Mathematical model of the motion of a flexibly stabilized satellite about its center of mass. I

Details Mathematical model of the motion of a flexibly stabilized satellite about its center of mass. I Mathematical model of the motion of a flexibly stabilized satellite about its center of mass. I

Sep 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975kosis..13..632k&link_type=abstract

Kosmicheskie Issledovaniia, vol. 13, Sept.-Oct. 1975, p. 632-637. In Russian.

Other

Magnetic Control, Mathematical Models, Nutation Dampers, Satellite Attitude Control, Spacecraft Stability, Astrodynamics, Astronavigation, Guidance Sensors

Scientific paper

Kaurov (1972) has proposed a procedure for determining the attitude of a satellite with a magnetic damper, using a technique where the navigational information contains the responses of a three-component indicator of the magnetic field intensity and some other instruments. A differential equation is derived for determining an attitude parameter that cannot be obtained from the three-component indicator.

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