Pages that link to "Item:Q2515229"
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The following pages link to On the stability of a planar resonant rotation of a satellite in an elliptic orbit (Q2515229):
Displaying 16 items.
- On the stability of resonant rotation of a symmetric satellite in an elliptical orbit (Q327547) (← links)
- Synchronization and antisynchronization of a planar oscillation of satellite in an elliptic orbit via active control (Q763151) (← links)
- On the evection resonance and its connection to the stability of outer satellites (Q955944) (← links)
- On the constructive algorithm for stability analysis of an equilibrium point of a periodic Hamiltonian system with two degrees of freedom in the second-order resonance case (Q1795451) (← links)
- On the stability of periodic Mercury-type rotations (Q1795456) (← links)
- Stability and bifurcation of resonance periodic motions of a symmetric satellite (Q2199056) (← links)
- On the constructive algorithm for stability investigation of an equilibrium point of a periodic Hamiltonian system with two degrees of freedom in first-order resonance case (Q2226122) (← links)
- Spin-orbital resonance motion of a satellite with two flexible viscoelastic rods in an elliptical orbit (Q2226149) (← links)
- Periodic solutions for a dumbbell satellite equation (Q2308167) (← links)
- Existence and stability of periodic oscillations of a rigid dumbbell satellite around its center of mass (Q2356878) (← links)
- On the Orbital Stability of Pendulum-like Oscillations of a Heavy Rigid Body with a Fixed Point in the Bobylev – Steklov Case (Q3391312) (← links)
- On the Orbital Stability of Pendulum Oscillations of a Dynamically Symmetric Satellite (Q6054852) (← links)
- Investigation of the nonlinear stability of a pendulum with variable length in elliptic orbit (Q6120360) (← links)
- Stability analysis of resonant rotation of a gyrostat in an elliptic orbit under third-and fourth-order resonances (Q6169683) (← links)
- On the orbital stability of pendulum periodic motions of a heavy rigid body with a fixed point in the case of principal inertia moments ratio 1 : 4 : 1 (Q6544365) (← links)
- Analytical solutions and stability of periodic attitude motions of gyrostat spacecrafts in weakly elliptical orbits (Q6669798) (← links)
