Dynamics And Mission Design Near Libration Points, Vol Iii: Advanced Methods For Collinear Points

Author:   Gerard Gomez (Univ De Barcelona, Spain) ,  Angel Jorba (Univ Politecnica De Catalunya, Spain) ,  Josep J Masdemont (Ieec-univ Politecnica De Catalunya, Spain) ,  Carles Simo (Univ De Barcelona, Spain)
Publisher:   World Scientific Publishing Co Pte Ltd
Volume:   4
ISBN:  

9789810242114


Pages:   204
Publication Date:   12 February 2001
Format:   Hardback
Availability:   In Print   Availability explained
This item will be ordered in for you from one of our suppliers. Upon receipt, we will promptly dispatch it out to you. For in store availability, please contact us.

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Dynamics And Mission Design Near Libration Points, Vol Iii: Advanced Methods For Collinear Points


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Overview

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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Author:   Gerard Gomez (Univ De Barcelona, Spain) ,  Angel Jorba (Univ Politecnica De Catalunya, Spain) ,  Josep J Masdemont (Ieec-univ Politecnica De Catalunya, Spain) ,  Carles Simo (Univ De Barcelona, Spain)
Publisher:   World Scientific Publishing Co Pte Ltd
Imprint:   World Scientific Publishing Co Pte Ltd
Volume:   4
Dimensions:   Width: 17.00cm , Height: 1.50cm , Length: 23.00cm
Weight:   0.499kg
ISBN:  

9789810242114


ISBN 10:   9810242115
Pages:   204
Publication Date:   12 February 2001
Audience:   College/higher education ,  Professional and scholarly ,  Undergraduate ,  Postgraduate, Research & Scholarly
Format:   Hardback
Publisher's Status:   Active
Availability:   In Print   Availability explained
This item will be ordered in for you from one of our suppliers. Upon receipt, we will promptly dispatch it out to you. For in store availability, please contact us.

Table of Contents

Quasi-periodic solutions near the equilateral points of the Earth-Moon system; global description of the orbits near the L1 point of the Earth-Sun system in the RTBP; quasi-periodic halo orbits; transfer from the Earth to a halo orbit; appendices - the JPL model, references systems and equations of motion, the model equations near the equilateral points in the Earth-Moon system, transfer between halo orbits of the RTBP.

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