Preface -- Introduction -- Chapter 1 Selection and Conversions of Coordinate System -- Chapter 2 Complete Solutions of the two-body Problem -- Chapter 3 Analytical methods of structural solutions for a perturbed satellite orbit -- Chapter 4 Non-singular point analytical solutions for a perturbed Earth’s satellite orbit by extrapolation -- Chapter 5 Design of satellite orbit and lifespan estimation -- Chapter 6 Orbital solutions of satellites of the Moon and major planets -- Chapter 7 Orbits in the restricted three-body problem and calculation methods -- Chapter 8 Numerical methods for satellite orbit extrapolation -- Chapter 9 Formulation of orbit determination and calculation of initial orbit -- Chapter 10 Determination of precession orbit -- Appendix.
This book highlights the fundamental physics of orbit theory, dynamical models, methods of orbit determination, design, measurement, adjustment, and complete calculations for the position, tracking, and prediction of satellites and deep spacecraft. It emphasizes specific methods, related mathematical calculations, and worked examples and exercises. Therefore, technicians and engineers in the aerospace industry can directly apply them to their practical work. Dedicated to undergraduate students and graduate students, researchers, and professionals in astronomy, physics, space science, and related aerospace industries, the book is an integrated work based on the accumulated knowledge in satellite orbit dynamics and the author’s more than five decades of personal research and teaching experience in astronomy and aerospace dynamics.
Algorithms for Satellite Orbital Dynamics
1st ed. 2023.
2023
1 Online-Ressource(XXXI, 553 p. 63 illus.)
Campusweiter Zugriff (Universität Hannover) - Vervielfältigungen (z.B. Kopien, Downloads) sind nur von einzelnen Kapiteln oder Seiten und nur zum eigenen wissenschaftlichen Gebrauch erlaubt. Keine Weitergabe an Dritte. Kein systematisches Downloaden durch Robots.
Buch
Elektronische Ressource
Englisch
DDC: | 629.4 |
Springer Verlag | 2021
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