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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भाषा अंग्रेज़ी ● स्वरूप PDF ● पेज 204 ● ISBN 9789812794628 ● फाइल का आकार 7.9 MB ● प्रकाशक World Scientific Publishing Company ● शहर Singapore ● देश SG ● प्रकाशित 2001 ● डाउनलोड करने योग्य 24 महीने ● मुद्रा EUR ● आईडी 2446659 ● कॉपी सुरक्षा Adobe DRM
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