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

    "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"--Page 4 of cover


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    Title :

    Hamiltonian perturbation solutions for spacecraft orbit prediction : the method of lie transforms


    Contributors:


    Publication date :

    2021


    Size :

    1 Online-Ressource (XIV, 377 Seiten)


    Remarks:

    Diagramme
    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
    Literaturverzeichnis: Seite 337-370




    Type of media :

    Book


    Type of material :

    Electronic Resource


    Language :

    English



    Classification :

    BKL:    33.06 Mathematische Methoden der Physik / 55.64 Raumfahrzeugführung



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