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The Elliptical Restricted Three Body Problem

The Elliptical Restricted Three Body Problem

Paperback (10 Jan 2025)

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Publisher's 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.

Book information

ISBN: 9783639717785
Publisher: KS Omniscriptum Publishing
Imprint: Scholars' Press
Pub date:
Language: English
Number of pages: 172
Weight: -1g
Height: 229mm
Width: 152mm
Spine width: 10mm