Bifurcation and stability of the relative equilibria of a gyrostat satellite

DOI10.1016/0021-8928(91)90052-VzbMath0785.70019MaRDI QIDQ1314018

V. N. Rubanovskij

Publication date: 2 March 1994

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

zbMATH Keywords

bifurcation diagramcentral triaxial ellipsoid of inertiagyrostatic torquerotor axis

Mathematics Subject Classification ID

Stability for nonlinear problems in mechanics (70K20) Orbital mechanics (70M20) Motion of the gyroscope (70E05)

Related Items (6)

Chaos and optimal control of steady-state rotation of a satellite-gyrostat on a circular orbit ⋮ Heteroclinic chaos and its local suppression in attitude dynamics of an asymmetrical dual-spin spacecraft and gyrostat-satellites. I: Main models and solutions ⋮ Heteroclinic chaos and its local suppression in attitude dynamics of an asymmetrical dual-spin spacecraft and gyrostat-satellites. II: The heteroclinic chaos investigation ⋮ The equilibrium positions of a satellite carrying a three-degree-of-freedom powered gyroscope in a central gravitational field ⋮ The stability of a family of non-trivial equilibrium orientations to the attracting centre of a gyrostat with an elastic rod ⋮ The Set of Relative Equilibria of a Stationary Orbital Asymmetric Gyrostat

Cites Work

• On the set op steady motions of a gyrostat satellite in a central Newtonian force field and the stability of these motions

This page was built for publication: Bifurcation and stability of the relative equilibria of a gyrostat satellite