Neural optimal control of flexible spacecraft slew maneuver

This paper deals with the problem of optimal large-angle single-axis maneuvers of a flexible spacecraft with simultaneous vibration suppression of elastic modes. A spacecraft model with a cylindrical hub and one flexible appendage and tip mass is considered. Gravity gradient torque is considered as...

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Bibliographic Details

Published in:	Acta astronautica Vol. 55; no. 10; pp. 817 - 827
Main Authors:	Nayeri, M.Reza Dehghan, Alasty, Aria, Daneshjou, Kamran
Format:	Journal Article
Language:	English
Published:	Elsevier Ltd 01.11.2004
ISSN:	0094-5765, 1879-2030
Online Access:	Get full text
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