Nonlinear finite time attitude control of flexible spacecraft based on a novel output redefinition method

A finite time attitude controller is designed for a flexible spacecraft based on a novel output redefinition method, in this paper. To make the flexible appendages vibration suppression effective, the appendage tip-point is selected as the output. First, a novel output redefinition method is propose...

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Veröffentlicht in:	Chinese journal of aeronautics 2023-11, Vol.36 (11), p.373-385
Hauptverfasser:	ESMAEILZADEH, Seyed Majid, ZEYGHAMI, Mohammad Sadegh
Format:	Artikel
Sprache:	eng
Schlagworte:	Attitude control Backstepping Finite time Flexible spacecraft H∞ control Output redefinition Robust
Online-Zugang:	Volltext
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