Near-minimum-time three-dimensional maneuvers of rigid and flexible spacecraft /

The purpose of this research is to control the attitude of rigid and flexible spacecraft in three-dimensions in a minimal amount of time. Vibration suppression will be accomplished passively using input smoothing, which is extremely important when dealing with flexible structures. Additionally, a c...

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Bibliographic Details

Main Author:	Bell, Mark James, 1968-
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 1993.
Subjects:	Major aerospace engineering.
Online Access:	Link to OAKTrust copy