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Record Nr. |
UNINA9910781403803321 |
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Titolo |
Methods in astrodynamics and celestial mechanics [[electronic resource] /] / edited by Raynor L. Duncombe, Victor G. Szebehely |
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Pubbl/distr/stampa |
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New York, : Academic Press, 1966 |
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ISBN |
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1-60086-491-0 |
1-60086-272-1 |
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Descrizione fisica |
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1 online resource (453 p.) |
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Collana |
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Progress in astronautics and aeronautics ; ; v. 17 |
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Altri autori (Persone) |
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DuncombeRaynor L |
SzebehelyVictor G. <1921-> |
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Disciplina |
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Soggetti |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Papers based mainly on the American Institute of Aeronautics and Astronautics and Institute of Navigation, Astrodynamics Specialist Conference. |
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Nota di bibliografia |
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Includes bibliographical references. |
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Nota di contenuto |
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""Cover""; ""Title""; ""Copyright""; ""The AIAA Astrodynamics Committee 1965""; ""The Astrodynamics Specialist Conference Committee 1965""; ""Preface""; ""Contents""; ""I. Behavior of Bodies near Libration Points""; ""Theory and Application of Motion around Equilibrium Positions""; ""Limiting Orbits at the Equilateral Centers of Libration""; ""Motion in the Vicinity of Libration Points of a Generalized Restricted Three-Body Model""; ""Resonances Affecting Motion near the Earth-Moon Equilateral Libration Points""; ""Effect of Initial Configurations on Libration Point Motion"" |
""Analytical Determination of Characteristic Exponents""""II. Asymptotic Representations of Space Vehicle Trajectories""; ""Generalized Method of Averaging and the von Zeipel Method""; ""Take-off from a Circular Orbit by a Small Thrust""; ""Matched Asymptotic Expansions, Patched Conics, and the Computation of Interplanetary Trajectories""; ""A Uniformly Valid Asymptotic Representation of Satellite Motion around the Smaller Primary in the Restricted Three-Body Problem""; ""Asymptotic Representations for Solutions to the Differential Equations of Satellite Theory"" |
""III. Orbit Determination and Mission Analysis""""Error Equations of Inertial Navigation with Special Application to Orbital Determination |
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