Observational analysis investigates resonant rotations in circular orbit, suggesting implications for satellite stabilization.
For a three-axis satellite with a ball damper, resonant rotations in the central gravitational field are studied. The equations of the rotational motion of a satellite in an elliptical orbit are obtained. For the case of a circular orbit, spatial resonance rotations of 1 : 1 and 2 : 1 were investigated using the averaging method.
No takes yet. Share an insight, caveat, or question.
N. I. Amel’kin (2025) studied this question.
Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context: