The elliptical restricted three body problem | Study on effects of triaxiality of primaries with oblate infinitesimal in the elliptical restricted three body problem

Shilpi Dewangan (u. a.)

ISBN 10: 3639717783 / ISBN 13: 9783639717785

Published by Scholars' Press, 2025

About this Item

The elliptical restricted three body problem | Study on effects of triaxiality of primaries with oblate infinitesimal in the elliptical restricted three body problem | Shilpi Dewangan (u. a.) | Taschenbuch | Englisch | 2025 | Scholars' Press | EAN 9783639717785 | Verantwortliche Person für die EU: SIA OmniScriptum Publishing, Brivibas Gatve 197, 1039 RIGA, LETTLAND, customerservice[at]vdm-vsg[dot]de | Anbieter: preigu.

Seller Inventory # 131263767

Bibliographic Details

• Title: The elliptical restricted three body problem | Study on effects of triaxiality of primaries with oblate infinitesimal in the elliptical restricted three body problem
• Publisher: Scholars' Press
• Publication Date: 2025
• Language: English
• ISBN 10: 3639717783
• ISBN 13: 9783639717785
• Binding: Taschenbuch
• Condition: Neu
• Dimensions: 220W x 150H x 11D millimeters 220 millimeters width by 150 millimeters height by 11 millimeters depth
• Weight: 274 grams
• Seller catalogs:
  • Bücher

About this title

Synopsis

Restricted three body problem is used to study the behavior of spacecraft, asteroids, and moons in systems like the Earth-Moon-Sun, Jupiter's moons etc. The present book deals with the problem of finding the existence and stability of the equilibrium points in the Elliptical restricted 3-body problem. It also helps in analyzing Lagrange points, which are positions in the orbital plane of the two massive bodies where the third body can maintain a stable position. Resonances play a critical role in understanding the long-term evolution of orbits in celestial mechanics. The linear and non-linear stability has been studied for 3rd and 4th order resonance.