Описание: * Unique focus on spacecraft and satellite reliability based on statistical analysis of mission failures and successes.
Автор: Kyle T. Alfriend Название: Spacecraft Formation Flying, ISBN: 0750685336 ISBN-13(EAN): 9780750685337 Издательство: Elsevier Science Цена: 11077 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Space agencies are now realizing that much of what has previously been achieved using hugely complex and costly single platform projects—large unmanned and manned satellites (including the present International Space Station)—can be replaced by a number of smaller satellites networked together. The key challenge of this approach, namely ensuring the proper formation flying of multiple craft, is the topic of this second volume in Elsevier’s Astrodynamics Series, Spacecraft Formation Flying: Dynamics, control and navigation.In this unique text, authors Alfriend et al. provide a coherent discussion of spacecraft relative motion, both in the unperturbed and perturbed settings, explain the main control approaches for regulating relative satellite dynamics, using both impulsive and continuous maneuvers, and present the main constituents required for relative navigation. The early chapters provide a foundation upon which later discussions are built, making this a complete, standalone offering.Intended for graduate students, professors and academic researchers in the fields of aerospace and mechanical engineering, mathematics, astronomy and astrophysics, Spacecraft Formation Flying is a technical yet accessible, forward-thinking guide to this critical area of astrodynamics.
Описание: The definitive reference for space engineers on all issues related to rendezvous and docking/berthing (RVD/B).
Автор: Patel Название: Spacecraft Power Systems ISBN: 0849327865 ISBN-13(EAN): 9780849327865 Издательство: Taylor&Francis Рейтинг: Цена: 28582 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Presents information on the various aspects of spacecraft power system design, analysis, and operation for various types of spacecrafts: earth-orbiting, interplanetary, and deep-space. This work presents modern data and procedures for designing electrical power systems that meet mission requirements at a minimum cost and weight.
Описание: Mission Geometry; Orbit and Constellation Design and Management (OCDM) is the most complete treatment available for many elements of space mission design and astronautics. Among these topics not covered elsewhere in the literature are:
The most extensive coverage available of constellation design and management;
Relative motion of satellites (global, local, at similar and widely differing altitudes);
Definition of an Orbit CostFunction for comparing the cost of access to and maintenance of alternative orbits;
Most extensive discussions available of autonomous navigation and autonomous orbit control;
The most complete discussion available of Earth coverage and viewing andlighting conditions;
Apparent motion of other satellites needed for cross-link pointing and antenna coverage;
Analytic expressions for the field of view of an array processor on the celestial sphere and projected onto the Earth's surface;
Detailed process for creating and analyzing mapping, pointing, and timing budgets;
Closed-form expressions for the ground track of a circular orbit, including high accuracy approximations for ground station coverage;
Convenient formulas for specialized orbits about the Earth and other planets;
Practical spacecraft problems such as time discontinuities, GPS coverage at satellite altitudes, and how to identify and handle singularities in measurement sets; and
New solutions for all possible spherical triangles without quadrant ambiguities and allowing all sides and angles to range from 0 to 360 deg.
OCDM discusses both the similarities and differences between orbit and altitude systems in terms of hardware, algorithms, design, and processing requirements. With the demand for reduced cost and the introduction of extensive on-board computing, what were once entirely separate disciplines have begun to merge. This volume will speed that process.
In all areas, OCDM is meant to be practical, with recommendations, insights, formulas, and numerical recipes based on 40 years of spaceflight experience from organizations worldwide. It is meant to be both a text and reference work that can be used by those entering the field and by senior engineers engaged in the design, analysis, construction, or on-orbit operations of orbit and attitude systems and components.
Описание: The revised edition of this practical, hands-on book discusses the range of launch vehicles in use today throughout the world, and includes the very latest details of some of the advanced propulsion systems currently being developed. The author covers the fundamentals of the subject, from the basic principles of rocket propulsion and vehicle dynamics through the theory and practice of liquid and solid propellant motors, to new and future developments.The revised edition will stick to the same principle of providing a serious exposition of the principles and practice of rocket propulsion, but from the point of view of the user and enquirer who is not an engineering specialist. Most chapters will remain substantially the same as the first edition; they will be updated where necessary and errata corrected. The main revisions will be to the chapter on electric propulsion where there have been significant new developments both in engine types and in practical applications. This is now seen as the key to planetary exploration by robotic probes and should therefore be reflected. Nuclear propulsion has emerged from the doldrums and is now seen as a definite possibility for outer solar system robotic exploration; and as enabling technology for a human mars expedition. A new chapter on nuclear thermal propulsion has been added to reflect this revival of interest.
Автор: Wijker Jaap Название: Mechanical Vibrations in Spacecraft Design ISBN: 3540405305 ISBN-13(EAN): 9783540405306 Издательство: Springer Рейтинг: Цена: 13672 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: All typical and special modal and response analysis methods, applied within the frame of the design of spacecraft structures, are described in this book. It therefore addresses graduate students and engineers in the aerospace field.
Автор: Wijker Название: Spacecraft Structures ISBN: 3540755527 ISBN-13(EAN): 9783540755524 Издательство: Springer Рейтинг: Цена: 22989 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Space flight encompasses many fields of technology. This monograph presents a cross section of the total field of expertise that is called "space flight". It provides insight into the design, construction and analysis aspects of spacecraft. Spacecraft includes satellites as well as launch vehicles, with a distinction between manned or unmanned.
Автор: Martin J. L. Turner Название: Rocket and Spacecraft Propulsion ISBN: 3642088694 ISBN-13(EAN): 9783642088698 Издательство: Springer Рейтинг: Цена: 16601 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: The revised third edition of this eminently practical, hands-on book discusses the range of launch vehicles in use today throughout the world, and includes the very latest details of some of the advanced propulsion systems currently being developed.
Описание: Provides the basics of spacecraft orbital dynamics plus attitude dynamics and control, using vectrix notation Spacecraft Dynamics and Control: An Introduction presents the fundamentals of classical control in the context of spacecraft attitude control.
Автор: Lai, Shu T. Название: Fundamentals of spacecraft charging ISBN: 0691129479 ISBN-13(EAN): 9780691129471 Издательство: Wiley Рейтинг: Цена: 10164 р. Наличие на складе: Поставка под заказ.
Описание: Covers various aspects of the field of spacecraft charging, ranging from secondary and backscattered electrons, spacecraft charging in Maxwellian plasmas, effective mitigation techniques, and potential wells and barriers to operational anomalies, meteors, and neutral gas release.
Автор: Conway Название: Spacecraft Trajectory Optimization ISBN: 0521518504 ISBN-13(EAN): 9780521518505 Издательство: Cambridge Academ Рейтинг: Цена: 11273 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This is a long-overdue volume dedicated to space trajectory optimization. Interest in the subject has grown, as space missions of increasing levels of sophistication, complexity, and scientific return - hardly imaginable in the 1960s - have been designed and flown. Although the basic tools of optimization theory remain an accepted canon, there has been a revolution in the manner in which they are applied and in the development of numerical optimization. This volume purposely includes a variety of both analytical and numerical approaches to trajectory optimization. The choice of authors has been guided by the editor's intention to assemble the most expert and active researchers in the various specialities presented. The authors were given considerable freedom to choose their subjects, and although this may yield a somewhat eclectic volume, it also yields chapters written with palpable enthusiasm and relevance to contemporary problems.
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