04484nam 2200613 a 450 991081169180332120230213212224.01-60086-488-01-60086-269-1(CKB)2550000000073461(EBL)3111479(SSID)ssj0001101019(PQKBManifestationID)11600750(PQKBTitleCode)TC0001101019(PQKBWorkID)11064164(PQKB)10902013(MiAaPQ)EBC3111479(Au-PeEL)EBL3111479(CaPaEBR)ebr10516523(OCoLC)922978744(EXLCZ)99255000000007346120780104d1964 uy 0engur|n|---|||||txtccrCelestial mechanics and astrodynamics[electronic resource] /edited by Victor G. SzebehelyNew York Academic Press19641 online resource (765 p.)Progress in astronautics and aeronautics ;v. 14"A selection of technical papers based mainly on the American Institute of Aeronautics and Astronautics Astrodynamics Conference held at New Haven, Connecticut, August 19-21, 1963."1-56347-863-3 Includes bibliographical references and index.""Cover""; ""Title""; ""Copyright""; ""The ARS Astrodynamics Committee 1962""; ""The AIAA Astrodynamics Committee 1963""; ""The Astrodynamics Conference Committee 1963""; ""Preface""; ""Astrodynamics in the AIAA""; ""Contents""; ""I. Orbit Prediction and General Perturbations""; ""Numerical Aspects of Uniformly Valid Asymptotic Approximations for a Class of Trajectories in the Restricted Three-Body Problem""; ""A Group of Earth-to-Moon Trajectories with Consecutive Collisions""; ""Two Fixed Center Approximations to the Restricted Problem""""A High-Order Perturbation Theory Using Rectangular Coordinates""""Trajectories of Satellites under the Influence of Air Drag""; ""II. Astronomical Constants and Physical Properties""; ""System of Astronomical Constants""; ""The Evaluation of Certain Astronomical Constants from the Radio Tracking of Mariner II""; ""Atmospheric Density Determination from Satellite Observations""; ""III. Orbit Selection""; ""Probabilistic Evaluation of Satellite Missions Involving Ground Coverage""; ""Orbital Aspects of Nonsynchronous Communication Satellite Systems""""Guidance of Unmanned Lunar and Interplanetary Spacecraft""""An Approximate Method for Computing Error Coefficient Matrices for Lunar Trajectories""; ""Minimum Lunar Orbit Inclination to Lunar Equatorial Plane for Earth-Launched Vehicle""; ""General Characteristics of the Launch Window for Orbital Launch to the Moon""; ""Launch Windows for Highly Eccentric Orbits""; ""Moon-to-Earth Trajectories""; ""An Analysis of Free Return Circumlunar Trajectories""; ""Free Return Circumlunar Trajectories from Launch Windows with Fixed Launch Azimuths""""IV. Orbit Mechanics of the Ranger and Mariner Missions""""Trajectory Design for Ranger and Mariner Missions""; ""Boost Vehicle Trajectories for Ranger and Mariner Programs""; ""Launch-to-Mission Completion Targeting for Ranger and Mariner Missions""; ""V. Orbit Transfer and Trajectory Optimization""; ""A Trajectory Optimization Technique Based upon the Theory of the Second Variation""; ""Minimum Impulse Transfer""; ""On Some Single-Impulse Transfer Problems""; ""Analysis of the Orbital Transfer Problem in Three-Dimensional Space""; ""VI. Orbit Determination""""Position and Velocity Estimates by Trajectory Rectification""""Self-Contained Orbit Determination Techniques""; ""Linearized Drag Analysis and Orbit Determination""; ""Orbit Determination in the Presence of Systematic Errors""; ""Contributors to Volume 14""Progress in astronautics and aeronautics ;v. 14.AstronauticsArtificial satellitesOrbitsAstronautics.Artificial satellitesOrbits.521.1Szebehely Victor G.1921-50849American Institute of Aeronautics and Astronautics Astrodynamics Conference(1963 :Yale University)MiAaPQMiAaPQMiAaPQBOOK9910811691803321Celestial mechanics and astrodynamics3936549UNINA