A novel output redefinition method for nonlinear \(H_\infty\) attitude stabilization of a flexible spacecraft
type: Item
instance of: scholarly article
title: A novel output redefinition method for nonlinear \(H_\infty\) attitude stabilization of a flexible spacecraft
author: Seyed Majid Esmaeilzadeh
author: Mohammad Sadegh Zeyghami
published in: Asian Journal of Control
publication date: 2024-08-06T00:00:00Z
Mathematics Subject Classification ID: 93-XX
zbMATH DE Number: 7892575
zbMATH Keywords: attitude
zbMATH Keywords: back-stepping
zbMATH Keywords: flexible spacecraft
zbMATH Keywords: \(H_\infty\) control
zbMATH Keywords: output redefinition
zbMATH Keywords: robust control
MaRDI profile type: Publication
cites work: Fixed-time sliding mode observer-based controller for a class of uncertain nonlinear double integrator systems
cites work: Robust fixed-time attitude stabilization control of flexible spacecraft with actuator uncertainty
cites work: Robust finite-time adaptive control algorithm for satellite fast attitude maneuver
cites work: Variable-structure control of spacecraft large-angle maneuvers
cites work: Attitude stabilization of rigid spacecraft with finite-time convergence
cites work: Output regulation of nonlinear systems
cites work: Controllability and Observability for Flexible Spacecraft
cites work: Q4141027
cites work: Space vehicle dynamics and control
DOI: 10.1002/ASJC.3296
description: scientific article; zbMATH DE number 7892575