ENGLISH

Dynamics and Mission Design Near Libration Points, Vol. III, Advanced Methods for Collinear Points

Book information

Publisher
World Scientific Pub Co Inc
Year
2001
ISBN
9810242115, 9789810242114
Open Library ID
OL15588805M
Language
english
Format
PDF
Filesize
2 MB (2295775 bytes)
Series
World Scientific Monograph Series in Mathematics 4
Pages
203\203
DPI
300
Orientation
yes
Scanned
yes
Time added
2011-08-31 04:54:40

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 notion 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 the quasiperiodic halo orbits. In the last chapter, the transfer from the Earth to a halo orbit is studied.

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