Hamiltonian Perturbation Solutions for Spacecraft Orbit Prediction : : The Method of Lie Transforms / / Martín Lara.

• Superior document: Title is part of eBook package: De Gruyter DG Ebook Package English 2021
• VerfasserIn: Lara, Martín,
• Place / Publishing House: Berlin ;, Boston : : De Gruyter, , [2021]; ©2021
• Year of Publication: 2021
• Language: English
• Series: De Gruyter Studies in Mathematical Physics , 54
• Physical Description: 1 online resource (XVI, 378 p.)
• Other title: Frontmatter --; Preface --; Contents --; 1 Introduction --; Part I: Hamiltonian perturbations by Lie transforms --; 2 The method of Lie transforms --; 3 Application to integrable problems --; Part II: Perturbed elliptic motion: Artificial satellite theory --; 4 The Kepler problem --; 5 The main problem of the artificial satellite --; 6 Zonal perturbations --; 7 Tesseral perturbations --; 8 Lunisolar perturbations --; 9 Non-conservative effects --; Part III: Relative motion and perturbed non-Keplerian motion --; 10 The Hill problem --; 11 Motion inside Hill’s sphere --; 12 Motion about the libration points --; 13 Quasi-satellite orbits --; Bibliography --; Index
• Format: Mode of access: Internet via World Wide Web.
• ISBN: 9783110668513; 9783110750720; 9783110750706; 9783110754001; 9783110753776; 9783110754162; 9783110753936
• ISSN: 2194-3532
• DOI: 10.1515/9783110668513
• Access: restricted access
• Hierarchical level: Monograph
• Statement of Responsibility: Martín Lara.

Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems are discussed according to the Lie transforms method, which is the de facto standard in analytical orbital motion calculations.