Application of a magnetohydrodynamic element in the control loop of a rotating spacecraft with a spike antenna

Details Application of a magnetohydrodynamic element in the control loop of a rotating spacecraft with a spike antenna Application of a magnetohydrodynamic element in the control loop of a rotating spacecraft with a spike antenna

Apr 2009

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2009cosre..47..156n&link_type=abstract

Cosmic Research, Volume 47, Issue 2, pp.156-172

Physics

45.20.Dc

Scientific paper

The problem of stabilization of a rotating spacecraft with a flexible spike antenna located along the axis of spacecraft rotation is considered. A magnetohydrodynamic element is used as a final-control element in the control loop of spacecraft attitude, and the solar direction sensor serves as a measuring device. At the first stage of investigation, the problem of stability is considered for stationary and non-stationary modes of rotation of the spacecraft with a flexible antenna and with a cavity partially filled with a low-viscosity liquid.

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