Optimal stabilization of a gyrostabilized satellite's positions with respect to equilibrium

Details Optimal stabilization of a gyrostabilized satellite's positions with respect to equilibrium Optimal stabilization of a gyrostabilized satellite's positions with respect to equilibrium

Oct 1976

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1976primm..40..800s&link_type=abstract

Prikladnaia Matematika i Mekhanika, vol. 40, Sept.-Oct. 1976, p. 800-807. In Russian.

Mathematics

Attitude Stability, Center Of Gravity, Circular Orbits, Gyrostabilizers, Optimal Control, Satellite Attitude Control, Asymptotic Methods, Euler Equations Of Motion, Inertial Coordinates, Kepler Laws, Mathematical Models, Moments Of Inertia, Perturbation Theory

Scientific paper

A method proposed by Rumiantsev (1970) is used in the present paper to
study the optimal attitude stabilization of a satellite by means of
rotors. The center of mass of the gyrostabilized satellite is assumed to
move as a material particle along a Keplerian orbit.

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