Spacecraft Trajectory Optimization / Edited by Bruce Conway

Von:

Conway, Bruce [aut]

Resource type: Ressourcentyp: Buch (Online)Buch (Online)Sprache: Englisch Reihen: Cambridge Aerospace Series ; no. 29 | Cambridge aerospace series ; 29Verlag: Cambridge : Cambridge University Press, 2010Auflage: Online-AusgBeschreibung: Online-Ressource (1 online resource (310 p.)) : digital, PDF file(s)ISBN:

9780511778025

Schlagwörter:

Andere physische Formen: 9780521518505. | 9781107653825. | Erscheint auch als: Spacecraft trajectory optimization. Druck-Ausgabe. Cambridge [u.a.] : Cambridge University Press, 2010. IX, 298 S. | Erscheint auch als: 9780521518505 Druck-AusgabeDDC-Klassifikation:

629.4/11 22

RVK: RVK: ZO 8000LOC-Klassifikation:

TL1075

DOI: DOI: 10.1017/CBO9780511778025Online-Ressourcen:

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Zusammenfassung: This is a long-overdue volume dedicated to space trajectory optimization. Interest in the subject has grown, as space missions of increasing levels of sophistication, complexity, and scientific return - hardly imaginable in the 1960s - have been designed and flown. Although the basic tools of optimization theory remain an accepted canon, there has been a revolution in the manner in which they are applied and in the development of numerical optimization. This volume purposely includes a variety of both analytical and numerical approaches to trajectory optimization. The choice of authors has been guided by the editor's intention to assemble the most expert and active researchers in the various specialities presented. The authors were given considerable freedom to choose their subjects, and although this may yield a somewhat eclectic volume, it also yields chapters written with palpable enthusiasm and relevance to contemporary problemsZusammenfassung: The problem of spacecraft trajectory optimization / Bruce A. Conway -- Primer vector theory and application / John E. Prussing -- Spacecraft trajectory optimization using direct transcription and nonlinear programming / Bruce A. Conway and Stephen W. Paris -- Elements of a software system for spacecraft trajectory optimization / Cesar Ocampo -- Low-thrust trajectory optimization using orbital averaging and control parameterization / Craig A. Kluever -- Analytic representation of optimal low-thrust transfer in circular orbit / Jean A. Kéchichian -- Global optimisation and space pruning for spacecraft trajectory design / Dario Izzo -- Incremental techniques for global space trajectory design / Massimiliano Vasile and Matteo Ceriotti -- Optimal low-thrust trajectories using stable manifolds / Christopher Martin and Bruce A. Conway -- Swarming theory applied to space trajectory optimization / Mauro Pontani and Bruce A. ConwayPPN: PPN: 883351927Package identifier: Produktsigel: ZDB-20-CTM | ZDB-20-CBO

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