Dynamics and Mission Design near Libration Points : Advanced Methods for Collinear Points

Advanced Methods for Collinear Points

By: Gerard Gomez, Angel Jorba, Josep J. Masdemont, C. Simo

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Hardcover | 1 December 1999

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204 Pages

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25.4 x 17.78 x 1.91

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

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Preface
Quasi-periodic Solutions Near the Equilateral Points of the Earth-Moon System	p. 1
Global Description of the Orbits Near the L[subscript 1] Point of the Earth-Sun System in the RTBP	p. 33
Quasi-periodic Halo Orbits	p. 69
Transfer From the Earth to a Halo Orbit	p. 93
The JPL Model	p. 127
Reference Systems and Equations of Motion	p. 133
The Model Equations Near the Equilateral Points in the Earth-Moon System	p. 147
Transfer Between Halo Orbits of the RTBP	p. 177
Bibliography	p. 187
Table of Contents provided by Blackwell. All Rights Reserved.

Dynamics and Mission Design near Libration Points : Advanced Methods for Collinear Points

Advanced Methods for Collinear Points

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Hardcover

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