Stability of a two-rotor vertical gyroscope on board a satellite in a central Newtonian force field

Details Stability of a two-rotor vertical gyroscope on board a satellite in a central Newtonian force field Stability of a two-rotor vertical gyroscope on board a satellite in a central Newtonian force field

Jul 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978kosis..16..492g&link_type=abstract

Kosmicheskie Issledovaniia, vol. 16, July-Aug. 1978, p. 492-496. In Russian.

Physics

Equations Of Motion, Gravitational Fields, Gyroscopic Stability, Gyrostabilizers, Rotary Gyroscopes, Satellite Orientation, Angular Velocity, Differential Equations, Moments Of Inertia, Navigation Aids, Springs (Elastic)

Scientific paper

The equations of motion of a two-rotor gyroscopic system are derived for the case where the center of the system's suspension travels along a geocentric sphere and the system is situated in a central Newtonian force field. The sufficient stability conditions are obtained for a space-borne vertical gyroscope. Calculations are carried out with allowance for the moments of inertia of all the elements of the gyroscopic system.

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