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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Vydané v:	Asian journal of control Ročník 26; číslo 3; s. 1625 - 1632
Hlavní autori:	Majid Esmaeilzadeh, Seyed, Sadegh Zeyghami, Mohammad
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Hoboken Wiley Subscription Services, Inc 01.05.2024
Predmet:	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
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