Автор: Spencer, David B. (the Pennsylvania State University, Usa) Conte, Davide (embry-riddle Aeronautical University, Usa) Название: Interplanetary astrodynamics ISBN: 0367759705 ISBN-13(EAN): 9780367759704 Издательство: Taylor&Francis Рейтинг: Цена: 96970.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Explores the history and significance of interplanetary space missions. Features detailed explanations and mathematical methods for trajectory optimization. Includes detailed explanations and mathematical methods for mission analysis for interplanetary missions.
Covers the introduction, mathematical methods, and applications of the N-body problem (N>2). Discusses navigation and targeting for interplanetary mission.
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)
Автор: Longuski Название: Introduction to Orbital Perturbations ISBN: 3030897605 ISBN-13(EAN): 9783030897604 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. Analytical solutions can help verify the results of numerical work, giving one confidence that his or her analysis is correct. The authors—all experienced experts in astrodynamics and space missions—take on the massive derivation problem step by step in order to help readers identify and understand possible analytical solutions in their own endeavors. The stages are elementary yet rigorous; suggested student research project topics are provided. After deriving the variational equations, the authors apply them to many interesting problems, including the Earth-Moon system, the effect of an oblate planet, the perturbation of Mercury's orbit due to General Relativity, and the perturbation due to atmospheric drag. Along the way, they introduce several useful techniques such as averaging, Poincar?'s method of small parameters, and variation of parameters. In the end, this textbook will help students, practicing engineers, and professionals across the fields of astrodynamics, astronomy, dynamics, physics, planetary science, spacecraft missions, and others. “An extensive, detailed, yet still easy-to-follow presentation of the field of orbital perturbations.” - Prof. Hanspeter Schaub, Smead Aerospace Engineering Sciences Department, University of Colorado, Boulder “This book, based on decades of teaching experience, is an invaluable resource for aerospace engineering students and practitioners alike who need an in-depth understanding of the equations they use.” - Dr. Jean Albert K?chichian, The Aerospace Corporation, Retired “Today we look at perturbations through the lens of the modern computer. But knowing the why and the how is equally important. In this well organized and thorough compendium of equations and derivations, the authors bring some of the relevant gems from the past back into the contemporary literature.” - Dr. David A Vallado, Senior Research Astrodynamicist, COMSPOC “The book presentation is with the thoroughness that one always sees with these authors. Their theoretical development is followed with a set of Earth orbiting and Solar System examples demonstrating the application of Lagrange’s planetary equations for systems with both conservative and nonconservative forces, some of which are not seen in orbital mechanics books.” - Prof. Kyle T. Alfriend, University Distinguished Professor, Texas A&M University
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: 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: 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: G?mez Название: Astrodynamics Network AstroNet-II ISBN: 3319239848 ISBN-13(EAN): 9783319239842 Издательство: Springer Рейтинг: Цена: 191560.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: These are the proceedings of the 'AstroNet-II International Final Conference'. This conference was one of the last milestones of the Marie-Curie Research Training Network on Astrodynamics 'AstroNet-II', that has been funded by the European Commission under the Seventh Framework Programme.The aim of the conference, and thus this book, is to communicate work on astrodynamics problems to an international and specialised audience. The results are presented by both members of the network and invited specialists. The topics include: trajectory design and control, attitude control, structural flexibility of spacecraft and formation flying.The book addresses a readership across the traditional boundaries between mathematics, engineering and industry by offering an interdisciplinary and multisectorial overview of the field.
Автор: Alessandro de Iaco Veris Название: Practical astrodynamics ISBN: 3319622196 ISBN-13(EAN): 9783319622194 Издательство: Springer Рейтинг: Цена: 134670.00 T Наличие на складе: Поставка под заказ. Описание: This modern textbook guides the reader through the theory and practice of the motion and attitude control of space vehicles.
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: 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.
Автор: Gуmez Gerard, Masdemont Josep J. Название: Astrodynamics Network Astronet-II: The Final Conference ISBN: 3319795643 ISBN-13(EAN): 9783319795645 Издательство: Springer Рейтинг: Цена: 204970.00 T Наличие на складе: Есть у поставщика Поставка под заказ. Описание: Leveraging discrete variational mechanics to explore the effect of an autonomous three-body interaction added to the restricted problem.- An efficient sub-optimal motion planning method for attitude manoeuvres.- Bifurcations thresholds of halo orbits.- Unconventional solar sailing.- Two-body approximations in the design of low-energy transfers between Galilean moons.- Artificial equilibria in the RTBP for a solar sail and applications.- Terminal entry phase trajectory generator for reusable launch vehicles.- Two ASRE approaches with application to spacecraft Coulomb formations.- Novel approach on the optimisation of mid-course corrections along interplanetary trajectories.- Vision-based navigation around small bodies.- Analytical and semianalytical propagation of space orbits: the role of polar-nodal variables.- Small spacecraft formation flying using solar radiation pressure.- A note on dynamics about the coherent Sun-Earth-Moon collinear libration points.- The Trojan problem from a Hamiltonian perturbative perspective.-On distributed control strategies for spacecraft formation flying.- Formation flying guidance for space debris observation, manipulation and capture.- Low thrust relative motion control of satellite formations in deep space.- Efficient modelling of small bodies gravitational potential for autonomous proximity operations.- Sun-Earth L1 and L2 to Moon transfers exploiting natural dynamics.- An introduction to differential algebra and the differential algebra manifold representation.- Identification of new orbits to enable future missions for the exploration of the Martian moon Phobos.
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