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|a TL1050
|b .A88 1965eb
|
| 082 |
0 |
4 |
|a 629.4ll
|2 22
|
| 049 |
|
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|a UAMI
|
| 111 |
2 |
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|a Astrodynamics Specialist Conference
|d (1965 :
|c Monterey, Calif.)
|
| 245 |
1 |
0 |
|a Methods in astrodynamics and celestial mechanics /
|c edited by Raynor L. Duncombe, Victor G. Szebehely.
|
| 260 |
|
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|a New York :
|b Academic Press,
|c 1966.
|
| 300 |
|
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|a 1 online resource (xvi, 436 pages) :
|b illustrations
|
| 336 |
|
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|a text
|b txt
|2 rdacontent
|
| 337 |
|
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|a computer
|b c
|2 rdamedia
|
| 338 |
|
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|a online resource
|b cr
|2 rdacarrier
|
| 490 |
1 |
|
|a Progress in astronautics and aeronautics ;
|v v. 17
|
| 500 |
|
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|a Papers based mainly on the American Institute of Aeronautics and Astronautics and Institute of Navigation, Astrodynamics Specialist Conference.
|
| 504 |
|
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|a Includes bibliographical references.
|
| 505 |
0 |
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|a 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
|
| 505 |
8 |
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|a 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
|
| 505 |
8 |
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|a 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
|
| 505 |
8 |
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|a 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
|
| 590 |
|
|
|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
| 650 |
|
0 |
|a Astrodynamics
|v Congresses.
|
| 650 |
|
6 |
|a Astrodynamique
|v Congrès.
|
| 650 |
|
7 |
|a Astrodynamics
|2 fast
|
| 655 |
|
7 |
|a Conference papers and proceedings
|2 fast
|
| 700 |
1 |
|
|a Duncombe, Raynor L.
|
| 700 |
1 |
|
|a Szebehely, Victor G.,
|d 1921-
|1 https://id.oclc.org/worldcat/entity/E39PBJvtbPtTP9XpV6YBmTWqwC
|
| 710 |
2 |
|
|a American Institute of Aeronautics and Astronautics.
|
| 710 |
2 |
|
|a Institute of Navigation.
|
| 758 |
|
|
|i has work:
|a Methods in astrodynamics and celestial mechanics (Text)
|1 https://id.oclc.org/worldcat/entity/E39PCGqMxMBMmFKC8Hg37m9CHy
|4 https://id.oclc.org/worldcat/ontology/hasWork
|
| 776 |
0 |
8 |
|i Print version:
|a Astrodynamics Specialist Conference (1965 : Monterey, Calif.).
|t Methods in astrodynamics and celestial mechanics.
|d New York : Academic Press, 1966
|w (DLC) 66021326
|
| 830 |
|
0 |
|a Progress in astronautics and aeronautics ;
|v v. 17.
|
| 856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111532
|z Texto completo
|
| 938 |
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|a EBL - Ebook Library
|b EBLB
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|b EBRY
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|b IZTAP
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