Hybrid methods for interplanetary low-thrust trajectory optimization /

Hybrid methods for interplanetary low-thrust trajectory optimization are proposed. These methods are combinations of selected, existing methods for trajectory optimization. The focus of this thesis is to obtain solutions to a class of trajectories that are typical to the Mars Sample Return mission....

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Bibliographic Details

Main Author:	Aroonwilairut, Krisada
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 2002.
Subjects:	Major aerospace engineering.
Online Access:	Link to OAKTrust copy