Dynamics of a gyrostat satellite subjected to the action of gravity moment. Equilibrium attitudes and their stability

We study the dynamics of the rotational motion of a gyrostat satellite moving in the central Newtonian force field along a circular orbit. We propose a method for determining the equilibrium attitudes (equilibrium orientations) of a gyrostat satellite in the orbital coordinate system for given value...

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Bibliographic Details
Main Author: Gutnik, S. A. (author)
Other Authors: Santos, Luís (author), Sarychev, V. A. (author), Silva, A. R. R. (author)
Format: article
Language:eng
Published: 2018
Subjects:
Positions
Vector
Real Root
System Science International
Direction Cosine
Stable Orientation
Axisymmetric Case
Lyapunov functions
Satellites
Stability
Dimensionless Parameters
Equilibrium Orientations
Existence Conditions
Gravitational Systems
Gyrostat Satellite
Orbital Coordinate System
Rotational Motion
Stability Condition
Orbits
Online Access:http://hdl.handle.net/10400.6/4756
Country:Portugal
Oai:oai:ubibliorum.ubi.pt:10400.6/4756

Internet

http://hdl.handle.net/10400.6/4756

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