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Fundamentals of astrodynamics (Record no. 1005)

MARC details
000 -LEADER
fixed length control field	05199 a2200265 4500
005 - DATE AND TIME OF LATEST TRANSACTION
control field	20250417110406.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field	240426b2020\|\|\|\|\|\|\|\| \|\|\|\| 00\| 0 eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN	9780486497044
041 ## - LANGUAGE CODE
Language code of text/sound track or separate title	English
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number	629.411 B38, 2
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name	Bate, Roger R.
Relator term	Author
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name	Mueller, Donald D.
Relator term	Co-Author
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name	White, Jerry E.
Relator term	Co-Author
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name	Saylor, William W.
Relator term	Co-Author
245 ## - TITLE STATEMENT
Title	Fundamentals of astrodynamics
250 ## - EDITION STATEMENT
Edition statement	2nd ed.
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Name of publisher	Dover Publications,
Place of publication	New York:
Year of publication	2020.
300 ## - PHYSICAL DESCRIPTION
Number of Pages	xii, 416p.; 24cms.
500 ## - GENERAL NOTE
General note	Developed at the U.S. Air Force Academy, this teaching text is widely known and used throughout the astrodynamics and aerospace engineering communities. Completely revised and updated, this second edition takes into account new developments of the past four decades, especially regarding information technology. Central emphasis is placed on the use of the universal variable formulation, although classical methods are also discussed. The development of the basic two-body and n-body equations of motion serves as a foundation for all that follows. Subsequent topics include orbit determination and the classical orbital elements, coordinate transformations, and differential correction. The Kepler and Gauss problems are treated in detail, and two-body mechanics are applied to the ballistic missile problem. Perturbations, integration schemes and error, and analytic formulations of several common perturbations are introduced. Example problems and exercises appear throughout the text, along with photographs, diagrams, and drawings. Four helpful appendixes conclude the book.<br/><br/>Table of contents:<br/><br/>Preface<br/>About the Authors<br/>Chapter 1 Two-Body Orbital Mechanics<br/>1.1 Historical Background and Basic Laws<br/>1.2 Basic Laws 1<br/>1.3 The N-Body Problem <br/>1.4 The Two-Body Problem <br/>1.5 Constants of Motion<br/>1.6 The Trajectory Equation <br/>1.7 Relating E and h to the Geometry of an Orbit<br/>1.8 The Elliptical Orbit <br/>1.9 The Circular Orbit <br/>1.10 The Parabolic Orbit <br/>1.11 The Hyperbolic Orbit<br/>1.12 Canonical Units<br/>Chapter 2 Orbit Determination from Observations <br/>2.1 Historical Background <br/>2.2 Coordinate Systems <br/>2.3 Classical Orbital Elements <br/>2.4 Determining the Orbital Elements from r and v <br/>2.5 Determining r and v from the Orbital Elements <br/>2.6 Coordinate Transformations <br/>2.7 Orbit Determination from a SingularRadar Observation <br/>2.8 SEZ to IJK Transformation Using an Ellipsoid Earth Model <br/>2.9 The Measurement of Time<br/>2.10 Orbit Determination from Three Position Vectors <br/>2.11 Orbit Determination from Optical Sightings <br/>2.12 Improving a Preliminary Orbit by Differential Correct<br/>2.13 Space Surveillance <br/>2.14 Ground Track of a Satellite <br/>Chapter 3 Basic Orbital Maneuvers <br/>3.1 Historical Background <br/>3.2 Low-Altitude Earth Orbits <br/>3.3 High-Altitude Earth Orbits <br/>3.4 In-Plane Orbit Changes<br/>3.5 Out-of-Plane Orbit Changes <br/>Chapter 4 Position and Velocity as a Function of Time <br/>4.1 Historical Background <br/>4.2 Time-of-Flight as a Function of<br/>Eccentric Anomaly<br/>4.3 A Universal Formulation for Time-of-Flight <br/>4.4 The Prediction Problem <br/>4.5 Implementing the Universal Variable Formulation <br/>4.6 Classical Formulations of the Kepler Problem <br/>Chapter 5 Orbit Determination from Two Positions and Time <br/>5.1 Historical Background <br/>5.2 The Gauss Problem—General Methods of Solution <br/>5.3 Solutions of the Gauss Problem via Universal Variables <br/>5.4 The p-Iteration Method <br/>5.5 The Gauss Problem Using the f and g Series <br/>5.6 The Original Gauss Method<br/>5.7 Practical Applications of the Gauss Problem—Intercept and Rendezvous<br/>5.8 Determination of Orbit from<br/>Sighting Directions at Station <br/>Chapter 6 Ballistic Missile Trajectories <br/>6.1 Historical Background <br/>6.2 The General Ballistic Missile Problem <br/>6.3 Effect of Launching Errors on Range <br/>6.4 The Effect of Earth Rotation <br/>Chapter 7 Lunar Trajectories <br/>7.1 Historical Background <br/>7.2 The Earth-Moon System <br/>7.3 Simple Earth-Moon Trajectories <br/>7.4 The Patched-Conic Approximation<br/>7.5 Noncoplanar Lunar Trajectories <br/>Chapter 8 Interplanetary Trajectories <br/>8.1 Historical Background<br/>8.2 The Solar System<br/>8.3 The Patched-Conic Approximation <br/>8.4 Noncoplanar Interplanetary Trajectories <br/>8.5 Planetary Flybys<br/>Chapter 9 Perturbations <br/>9.1 Historical Background <br/>9.2 Cowell’s Method<br/>9.3 Encke’s Method<br/>9.4 Variation of Parameters or Elements <br/>9.5 Comments on Integration Schemes and Errors <br/>9.6 Numerical Integration Methods <br/>9.7 Analytic Formulations of Perturbative Accelerations <br/>Chapter 10 Special Topics<br/>10.1 Historical Background <br/>10.2 General Perturbation Models <br/>10.3 NORAD Propagators and Two-Line Element Sets <br/>10.4 Relative Motion of Satellites<br/>Appendix A Astrodynamic Constants<br/>Appendix B Vector Review <br/>B.1 Definitions<br/>B.2 Vector Operations <br/>B.3 Velocity<br/>Appendix C Gauss Problem <br/>Appendix D Proposed Three-Line Element Set<br/>Definition
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term	Orbital mechanics
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term	Position and Velocity as a Function of Time
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term	Relating E and h to the Geometry of an Orbit
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term	Astrodynamics
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type	Books

Holdings
Withdrawn status	Lost status	Damaged status	Not for loan	Permanent Location	Current Location	Shelving location	Full call number	Accession Number	Koha item type
				Dr. S. R. Ranganathan Library	Dr. S. R. Ranganathan Library	General Stacks	629.411 B38, 2	3212	Books