Magnetic attitude control system for low-Earth orbit satellites
type: Item
instance of: scholarly article
title: Magnetic attitude control system for low-Earth orbit satellites
zbMATH Open document ID: 0994.70021
DOI: 10.1023/A:1011484008063
published in: Multibody System Dynamics
publication date: 2002-10-07T00:00:00Z
review text: The stabilization of a small spacecraft on the low-Earth orbit is done by a three-axis magnetometer. Both orbital motion parameters and attitude can be estimated by the vector function Lyapunov method. The authors also propose a recursive state estimation algorithm with enhanced convergence.
reviewed by: Johannes Viktor Feitzinger
Mathematics Subject Classification ID: 70M20
Mathematics Subject Classification ID: 70Q05
zbMATH DE Number: 1655763
zbMATH Keywords: magnetic attitude control
zbMATH Keywords: stabilization of spacecraft
zbMATH Keywords: low-Earth orbit
zbMATH Keywords: three-axis magnetometer
zbMATH Keywords: vector function Lyapunov method
zbMATH Keywords: recursive state estimation algorithm
zbMATH Keywords: enhanced convergence
MaRDI profile type: Publication
full work available at URL: a:1011484008063
OpenAlex ID: W135447109
author: D. Lebedev
author: Alexandra Tkachenko
description: scientific article; zbMATH DE number 1655763