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The elliptical restricted three body problem

Shilpi Dewangan Ashutosh Narayan

$126.95   $101.92

Paperback

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English
Scholars' Press
10 January 2025
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.
By:   ,
Imprint:   Scholars' Press
Dimensions:   Height: 229mm,  Width: 152mm,  Spine: 10mm
Weight:   236g
ISBN:   9783639717785
ISBN 10:   3639717783
Pages:   172
Publication Date:  
Audience:   General/trade ,  ELT Advanced
Format:   Paperback
Publisher's Status:   Active

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