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Author: Yasheng Zhang Publisher: Springer ISBN: 9811029482 Category : Technology & Engineering Languages : en Pages : 243
Book Description
This book focuses on the theory and design of special space orbits. Offering a systematic and detailed introduction to the hovering orbit, spiral cruising orbit, multi-target rendezvous orbit, initiative approaching orbit, responsive orbit and earth pole-sitter orbit, it also discusses the concept, theory, design methods and application of special space orbits, particularly the design and control method based on kinematics and astrodynamics. In addition the book presents the latest research and its application in space missions. It is intended for researchers, engineers and postgraduates, especially those working in the fields of orbit design and control, as well as space-mission planning and research.
Author: Yasheng Zhang Publisher: Springer ISBN: 9811029482 Category : Technology & Engineering Languages : en Pages : 243
Book Description
This book focuses on the theory and design of special space orbits. Offering a systematic and detailed introduction to the hovering orbit, spiral cruising orbit, multi-target rendezvous orbit, initiative approaching orbit, responsive orbit and earth pole-sitter orbit, it also discusses the concept, theory, design methods and application of special space orbits, particularly the design and control method based on kinematics and astrodynamics. In addition the book presents the latest research and its application in space missions. It is intended for researchers, engineers and postgraduates, especially those working in the fields of orbit design and control, as well as space-mission planning and research.
Author: George Sebestyen Publisher: Springer ISBN: 3319683152 Category : Technology & Engineering Languages : en Pages : 317
Book Description
In recent decades, the number of satellites being built and launched into Earth’s orbit has grown immensely, alongside the field of space engineering itself. This book offers an in-depth guide to engineers and professionals seeking to understand the technologies behind Low Earth Orbit satellites. With access to special spreadsheets that provide the key equations and relationships needed for mastering spacecraft design, this book gives the growing crop of space engineers and professionals the tools and resources they need to prepare their own LEO satellite designs, which is especially useful for designers of small satellites such as those launched by universities. Each chapter breaks down the various mathematics and principles underlying current spacecraft software and hardware designs.
Author: Gerald R. Hintz Publisher: Springer Nature ISBN: 3030965732 Category : Technology & Engineering Languages : en Pages : 461
Book Description
Now in an updated second edition, this classroom-tested textbook covers fundamental and advanced topics in orbital mechanics and astrodynamics designed to introduce readers to the basic dynamics of space flight. The book explains concepts and engineering tools a student or practicing engineer can apply to mission design and navigation of space missions. Through highlighting basic, analytic, and computer-based methods for designing interplanetary and orbital trajectories, the text provides excellent insight into astronautical techniques and tools. The second edition includes new material on the observational basics of orbit determination, information about precision calculations for data used inflight, such as Mars 2020 with the Ingenuity Helicopter, and improvements in mission design procedures, including the automated design of gravity-assist trajectories. Orbital Mechanics and Astrodynamics: Techniques and Tools for Space Missions is ideal for students in astronautical or aerospace engineering and related fields, as well as engineers and researchers in space industrial and governmental research and development facilities, as well as researchers in astronautics.
Author: Howard D Curtis Publisher: Elsevier ISBN: 0080887848 Category : Technology & Engineering Languages : en Pages : 744
Book Description
Orbital Mechanics for Engineering Students, Second Edition, provides an introduction to the basic concepts of space mechanics. These include vector kinematics in three dimensions; Newton’s laws of motion and gravitation; relative motion; the vector-based solution of the classical two-body problem; derivation of Kepler’s equations; orbits in three dimensions; preliminary orbit determination; and orbital maneuvers. The book also covers relative motion and the two-impulse rendezvous problem; interplanetary mission design using patched conics; rigid-body dynamics used to characterize the attitude of a space vehicle; satellite attitude dynamics; and the characteristics and design of multi-stage launch vehicles. Each chapter begins with an outline of key concepts and concludes with problems that are based on the material covered. This text is written for undergraduates who are studying orbital mechanics for the first time and have completed courses in physics, dynamics, and mathematics, including differential equations and applied linear algebra. Graduate students, researchers, and experienced practitioners will also find useful review materials in the book. NEW: Reorganized and improved discusions of coordinate systems, new discussion on perturbations and quarternions NEW: Increased coverage of attitude dynamics, including new Matlab algorithms and examples in chapter 10 New examples and homework problems
Author: Guochang Xu Publisher: Springer Science & Business Media ISBN: 3642327931 Category : Science Languages : en Pages : 444
Book Description
The development of the orbits theory lags behind the development of satellite technology. This book provides, for the first time in the history of human satellite development, the complete third order solution of the orbits under all possible disturbances. It describes the theory of satellite orbits, derives the complete solutions of the orbital disturbances, describes the algorithms of orbits determination based on the theory, describes the applications of the theory to the phenomenon of the satellite formation physically. The subjects include: Orbits Motion Equations, Disturbance theory, Solutions of the differential Equations, Algorithms of Orbits determinations, Applications of the theory to the satellite formation.
