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Methods in astrodynamics and celestial mechanics /

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autores Corporativos: Astrodynamics Specialist Conference Monterey, Calif., American Institute of Aeronautics and Astronautics, Institute of Navigation
Otros Autores: Duncombe, Raynor L., Szebehely, Victor G., 1921-
Formato: Electrónico Congresos, conferencias eBook
Idioma:Inglés
Publicado: New York : Academic Press, 1966.
Colección:Progress in astronautics and aeronautics ; v. 17.
Temas:
Acceso en línea:Texto completo
Tabla de Contenidos:
  • 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 ExponentsII. 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 AnalysisError Equations of Inertial Navigation with Special Application to Orbital Determination and Guidance
  • Efficient and Accurate Orbit Prediction for Very Long Periods of Time
  • Parameter Hunting Procedures
  • Accuracy in the Determination of Lunar Transponder Location from Postarrival Tracking
  • Interplanetary Maneuvers in Manned Helionautical Missions
  • IV. Optimization in Astrodynamics
  • A General Method for Selection and Optimization of Trajectories
  • Application of a Finite-Difference Newton-Raphson Algorithm to Problems of Low-Thrust Trajectory OptimizationNonlinear Optimal Control Problems with Control Appearing Linearly
  • Contributors To Volume 17