Nonlinear Stability Analysis of Elliptical restricted three body problem: Stability Of The Oblate Infinitesimal In The Elliptical Restricted Three Body Problem With Oblate Radiating Primaries - Tapa blanda
Sinopsis
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.
"Sinopsis" puede pertenecer a otra edición de este libro.
Resultados de la búsqueda para Nonlinear Stability Analysis of Elliptical restricted...
Imagen del vendedor
Nonlinear Stability Analysis of Elliptical restricted three body problem
Publicado por
Scholars' Press Mrz 2020, 2020
ISBN 10: 6138926021
ISBN 13: 9786138926023
Nuevo
Taschenbuch
Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Alemania
Calificación del vendedor: 5 de 5 estrellas
Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -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. 212 pp. Englisch. Nº de ref. del artículo: 9786138926023
Comprar nuevo
EUR 89,90
Envío por EUR 23,00
Se envía de Alemania a Estados Unidos de America
Se envía de Alemania a Estados Unidos de America
Cantidad disponible: 2 disponibles
Imagen del vendedor
Nonlinear Stability Analysis of Elliptical restricted three body problem
Librería: moluna, Greven, Alemania
Calificación del vendedor: 5 de 5 estrellas
Condición: New. Nº de ref. del artículo: 385853900
Comprar nuevo
EUR 71,55
Envío por EUR 48,99
Se envía de Alemania a Estados Unidos de America
Se envía de Alemania a Estados Unidos de America
Cantidad disponible: Más de 20 disponibles
Imagen de archivo
Nonlinear Stability Analysis of Elliptical restricted three body problem: Stability Of The Oblate Infinitesimal In The Elliptical Restricted Three Body Problem With Oblate Radiating Primaries
Librería: Books Puddle, New York, NY, Estados Unidos de America
Calificación del vendedor: 4 de 5 estrellas
Condición: New. pp. 212. Nº de ref. del artículo: 26377846714
Comprar nuevo
EUR 137,56
Envío por EUR 3,44
Se envía dentro de Estados Unidos de America
Se envía dentro de Estados Unidos de America
Cantidad disponible: 4 disponibles
Imagen del vendedor
Nonlinear Stability Analysis of Elliptical restricted three body problem | Stability Of The Oblate Infinitesimal In The Elliptical Restricted Three Body Problem With Oblate Radiating Primaries
Librería: preigu, Osnabrück, Alemania
Calificación del vendedor: 5 de 5 estrellas
Taschenbuch. Condición: Neu. Nonlinear Stability Analysis of Elliptical restricted three body problem | Stability Of The Oblate Infinitesimal In The Elliptical Restricted Three Body Problem With Oblate Radiating Primaries | Ashutosh Narayan | Taschenbuch | 212 S. | Englisch | 2020 | Scholars' Press | EAN 9786138926023 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. Nº de ref. del artículo: 118209261
Comprar nuevo
EUR 74,80
Envío por EUR 70,00
Se envía de Alemania a Estados Unidos de America
Se envía de Alemania a Estados Unidos de America
Cantidad disponible: 5 disponibles
Imagen de archivo
Nonlinear Stability Analysis of Elliptical restricted three body problem: Stability Of The Oblate Infinitesimal In The Elliptical Restricted Three Body Problem With Oblate Radiating Primaries
Impresión bajo demandaLibrería: Majestic Books, Hounslow, Reino Unido
Calificación del vendedor: 4 de 5 estrellas
Condición: New. Print on Demand pp. 212. Nº de ref. del artículo: 385008741
Comprar nuevo
EUR 139,82
Envío por EUR 7,50
Se envía de Reino Unido a Estados Unidos de America
Se envía de Reino Unido a Estados Unidos de America
Cantidad disponible: 4 disponibles
Imagen del vendedor
Nonlinear Stability Analysis of Elliptical restricted three body problem
Publicado por
Scholars' Press Mär 2020, 2020
ISBN 10: 6138926021
ISBN 13: 9786138926023
Nuevo
Taschenbuch
Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemania
Calificación del vendedor: 5 de 5 estrellas
Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -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.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 212 pp. Englisch. Nº de ref. del artículo: 9786138926023
Comprar nuevo
EUR 89,90
Envío por EUR 60,00
Se envía de Alemania a Estados Unidos de America
Se envía de Alemania a Estados Unidos de America
Cantidad disponible: 1 disponibles
Imagen de archivo
Nonlinear Stability Analysis of Elliptical restricted three body problem: Stability Of The Oblate Infinitesimal In The Elliptical Restricted Three Body Problem With Oblate Radiating Primaries
Impresión bajo demandaLibrería: Biblios, Frankfurt am main, HESSE, Alemania
Calificación del vendedor: 4 de 5 estrellas
Condición: New. PRINT ON DEMAND pp. 212. Nº de ref. del artículo: 18377846704
Comprar nuevo
EUR 142,26
Envío por EUR 9,95
Se envía de Alemania a Estados Unidos de America
Se envía de Alemania a Estados Unidos de America
Cantidad disponible: 4 disponibles
Imagen del vendedor
Nonlinear Stability Analysis of Elliptical restricted three body problem : Stability Of The Oblate Infinitesimal In The Elliptical Restricted Three Body Problem With Oblate Radiating Primaries
Impresión bajo demandaLibrería: AHA-BUCH GmbH, Einbeck, Alemania
Calificación del vendedor: 5 de 5 estrellas
Taschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - 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. Nº de ref. del artículo: 9786138926023
Comprar nuevo
EUR 90,98
Envío por EUR 61,67
Se envía de Alemania a Estados Unidos de America
Se envía de Alemania a Estados Unidos de America
Cantidad disponible: 1 disponibles
Imagen de archivo
Nonlinear Stability Analysis of Elliptical restricted three body problem: Stability Of The Oblate Infinitesimal In The Elliptical Restricted Three Body Problem With Oblate Radiating Primaries
Librería: Mispah books, Redhill, SURRE, Reino Unido
Calificación del vendedor: 4 de 5 estrellas
paperback. Condición: New. NEW. SHIPS FROM MULTIPLE LOCATIONS. book. Nº de ref. del artículo: ERICA82361389260216
Comprar nuevo
EUR 193,77
Envío por EUR 28,85
Se envía de Reino Unido a Estados Unidos de America
Se envía de Reino Unido a Estados Unidos de America
Cantidad disponible: 1 disponibles