Ebook Info
- Published: 2001
- Number of pages: 204 pages
- Format: PDF
- File Size: 2.19 MB
- Authors: Gerard Gomez
Description
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.
User’s Reviews
Reviews from Amazon users which were colected at the time this book was published on the website:
⭐
⭐
Keywords
Free Download Dynamics and Mission Design Near Libration Points, Vol. III, Advanced Methods for Collinear Points in PDF format
Dynamics and Mission Design Near Libration Points, Vol. III, Advanced Methods for Collinear Points PDF Free Download
Download Dynamics and Mission Design Near Libration Points, Vol. III, Advanced Methods for Collinear Points 2001 PDF Free
Dynamics and Mission Design Near Libration Points, Vol. III, Advanced Methods for Collinear Points 2001 PDF Free Download
Download Dynamics and Mission Design Near Libration Points, Vol. III, Advanced Methods for Collinear Points PDF
Free Download Ebook Dynamics and Mission Design Near Libration Points, Vol. III, Advanced Methods for Collinear Points