk. In addition, selected topics on space situation analysis are also presented, including orbital anomaly and space event analysis, and so on. The book offers a valuable guide for researchers and engineers in the fields of astrodynamics, space telemetry, tracking and command (TT&C), space surveillance, space situational awareness, and space debris, as well as for graduates majoring in flight vehicle design and related fields.
Автор: Tabor Jean Название: Deciphering Spacecraft Systems and Orbital Calculations ISBN: 1632401355 ISBN-13(EAN): 9781632401359 Издательство: Неизвестно Цена: 128690.00 T Наличие на складе: Есть у поставщика Поставка под заказ.
Автор: Daniel J. Scheeres Название: Orbital Motion in Strongly Perturbed Environments ISBN: 3642431631 ISBN-13(EAN): 9783642431630 Издательство: Springer Рейтинг: Цена: 121890.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: The investigation of minor solar system bodies, such as comets and asteroids, using spacecraft requires an understanding of orbital motion in strongly perturbed environments. The solutions to a wide range of complex and challenging problems in this field are reviewed in this comprehensive and authoritative work.
Автор: Xuefeng Li; Chaobing Li Название: Navigation and Guidance of Orbital Transfer Vehicle ISBN: 9811348588 ISBN-13(EAN): 9789811348587 Издательство: Springer Рейтинг: Цена: 107130.00 T Наличие на складе: Поставка под заказ. Описание: This book uses the entire flying process, starting from ground launching of the orbital transfer vehicle (OTV) to injecting payload into earth synchronous orbit, as an example for real-world engineering practices. It discusses in detail the analysis design and integrated OTV navigation and guidance system technologies in combination with the engineering experiences of the authors in analysis, design and integrated OTV navigation and guidance system applications, and the research on navigation and guidance theories. It focuses on establishing motion of air vehicle equations, control system hardware components, orbit prediction technology, inertial navigation and initial alignment technologies, INS/GNSS integrated navigation technologies, INS/CNS integrated navigation technologies, redundant fault tolerance and failure reconfiguration technology of inertial sensors, guidance and midcourse correction technologies and orbit control strategies. The book is a valuable reference book for the engineers, technicians and researchers who are engaged in analysis, design and integrated application of OTV navigation and guidance control systems. It can also be used as teaching material for postgraduates and senior undergraduates majoring in OTV navigation and guidance systems and other related subjects.
Автор: D.Subbaram Naidu Название: Aeroassisted Orbital Transfer ISBN: 3540198199 ISBN-13(EAN): 9783540198192 Издательство: Springer Рейтинг: Цена: 81050.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Aeroassisting, or aerobraking, opens new opportunities for space missions, particularly with regard to the establishment of permanent space stations and long-distance space exploration. This monograph explores major areas of research in the field.
Автор: Audrey L. Allison Название: The ITU and Managing Satellite Orbital and Spectrum Resources in the 21st Century ISBN: 3319053132 ISBN-13(EAN): 9783319053134 Издательство: Springer Рейтинг: Цена: 60940.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Access to satellite orbits and spectrum is managed by the ITU, a United Nations body that strives to extend the benefits of new technologies to the world, while ensuring equitable access to these resources.
Автор: Javier Roa Название: Regularization in Orbital Mechanics: Theory and Practice ISBN: 3110558556 ISBN-13(EAN): 9783110558555 Издательство: Walter de Gruyter Цена: 140090.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание:
Regularized equations of motion can improve numerical integration for the propagation of orbits, and simplify the treatment of mission design problems. This monograph discusses standard techniques and recent research in the area. While each scheme is derived analytically, its accuracy is investigated numerically. Algebraic and topological aspects of the formulations are studied, as well as their application to practical scenarios such as spacecraft relative motion and new low-thrust trajectories.
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