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Dynamics and Mission Design Near Libration Points - Vol I : Fundamentals.

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 p...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Llibre, J.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Singapore : World Scientific Publishing Company, 2001.
Colección:World Scientific monograph series in mathematics.
Temas:
Acceso en línea:Texto completo

MARC

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245 1 0 |a Dynamics and Mission Design Near Libration Points - Vol I :  |b Fundamentals. 
260 |a Singapore :  |b World Scientific Publishing Company,  |c 2001. 
300 |a 1 online resource (464 pages) 
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490 1 |a World Scientific Monograph Series in Mathematics 
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520 |a 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 Numerical Study; The Neigh. 
505 0 |a Foreword ; Preface ; Introduction: Libration Points and Station Keeping ; 0.1 The Neighborhood of Libration Points as a Useful Place for Spacecrafts ; 0.1.1 The Libration Points in the Restricted Three-body Problem. 
505 8 |a 0.1.2 The Libration Points in Perturbations of the Restricted Threebody Problem 0.1.3 Possible Missions Around the Libration Points ; 0.1.4 The Real Nominal Quasi-periodic Orbit ; 0.2 Station Keeping of Libration Point Orbits ; 0.2.1 Unstable Nominal Orbits. 
505 8 |a 0.2.2 Requirements for an On/off Control Chapter 1 Bibliographical Survey ; 1.1 Numerical Results for Three-dimensional Periodic Orbits Around L1, L2 and L3; 1.1.1 References ; 1.1.2 Equations. General Properties ; 1.1.3 Linear Theory Around the Equilibrium Points ; 1.1.4 Description of the Results. 
505 8 |a 1.2 Analytic Results for Halo Orbits Associated to L1, L2 and L31.2.1 References ; 1.2.2 Equations of Motion ; 1.2.3 Construction of Halo Periodic Solutions ; 1.3 Motion Near L4 and L5 ; 1.3.1 References ; 1.3.2 The Triangular Equilibrium Points, Location and Stability; 1.3.3 Numerical Explorations ; 1.3.4 Analytic Results ; 1.4 Station Keeping. 
505 8 |a 1.4.1 References 1.4.2 The Control of Libration Point Satellites ; 1.4.3 Station Keeping for a Translunar Station ; 1.4.4 Control of an Unstable Periodic Orbit ; 1.4.5 Station Keeping for the ISEE-C. Algorithm and Results ; 1.4.6 Additional Work. 
590 |a ProQuest Ebook Central  |b Ebook Central Academic Complete 
650 0 |a Three-body problem. 
650 0 |a Lagrangian points. 
650 6 |a Problème à trois corps. 
650 6 |a Points de Lagrange. 
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650 7 |a Three-body problem  |2 fast 
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