portada Nonlinear Stability Analysis of Elliptical restricted three body problem (en Inglés)

Nonlinear Stability Analysis of Elliptical restricted three body problem (en Inglés)

Formato

Libro Físico

Autor

Ashutosh Narayan

Editorial

Scholars' Press

Idioma

Inglés

N° páginas

212

Encuadernación

Tapa Blanda

Dimensiones

22.9x15.2x1.2 cm

Peso

0.32 kg.

ISBN13

9786138926023

Categorías

Matemáticas

Nonlinear Stability Analysis of Elliptical restricted three body problem (en Inglés)

Ashutosh Narayan (Autor) · Scholars' Press · Tapa Blanda

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Reseña del libro "Nonlinear Stability Analysis of Elliptical restricted three body problem (en Inglés)"

The elliptical restricted three body problem describes the motion of a particle called third body (infinitesimal mass) under the gravitational attraction forces of two finite bodies, called the primaries, which revolve on the elliptic orbits in a plane around their common center of mass. In the restricted problems, the motion of two finite bodies (called primaries) satisfies the differential equation governing the dynamics of two body problem. Hence, the primaries may describe in circular, elliptical, parabolic or hyperbolic orbits. In the case when the primaries move along a circular orbit, then it is called circular restricted three body problem and if the primaries move on the elliptic orbit, then it is called, Elliptical restricted three body problems. The restricted problem of these bodies (circular or elliptical) is widely application in space Dynamics, Celestial Mechanics, Cosmology and Stellar dynamics.