Orbital mechanics
Annotation
Saved in:
| Other Authors: | |
|---|---|
| Format: | eBook |
| Language: | English |
| Published: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
©2002.
|
| Edition: | 3rd ed. |
| Series: | AIAA education series.
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| Subjects: | |
| ISBN: | 9781601192080 1601192088 1563475375 9781563475375 9781600860973 1600860974 |
| Physical Description: | 1 online resource (xv, 460 pages) : illustrations |
Cover
Table of contents
| LEADER | 06526cam a2200541 a 4500 | ||
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| 003 | OCoLC | ||
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| 008 | 070425s2002 vaua ob 001 0 eng d | ||
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| 020 | |a 9781563475375 | ||
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| 020 | |a 1600860974 |q (e-book) | ||
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| 020 | |z 9781563475375 |q (hardcover ; |q alk. paper) | ||
| 024 | 3 | |a 9781563475375 | |
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| 245 | 0 | 0 | |a Orbital mechanics / |c edited by Vladimir A. Chobotov. |
| 250 | |a 3rd ed. | ||
| 260 | |a Reston, Va. : |b American Institute of Aeronautics and Astronautics, |c ©2002. | ||
| 300 | |a 1 online resource (xv, 460 pages) : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a AIAA education series | |
| 504 | |a Includes bibliographical references and index. | ||
| 506 | |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty | ||
| 520 | 8 | |a Annotation |b Designed to be used as a graduate student textbook and a ready reference for the busy professional, this third edition of "Orbital Mechanics is structured so that you can easily look up the things you need to know. This edition includes more recent developments in space exploration (e.g. Galileo, Cassini, Mars Odyssey missions). Also, the chapter on space debris was rewritten to reflect new developments in that area. The well-organized chapters cover every basic aspect of orbital mechanics, from celestial relationships to the problems of space debris. The book is clearly written in language familiar to aerospace professionals and graduate students, with all of the equations, diagrams, and graphs you would like to have close at hand. An updated software package on CD-ROM includes: HW Solutions, which presents a range of viewpoints and guidelines for solving selected problems in the text; Orbital Calculator, which provides an interactive environment for the generation of Keplerian orbits, orbital transfer maneuvers, and animation of ellipses, hyperbolas, 'and interplanetary orbits; and Orbital Mechanics Solutions | |
| 505 | 0 | |a Cover -- Title -- Copyright -- Foreword -- Preface -- About the Authors -- Table of Contents -- Chapter 1. Basic Concepts -- 1.1 A Historical Perspective -- 1.2 Velocity and Acceleration -- Problems -- Selected Solutions -- Chapter 2. Celestial Relationships -- 2.1 Coordinate Systems -- 2.2 Time Systems -- References -- Chapter 3. Keplerian Orbits -- 3.1 Newton's Universal Law of Gravitation -- 3.2 General and Restricted Two-Body Problem -- 3.3 Conservation of Mechanical Energy -- 3.4 Conservation of Angular Momentum | |
| 505 | 8 | |a 3.5 Orbital Parameters of a Satellite3.6 Orbital Elements -- References -- Problems -- Selected Solutions -- Chapter 4. Position and Velocity as a Function of Time -- 4.1 General Relationships -- 4.2 Solving Kepler's Equation -- 4.3 A Universal Approach -- 4.4 Expressions with f and g -- 4.5 Summary of the Universal Approach -- 4.6 The Classical Element Set -- 4.7 The Rectangular Coordinate System -- 4.8 Modified Classical to Cartesian Transformation -- 4.9 Rectangular to Modified Classical Elements Transformation | |
| 505 | 8 | |a 4.10 The Spherical (ADBARV) Coordinate System4.11 Rectangular to Spherical Transformation -- 4.12 Spherical to Rectangular Transformation -- 4.13 The Earth-Relative Spherical (LDBARV) Coordinate System -- 4.14 Geodetic and Geocentric Altitudes -- 4.15 Converting from Perigee/Apogee Radii to Perigee/Apogee Altitudes -- 4.16 Converting from Perigee/Apogee Altitudes to Perigee/Apogee Radii -- References -- Problems -- Selected Solutions -- Chapter 5. Orbital Maneuvers -- 5.1 Orbital Energy -- 5.2 Single-Impulse Maneuvers | |
| 505 | 8 | |a 5.3 Single- and Two-Impulse Transfer Comparison for Coplanar Transfers Between Elliptic Orbits That Differ Only in Their Apsidal Orientation5.4 Hohmann Transfer -- 5.5 The Bi-elliptic Transfer -- 5.6 Restricted Three-Impulse Plane Change Maneuver for Circular Orbits -- 5.7 General Three-Impulse Plane Change Maneuver for Circular Orbit -- 5.8 Hohmann Transfer with Split-Plane Change -- 5.9 Bi-elliptic Transfer with Split-Plane Change -- 5.10 Transfer Between Coplanar Elliptic Orbits -- References -- Problems -- Selected Solutions | |
| 505 | 8 | |a Chapter 6. Complications to Impulsive Maneuvers6.1 N-Impulse Maneuvers -- 6.2 Fixed-Impulse Transfers -- 6.3 Finite-Duration Burns: Gravity Losses -- 6.4 Very Low Thrust Transfers -- References -- Problems -- Selected Solutions -- Chapter 7. Relative Motion in Orbit -- 7.1 Space Rendezvous -- 7.2 Terminal Rendezvous -- 7.3 Applications of Rendezvous Equations -- 7.4 An Exact Analytical Solution for Two-Dimensional Relative Motion -- 7.5 Optimal Multiple-Impulse Rendezvous -- References -- Problems -- Selected Solutions | |
| 590 | |a Knovel |b Knovel (All titles) | ||
| 650 | 0 | |a Orbital mechanics. | |
| 650 | 0 | |a Artificial satellites |x Orbits. | |
| 650 | 0 | |a Navigation (Astronautics) | |
| 655 | 7 | |a elektronické knihy |7 fd186907 |2 czenas | |
| 655 | 9 | |a electronic books |2 eczenas | |
| 700 | 1 | |a Chobotov, Vladimir A. | |
| 776 | 0 | 8 | |i Print version: |t Orbital mechanics. |b 3rd ed. |d Reston, Va. : American Institute of Aeronautics and Astronautics, ©2002 |z 1563475375 |w (DLC) 2002008309 |w (OCoLC)49923275 |
| 830 | 0 | |a AIAA education series. | |
| 856 | 4 | 0 | |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpOME00001/orbital-mechanics-3rd?kpromoter=marc |y Full text |
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