Celestial Dynamics at High Eccentricities
Taylor & Francis (Publisher)
Published on 22. July 1999
Book
Hardback
220 pages
978-90-5699-212-5 (ISBN)
Description
This book aims to extend the range of application of analytical and semi-analytical techniques of classical celestial mechanics for the case of motion in highly eccentric orbits. The technique, developed by the authors and described in detail here, is based on the traditional mean, true, or eccentric anomalies with the elliptic anomaly and corresponding Fourier expansions for Jacobi elliptic functions. It makes it possible to represent more effectively the motion of celestial objects in highly eccentric orbits, which until now has been studied mostly using numerical integration. The specific methodology described in the book is linked closely to mathematical software used widely in the West, and is therefore of relevance to researchers worldwide.
More details
Series
Language
English
Place of publication
London
United Kingdom
Target group
College/higher education
Professional and scholarly
Dimensions
Height: 254 mm
Width: 191 mm
Weight
657 gr
ISBN-13
978-90-5699-212-5 (9789056992125)
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Schweitzer Classification
Persons
Content
1. Elliptic Anomaly in the Two-Body Problem 2. Elliptic Anomaly in Perturbed Motion 3. Linear Theory of Motion for Highly Eccentric Artificial Satellites 4. Theory of Motion of Asteroids in Highly Eccentric (Non-Intersecting) Orbits 5. Theory of Motion of the Objects in Orbits Intersecting in Projection 6. Computational Formulas