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

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.

Dettagli sul prodotto

• Autori: Gerard Gomez, Gomez Gerard, Angel Jorba, Jorba Angel, Josep J Masdemont, Josep J Masdemont, Josep J. Masdemont, C. Simo, Carles Simo, Simo Carles
• Editore: Ingram Publishers Services
• Lingue: Inglese
• Formato: Copertina rigida
• Pubblicazione: 12.02.2001
• EAN: 9789810242114
• ISBN: 978-981-02-4211-4
• Serie: World Scientific Monograph Series In Mathematics; World Scientific Monograph Mat; World Scientific Monograph Ser; World Scientific Monograph Series in Mathematics
• Categorie: Scienze naturali, medicina, informatica, tecnica > Matematica > Analisi; MATHEMATICS / Applied, TECHNOLOGY & ENGINEERING / Aeronautics & Astronautics, astronautics, Applied mathematics, Aerospace & aviation technology, Aerospace and aviation technology