Optimal damping of nutational motion of spin-stabilized satellites

Details Optimal damping of nutational motion of spin-stabilized satellites Optimal damping of nutational motion of spin-stabilized satellites

May 1976

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1976cemec..13..383s&link_type=abstract

Celestial Mechanics, vol. 13, May 1976, p. 383-405. In Russian.

Computer Science

Nutation Dampers, Optimal Control, Rotary Stability, Satellite Rotation, Spin Stabilization, Viscous Damping, Cylindrical Shells, Equations Of Motion, Orbital Mechanics, Steady State

Scientific paper

The paper investigates the dynamics of a satellite nutation damping system consisting of a mass on a spring placed in a cylinder filled with a viscous fluid. Damping is accomplished through the viscous-friction type interaction during the oscillations of the mass in the fluid. Neglecting the external forces acting on the satellite, the authors derive the equations of motion for the satellite-damper system. Conditions for stability of steady-state spinning are obtained, and optimal satellite and damper parameters ensuring maximal rate of damping the nutational motion are determined.

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