Gerard Gomez & Angel Jorba 
DYNAMICS & MISSION DESIGN VOL III (V4) [PDF ebook] 
Volume III: Advanced Methods for Collinear 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 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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Bahasa Inggris ● Format PDF ● Halaman 204 ● ISBN 9789812794628 ● Ukuran file 7.9 MB ● Penerbit World Scientific Publishing Company ● Kota Singapore ● Negara SG ● Diterbitkan 2001 ● Diunduh 24 bulan ● Mata uang EUR ● ID 2446659 ● Perlindungan salinan Adobe DRM
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