A novel output redefinition method for nonlinear H∞ attitude stabilization of a flexible spacecraft

This paper addresses a novel output redefinition method for the nonlinear H∞$$ {H}_{\infty } $$ attitude stabilization problem of a flexible spacecraft. As an idea, the flexible appendage tip‐point can be selected as attitude output which may improve attitude pointing accuracy. However, it makes the...

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Bibliographic Details

Published in:	Asian journal of control Vol. 26; no. 3; pp. 1625 - 1632
Main Authors:	Majid Esmaeilzadeh, Seyed, Sadegh Zeyghami, Mohammad
Format:	Journal Article
Language:	English
Published:	Hoboken Wiley Subscription Services, Inc 01.05.2024
Subjects:	attitude Attitude control Attitude stability back‐stepping Control systems design Flexible spacecraft H-infinity control H∞$$ {H}_{\infty } $$ control output redefinition robust control Spacecraft
ISSN:	1561-8625, 1934-6093
Online Access:	Get full text
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