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

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

Volume III: Advanced Methods for Collinear Points

  1. 204 pages
  2. English
  3. PDF
  4. Available on iOS & Android
eBook - PDF

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

Volume III: Advanced Methods for Collinear Points

Book details
Table of contents
Citations

About This Book

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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Yes, you can access Dynamics And Mission Design Near Libration Points, Vol Iii: Advanced Methods For Collinear Points by Gerard Gomez, Angel Jorba, Josep J Masdemont in PDF and/or ePUB format, as well as other popular books in Mathematics & Differential Equations. We have over one million books available in our catalogue for you to explore.

Information

Publisher
World Scientific
Year
2001
ISBN
9789812794628
Topic
Mathematics
Subtopic
Differential Equations
Index
Mathematics

Table of contents

  1. Contents
  2. Preface
  3. Chapter 1 Quasi-periodic Solutions Near the Equilateral Points of the Earth-Moon System
  4. Chapter 2 Global Description of the Orbits Near the L1 Point of the Earth-Sun System in the RTBP
  5. Chapter 3 Quasi-periodic Halo Orbits
  6. Chapter 4 Transfer From the Earth to a Halo Orbit
  7. Appendix A The JPL Model
  8. Appendix B Reference Systems and Equations of Motion
  9. Appendix C The Model Equations Near the Equilateral Points in the Earth-Moon System
  10. Appendix D Transfer Between Halo Orbits of the RTBP
  11. Bibliography