Attitude dynamics of a rigid body on a Keplerian orbit: A simplification
type: Item
instance of: scholarly article
title: Attitude dynamics of a rigid body on a Keplerian orbit: A simplification
zbMATH Open document ID: 0767.70005
DOI: 10.1007/BF00692512
author: M. Arribas
author: Antonio Elipe
published in: Celestial Mechanics and Dynamical Astronomy
publication date: 1993-05-16T00:00:00Z
Mathematics Subject Classification ID: 70E15
Mathematics Subject Classification ID: 70F05
Mathematics Subject Classification ID: 70H05
Mathematics Subject Classification ID: 70M20
zbMATH DE Number: 167666
zbMATH Keywords: Lie series
zbMATH Keywords: triaxial rigid body
zbMATH Keywords: Euler-Poinsot model
zbMATH Keywords: moments of inertia
MaRDI profile type: Publication
cites work: Effects of gravity-gradient torque on the rotational motion of A triaxial satellite in a precessing elliptic orbit
cites work: Simplify or perish
cites work: The General Problem of the Motion of Coupled Rigid Bodies about a Fixed Point
full work available at URL: https://doi.org/10.1007/bf00692512
OpenAlex ID: W2008691587
description: scientific article; zbMATH DE number 167666