Name: The Elliptical Restricted Three Body Problem: Study on Effects of Triaxiality of Primaries With Oblate Infinitesimal in the Elliptical Restricted Three Body Problem (en Inglés)
Price: 333.85 PEN
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Author: Shilpi Dewangan; Ashutosh Narayan
ISBN: 9783639717785

portada The Elliptical Restricted Three Body Problem: Study on Effects of Triaxiality of Primaries With Oblate Infinitesimal in the Elliptical Restricted Three Body Problem (en Inglés)

The Elliptical Restricted Three Body Problem: Study on Effects of Triaxiality of Primaries With Oblate Infinitesimal in the Elliptical Restricted Three Body Problem (en Inglés)

Formato

Libro Físico

Editorial

Scholars' Press

Autor

Shilpi Dewangan; Ashutosh Narayan

Idioma

Inglés

N° páginas

172

Encuadernación

Tapa Blanda

ISBN13

9783639717785

The Elliptical Restricted Three Body Problem: Study on Effects of Triaxiality of Primaries With Oblate Infinitesimal in the Elliptical Restricted Three Body Problem (en Inglés)

Shilpi Dewangan; Ashutosh Narayan (Autor) · Scholars' Press · Tapa Blanda

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Reseña del libro "The Elliptical Restricted Three Body Problem: Study on Effects of Triaxiality of Primaries With Oblate Infinitesimal in the Elliptical Restricted Three Body Problem (en Inglés)"

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.