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The elliptical restricted three body problem
The elliptical restricted three body problem
Knygos.lt klubas Knygos.lt nariams
122,98 €
-30%
Įprastai
175,69 €
  • Išsiųsime per 12–18 d.d.
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…
  • Leidėjas:
  • ISBN-10: 3639717783
  • ISBN-13: 9783639717785
  • Formatas: 15.2 x 22.9 x 1 cm, minkšti viršeliai
  • Kalba: Anglų

The elliptical restricted three body problem (el. knyga) (skaityta knyga) | knygos.lt

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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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  • Autorius: Shilpi Dewangan
  • Leidėjas:
  • ISBN-10: 3639717783
  • ISBN-13: 9783639717785
  • Formatas: 15.2 x 22.9 x 1 cm, minkšti viršeliai
  • Kalba: Anglų

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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