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The three-body problem
Authors: ---
ISBN: 9780511616006 9780521852241 0511132891 9780511132896 0511131534 9780511131530 0511616007 1280431695 9781280431692 0511132352 9780511132353 0521852242 1107154332 9786610431694 0511200919 0511183070 0511311176 Year: 2006 Publisher: Cambridge Cambridge University Press

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Abstract

How do three celestial bodies move under their mutual gravitational attraction? This problem has been studied by Isaac Newton and leading mathematicians over the last two centuries. Poincaré's conclusion, that the problem represents an example of chaos in nature, opens the new possibility of using a statistical approach. For the first time this book presents these methods in a systematic way, surveying statistical as well as more traditional methods. The book begins by providing an introduction to celestial mechanics, including Lagrangian and Hamiltonian methods, and both the two and restricted three body problems. It then surveys statistical and perturbation methods for the solution of the general three body problem, providing solutions based on combining orbit calculations with semi-analytic methods for the first time. This book should be essential reading for students in this rapidly expanding field and is suitable for students of celestial mechanics at advanced undergraduate and graduate level.

The integral manifolds of the three body problem
Authors: --- ---
ISSN: 00659266 ISBN: 0821806920 Year: 1998 Publisher: Providence, R.I. American Mathematical Society

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Book
Dynamics and mission design near libration points
Author:
ISBN: 1281934577 9786611934576 9812794638 9789812794635 9781281934574 Year: 2001 Publisher: Singapore ; River Edge, NJ : World Scientific,

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The aim of this book is to explain, analyze and compute the kinds of motions that appear in an extended vicinity of the geometrically defined equilateral points of the Earth-Moon system, as a source of possible nominal orbits for future space missions. The methodology developed here is not specific to astrodynamics problems. The techniques are developed in such a way that they can be used to study problems that can be modeled by dynamical systems.
Contents:

  • Global Stability Zones Around the Triangular Libration Points
  • The Normal Form Around L5 in the Three-dim

Book
Dynamics and mission design near libration points.
Author:
ISBN: 1281934569 9786611934569 981279462X 9789812794628 9781281934567 Year: 2001 Publisher: Singapore ; River Edge, NJ : World Scientific,

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This book studies several problems related to the analysis of planned or possible spacecraft missions. It is divided into four chapters. The first chapter is devoted to the computation of quasiperiodic solutions for the motion of a spacecraft near the equilateral points of the Earth-Moon system. The second chapter gives a complete description of the orbits near the collinear point, L1, between the Earth and the Sun in the restricted three-body problem (RTBP) model. In the third chapter, methods are developed to compute the nominal orbit and to design and test the control strategy for t


Book
Dynamics and mission design near libration points.
Author:
ISBN: 1281956295 9786611956295 9812810633 9789812810632 9781281956293 Year: 2001 Publisher: Singapore ; River Edge, N.J. : World Scientific,

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In this book the problem of station keeping is studied for orbits near libration points in the solar system. The main focus is on orbits near halo ones in the (Earth+Moon)-Sun system. Taking as starting point the restricted three-body problem, the motion in the full solar system is considered as a perturbation of this simplified model. All the study is done with enough generality to allow easy application to other primary-secondary systems as a simple extension of the analytical and numerical computations. Contents: Bibliographical Survey Halo Orbits. Analytical and


Book
Dynamics and mission design near libration points.
Author:
ISBN: 1281956309 9786611956301 9812810641 9789812810649 9781281956309 Year: 2001 Publisher: Singapore ; River Edge, NJ : World Scientific,

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It is well known that the restricted three-body problem has triangular equilibrium points. These points are linearly stable for values of the mass parameter, μ, below Routh's critical value, μ1. It is also known that in the spatial case they are nonlinearly stable, not for all the initial conditions in a neighborhood of the equilibrium points L4, L5 but for a set of relatively large measures. This follows from the celebrated Kolmogorov-Arnold-Moser theorem. In fact there are neighborhoods of computable size for which one obtains "practical stability" in the sense t


Book
The three-body problem
Author:
ISBN: 0444874402 0444600744 9780444874405 Year: 1990 Volume: 4 Publisher: Amsterdam: Elsevier,

The restricted 3-body problem : / : plane periodic orbits
Authors: --- ---
ISBN: 3110137038 3110901730 Year: 1994 Volume: 17 Publisher: Berlin New York, NY : Walter de Gruyter,

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The Restricted 3-Body Problem: Plane Periodic Orbits (Special Research Unit 227--Prevention and Intervention in Ch)

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