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
Seller: Ria Christie Collections, Uxbridge, United KingdomRia Christie Collections
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Softcover
Condition: New
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Item description from seller
In English.
Seller Inventory # ria9783639717785_new
- 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
- Dewangan, Shilpi; Narayan, Ashutosh
- Publisher
- Scholars' Press
- Publication year
- 2025
- Condition
- New
- Binding
- Soft cover
- Language
- English
- ISBN 10
- 3639717783
- ISBN 13
- 9783639717785
- Item weight
- 360 grams
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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