000			04205nam a22004693i 4500
001			EBC3111479
003			MiAaPQ
005			20240729124519.0
006			m o d |
007			cr cnu||||||||
008			240724s1964 xx o ||||0 eng d
020			_a9781600862694 _q(electronic bk.)
020			_z9781563478635
035			_a(MiAaPQ)EBC3111479
035			_a(Au-PeEL)EBL3111479
035			_a(CaPaEBR)ebr10516523
035			_a(OCoLC)922978744
040			_aMiAaPQ _beng _erda _epn _cMiAaPQ _dMiAaPQ
050		4	_aTL790 -- .C45 1964eb
082	0		_a521.1
100	1		_aSzebehely, Victor G.
245	1	0	_aCelestial Mechanics and Astrodynamics.
250			_a1st ed.
264		1	_aReston : _bAmerican Institute of Aeronautics and Astronautics, _c1964.
264		4	_c©1964.
300			_a1 online resource (765 pages)
336			_atext _btxt _2rdacontent
337			_acomputer _bc _2rdamedia
338			_aonline resource _bcr _2rdacarrier
490	1		_aProgress in Astronautics and Aeronautics
505	0		_aCover -- 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.
505	8		_aV. 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.
588			_aDescription based on publisher supplied metadata and other sources.
590			_aElectronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.
650		0	_aAstronautics.
650		0	_aArtificial satellites -- Orbits.
655		4	_aElectronic books.
776	0	8	_iPrint version: _aSzebehely, Victor G. _tCelestial Mechanics and Astrodynamics _dReston : American Institute of Aeronautics and Astronautics,c1964 _z9781563478635
797	2		_aProQuest (Firm)
830		0	_aProgress in Astronautics and Aeronautics
856	4	0	_uhttps://ebookcentral.proquest.com/lib/orpp/detail.action?docID=3111479 _zClick to View
999			_c68146 _d68146