Output attitude tracking for flexible spacecraft
type: Item
instance of: scholarly article
title: Output attitude tracking for flexible spacecraft
zbMATH Open document ID: 1011.93522
DOI: 10.1016/S0005-1098(02)00082-1
author: Yanyan Li
published in: Automatica
publication date: 2003-02-17T00:00:00Z
Mathematics Subject Classification ID: 93C95
Mathematics Subject Classification ID: 70Q05
zbMATH DE Number: 1869146
zbMATH Keywords: nonlinear control
zbMATH Keywords: output tracking
zbMATH Keywords: dynamic control
zbMATH Keywords: flexible spacecraft
MaRDI profile type: Publication
cites work: Stabilization by smooth feedback of the angular velocity of a rigid body
cites work: Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models
cites work: Functional analysis in modern applied mathematics
cites work: Adaptive robust tracking for flexible spacecraft in presence of disturbances
cites work: Exact nonlinear control of large angle rotational maneuvers
cites work: Control of large flexible space structures
cites work: Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
cites work: Global stabilization of flexible multibody spacecraft using quaternion-based nonlinear control law
cites work: Q3029380
cites work: Attitude control without angular velocity measurement: a passivity approach
cites work: Q3998946
cites work: The attitude control problem
description: scientific article; zbMATH DE number 1869146