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.
Reihe
Sprache
Verlagsort
Zielgruppe
Für höhere Schule und Studium
Für Beruf und Forschung
Maße
Höhe: 254 mm
Breite: 191 mm
Gewicht
ISBN-13
978-90-5699-212-5 (9789056992125)
Copyright in bibliographic data is held by Nielsen Book Services Limited or its licensors: all rights reserved.
Schweitzer Klassifikation
Autor*in
Institute of Applied Astronomy, Russia
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