G - Physics – 05 – D
Patent
G - Physics
05
D
341/97
G05D 1/08 (2006.01) B64G 1/32 (2006.01) B64G 1/44 (2006.01) B64G 1/26 (2006.01) B64G 1/28 (2006.01)
Patent
CA 2018386
ABSTRACT OF THE DISCLOSURE A satellite comprising a deployable solar generator that can be oriented relative to the satellite body is kept facing the sun at all times. It includes an attitude stabilization device comprising a superconductive material closed loop carried by a support coupled to the solar generator and disposed on a side of the support facing substantially away from the sun. A secondary loop parallel to the closed loop is substantially the same shape and size as the closed loop, and is carried by the support near the loop. A resistive circuit is carried by the support near at least part of the closed loop. A selective electrical power supply circuit is connected electrically to the secondary loop and to the resistive circuit.
Aerospatiale Societe Nationale Industrielle
Reboux Alain
Riches Mckenzie & Herbert Llp
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