The elliptical restricted three body problem | Study on effects of triaxiality of primaries with oblate infinitesimal in the elliptical restricted three body problem. This item is unavailable.
Language: English
Published by Scholars' Press, 2025
- Softcover
- New
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Softcover
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US$ 405.62
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The elliptical restricted three body problem | Study on effects of triaxiality of primaries with oblate infinitesimal in the elliptical restricted three body problem | Shilpi Dewangan (u. a.) | Taschenbuch | Englisch | 2025 | Scholars' Press | EAN 9783639717785 | Verantwortliche Person für die EU: SIA OmniScriptum Publishing, Brivibas Gatve 197, 1039 RIGA, LETTLAND, customerservice[at]vdm-vsg[dot]de | Anbieter: preigu.
Seller Inventory # 131263767
- Title
- The elliptical restricted three body problem | Study on effects of triaxiality of primaries with oblate infinitesimal in the elliptical restricted three body problem
- Author
- Shilpi Dewangan (u. a.)
- Publisher
- Scholars' Press
- Publication year
- 2025
- Condition
- Neu
- Binding
- Taschenbuch
- Language
- English
- ISBN 10
- 3639717783
- ISBN 13
- 9783639717785
- Item weight
- 274 grams
- Dimensions
- 220 x 150 x 11 mm
- Seller catalogs
- Bücher
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.
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