Автор: Harkins Hugh Название: Counter-Space Defence Co-Orbital Satellite Fighter: The Soviet Istrebitel Sputnik Anti-Satellite Complex ISBN: 1903630673 ISBN-13(EAN): 9781903630679 Издательство: Неизвестно Цена: 16670.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Counter-Space Defence Satellite Fighter - ASAT (Anti-Satellite) complexThe Soviet Counter-Space Defence Satellite Fighter complex was the only dedicated anti-satellite system to be operationally deployed during the Cold War. This system, which was allocated to alert duties in 1972 and attained full operational capability in 1978, served beyond the break-up of the Soviet Union in December 1991, being decommissioned by the Russian Federation in 1993.This volume sets out to detail, from the historical and technological perspectives, the Counter-Space Defence Satellite Fighter complex. The road, factual and propaganda, that led to the development of the ASAT complex is detailed, as well as the Counter-Space Defence Satellite Fighter complex itself, along with the flight test and development program leading to actual deployment of the system.At varying times throughout the text the various weapon systems discussed will be referred to under their Soviet service and or manufacturer names and designations as well as, at appropriate times, under their NATO shadow designations, the latter of course being accepted by the Soviet Union for use in arms limitations and other treaties.All technical data concerning the respective weapon systems and their components have been provided by the respective design bureau/offices, as has much of the imagery and graphics with additional impute from United States intelligence agencies and defense department, the space agencies of the Ukraine and the Russian Federation, United States National Aeronautics and Space Administration and the Ministry of Defense of the Russian Federation.
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: 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: Longuski James M., Hoots Felix R., Pollock George E. IV Название: Introduction to Orbital Perturbations ISBN: 3030897575 ISBN-13(EAN): 9783030897574 Издательство: Springer Рейтинг: Цена: 55890.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This textbook provides details of the derivation of Lagrange`s planetary equations and of the closely related Gauss`s variational equations, thereby covering a sorely needed topic in existing literature.
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: H. jr. Oertel; H. K?rner Название: Orbital Transport ISBN: 3642457223 ISBN-13(EAN): 9783642457227 Издательство: Springer Рейтинг: Цена: 93160.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Third Aerospace Symposium, Braunschweig 26.-28.August 1991
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: 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: 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: Liu Название: Algorithms for Satellite Orbital Dynamics ISBN: 9811948380 ISBN-13(EAN): 9789811948381 Издательство: Springer Рейтинг: Цена: 60550.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: This book highlights the fundamental physics of orbit theory, dynamical models, methods of orbit determination, design, measurement, adjustment, and complete calculations for the position, tracking, and prediction of satellites and deep spacecraft. It emphasizes specific methods, related mathematical calculations, and worked examples and exercises. Therefore, technicians and engineers in the aerospace industry can directly apply them to their practical work. Dedicated to undergraduate students and graduate students, researchers, and professionals in astronomy, physics, space science, and related aerospace industries, the book is an integrated work based on the accumulated knowledge in satellite orbit dynamics and the author’s more than five decades of personal research and teaching experience in astronomy and aerospace dynamics.
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.
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)
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