Dynamics and mission design near libration points

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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...

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Detalles Bibliográficos
Autores principales: Gómez, G, Jorba, A, Simo, C, Masdemont, J
Lenguaje:eng
Publicado: World Scientific 2001
Materias:
Mathematical Physics and Mathematics
Acceso en línea:http://cds.cern.ch/record/496161
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author Gómez, G
Jorba, A
Simo, C
Masdemont, J
author_facet Gómez, G
Jorba, A
Simo, C
Masdemont, J
author_sort Gómez, G
collection CERN
description 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, L 1 , 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 the qua
id cern-496161
institution Organización Europea para la Investigación Nuclear
language eng
publishDate 2001
publisher World Scientific
record_format invenio
spelling cern-4961612021-04-22T02:55:21Zhttp://cds.cern.ch/record/496161engGómez, GJorba, ASimo, CMasdemont, JDynamics and mission design near libration pointsMathematical Physics and MathematicsThis 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, L 1 , 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 the quaWorld Scientificoai:cds.cern.ch:4961612001
spellingShingle Mathematical Physics and Mathematics
Gómez, G
Jorba, A
Simo, C
Masdemont, J
Dynamics and mission design near libration points
title Dynamics and mission design near libration points
title_full Dynamics and mission design near libration points
title_fullStr Dynamics and mission design near libration points
title_full_unstemmed Dynamics and mission design near libration points
title_short Dynamics and mission design near libration points
title_sort dynamics and mission design near libration points
topic Mathematical Physics and Mathematics
url http://cds.cern.ch/record/496161
work_keys_str_mv AT gomezg dynamicsandmissiondesignnearlibrationpoints
AT jorbaa dynamicsandmissiondesignnearlibrationpoints
AT simoc dynamicsandmissiondesignnearlibrationpoints
AT masdemontj dynamicsandmissiondesignnearlibrationpoints

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