Author: Jeffrey S. Parker Publisher: John Wiley & Sons ISBN: 1118853873 Category : Technology & Engineering Languages : en Pages : 452
Book Description
Based on years of research conducted at the NASA Jet Propulsion Laboratory, Low-Energy Lunar Trajectory Design provides high-level information to mission managers and detailed information to mission designers about low-energy transfers between Earth and the moon. The book answers high-level questions about the availability and performance of such transfers in any given month and year. Low-energy lunar transfers are compared with various other types of transfers, and placed within the context of historical missions. Using this book, designers may reconstruct any transfer described therein, as well as design similar transfers with particular design parameters. An Appendix, “Locating the Lagrange Points,” and a useful list of terms and constants completes this technical reference. Surveys thousands of possible trajectories that may be used to transfer spacecraft between Earth and the moon, including transfers to lunar libration orbits, low lunar orbits, and the lunar surface Provides information about the methods, models, and tools used to design low-energy lunar transfers Includes discussion about the variations of these transfers from one month to the next, and the important operational aspects of implementing a low-energy lunar transfer Additional discussions address navigation, station-keeping, and spacecraft systems issues
Author: Oliver Montenbruck Publisher: Springer Science & Business Media ISBN: 3642583512 Category : Science Languages : en Pages : 371
Book Description
This modern presentation guides readers through the theory and practice of satellite orbit prediction and determination. Starting from the basic principles of orbital mechanics, it covers elaborate force models as well as precise methods of satellite tracking. The accompanying CD-ROM includes source code in C++ and relevant data files for applications. The result is a powerful and unique spaceflight dynamics library, which allows users to easily create software extensions. An extensive collection of frequently updated Internet resources is provided through WWW hyperlinks.
Author: John E. Prussing Publisher: Oxford University Press, USA ISBN: 9780199837700 Category : Orbital mechanics Languages : en Pages : 0
Book Description
For nearly two decades, Orbital Mechanics by John E. Prussing and Bruce A. Conway has been the most authoritative textbook on space trajectories and orbital transfers. Completely revised and updated, this edition provides: * Current data and statistics, along with coverage of new research and the most recent developments in the field * Three new chapters: "The Three-Body Problem" (Ch. 4), "Continuous-Thrust Transfer" (Ch. 8), and "Canonical Systems and the Lagrange Equations" (Ch. 12) * New material on multiple-revolution Lambert solutions, gravity-assist applications, and the state transition matrix for a general conic orbit * New examples and problems throughout * A new Companion Website with PowerPoint slides (www.oup.com/us/prussing)
Author: J.R. Wertz Publisher: Springer Science & Business Media ISBN: 9400999070 Category : Technology & Engineering Languages : en Pages : 877
Book Description
Roger D. Werking Head, Attitude Determination and Control Section National Aeronautics and Space Administration/ Goddard Space Flight Center Extensiye work has been done for many years in the areas of attitude determination, attitude prediction, and attitude control. During this time, it has been difficult to obtain reference material that provided a comprehensive overview of attitude support activities. This lack of reference material has made it difficult for those not intimately involved in attitude functions to become acquainted with the ideas and activities which are essential to understanding the various aspects of spacecraft attitude support. As a result, I felt the need for a document which could be used by a variety of persons to obtain an understanding of the work which has been done in support of spacecraft attitude objectives. It is believed that this book, prepared by the Computer Sciences Corporation under the able direction of Dr. James Wertz, provides this type of reference. This book can serve as a reference for individuals involved in mission planning, attitude determination, and attitude dynamics; an introductory textbook for stu dents and professionals starting in this field; an information source for experimen ters or others involved in spacecraft-related work who need information on spacecraft orientation and how it is determined, but who have neither the time nor the resources to pursue the varied literature on this subject; and a tool for encouraging those who could expand this discipline to do so, because much remains to be done to satisfy future needs.
Author: G Gómez Publisher: World Scientific ISBN: 9814486043 Category : Science Languages : en Pages : 692
Book Description
This book presents the state of the art in numerical and analytical techniques as well as future trends associated with mission design for libration point orbits. It contains papers explaining theoretical developments and their applications, including the accurate description of some actual libration point missions of ESA and NASA. The existing software in the field and some applications beyond the neighborhood of the Earth are also presented. Special emphasis is placed on the use of dynamical systems methodology in the libration-point-orbits mission design. Contents:Mission Analysis and Operations:Orbit Determination Issues for Libration Point Orbits (M Beckman)Libration Point Missions, 1978–2002 (D W Dunham & R W Farquhar)Herschel, Plank and GAIA Orbit Design (M Hechler & J Cobos)The SOHO Mission L1 Halo Orbit Recovery from the Attitude Control Anomalies of 1998 (C E Roberts)Dynamics Around the Libration Points:New Results on Computation of Translunar Halo Orbits of the Real Earth–Moon System (M A Andreu)Astrodynamical Applications of Invariant Manifolds Associated with Collinear Lissajous Libration Orbits (J Cobos & J J Masdemont)Halo Orbits in the Sun–Mars System (I Gacka)Libration Point Orbits: A Survey from the Dynamical Point of View (G Gómez et al.)Software Tools:Software Architexture and Use of Satellite Tool Kit's Astrogator Module for Libration Point Orbit Missions (J Carrico & E Fletcher)An Architecture for a Generalized Spacecraft Trajectory Design and Optimization System (C Ocampo)Solar System Dynamics and Applications:Restricted Four and Five Body Problems in the Solar System (F Gabern & À Jorba)One Kind of Collision Orbits Related to Lagrangian Libration Points (A E Rosaev)Statistical Theory of Interior–Exterior Transition and Collision Probabilities (S Ross)Smaller Alignment Index (SALI): Determining the Ordered or Chaotic Nature of Orbits in Conservative Dynamical Systems (Ch Skokos et al.)and other papers Readership: Researchers in aerospace engineering, mechanics, nonlinear science, chaos and dynamical systems. Keywords:Libration Point;Astrodynamics;Halo Orbits;Mission Design;Three-Body Problem;Solar System Dynamics;Trajectory Design
Author: Yasheng Zhang
Author: Yasheng Zhang
Author: George Sebestyen
Author: Gerald R. Hintz
Author: Howard D Curtis
Author: Guochang Xu
Author: Jeffrey S. Parker
Author: Oliver Montenbruck
Author: John E. Prussing
Author: J.R. Wertz
Author: G Gómez