Mathematical modelling and stabilization of large flexible spacecraft subject to orbital perturbation
type: Item
instance of: scholarly article
title: Mathematical modelling and stabilization of large flexible spacecraft subject to orbital perturbation
zbMATH Open document ID: 0697.70026
DOI: 10.1016/0895-7177(89)90326-9
author: N. E. Zubov
published in: Mathematical and Computer Modelling
publication date: 1989-01-01T00:00:00Z
Mathematics Subject Classification ID: 70M20
Mathematics Subject Classification ID: 70K99
Mathematics Subject Classification ID: 70Q05
zbMATH DE Number: 4143511
zbMATH Keywords: modelling of large flexible spacecraft
zbMATH Keywords: stabilization under the influence of orbital (radial) perturbation
zbMATH Keywords: Hamilton's principle
zbMATH Keywords: Lyapunov's approach
MaRDI profile type: Publication
full work available at URL: 0895-7177(89)90326-9
OpenAlex ID: W2070523362
cites work: Modelling of flexible spacecraft and their stabilization†
cites work: Stabilization of a class of hybrid systems arising in flexible spacecraft
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cites work: Q5552615
cites work: Hamilton's principle - Finite-element methods and flexible body dynamics
cites work: Long-term coupling effects between librational and orbital motions of a satellite
cites work: Stability of flexible spacecrafts
description: scientific article; zbMATH DE number 4143511