Stabilization due to gyroscopic coupling in dual-spin satellites subject to gravitational torques
From MaRDI portal
Publication:3930701
DOI10.1007/BF01234177zbMath0475.70029OpenAlexW2035753671MaRDI QIDQ3930701
No author found.
Publication date: 1981
Published in: Celestial Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/bf01234177
circular orbitsattitude stabilizationregions of stabilitydual spin satellitesgravity gradient stabilization of gyrostat satellitesinfinitesimal stability and instability
Related Items (9)
Steady motions in controlled gyrostat systems ⋮ Solutions homoclinic to regular precessions of a symmetric satellite ⋮ Investigation of equilibria of a satellite subjected to gravitational and aerodynamic torques ⋮ Hamiltonian and chaotic attitude dynamics of an orbiting gyrostat satellite under gravity-gradient torques ⋮ Application of computer algebra methods for investigation of stationary motions of a gyrostat satellite ⋮ Dynamics of a gyrostat satellite subjected to the action of gravity moment. Equilibrium attitudes and their stability ⋮ Symbolic-numerical methods of studying equilibrium positions of a gyrostat satellite ⋮ Bifurcations of the relative equilibria of a gyrostat satellite for a special case of the alignment of its gyrostatic moment ⋮ Dynamics of an axisymmetric gyrostat satellite. Equilibrium positions and their stability
Cites Work
- Unnamed Item
- Differential equations: Stability, oscillations, time lags
- Non-linear resonant attitude motions in gravity-stabilized gyrostat satellites
- On the Stability of Equilibrium Sets of Discrete Conservative Mechanical Systems
- The quadratic approximation in rotational dynamical equations
- Stability of orbiting gyrostats in the elementary cases
- Stability Analysis of All Possible Equilibria for Gyrostat Satellities under Gravitational Torques
- Stable tumbling motions of a dual-spin satellite subject to gravitational torques.
This page was built for publication: Stabilization due to gyroscopic coupling in dual-spin satellites subject to gravitational torques