| Description |
1 online resource |
| Series |
Progress in astronautics and aeronautics ; v. 14 |
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Progress in astronautics and aeronautics ; v. 14.
|
| Contents |
""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"" |
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""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"" |
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""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"" |
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""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"" |
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""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"" |
| Notes |
"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." |
| Bibliography |
Includes bibliographical references and index |
| Notes |
Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002. http://purl.oclc.org/DLF/benchrepro0212 MiAaHDL |
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Print version record |
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digitized 2010 HathiTrust Digital Library committed to preserve pda MiAaHDL |
| Subject |
Astronautics.
|
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Artificial satellites -- Orbits.
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Artificial satellites -- Orbits
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Astronautics
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Astrodynamique -- Congrès.
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Mécanique céleste -- Congrès.
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| Form |
Electronic book
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| Author |
Szebehely, Victor G., 1921-
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American Institute of Aeronautics and Astronautics Astrodynamics Conference (1963 : Yale University)
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| LC no. |
64025707 |
| ISBN |
9781600862694 |
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1600862691 |
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9781563478635 |
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1563478633 |
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