Design of the RLG Current Stabilizer Circuit for Attitude Control in the Satellite

Details Design of the RLG Current Stabilizer Circuit for Attitude Control in the Satellite Design of the RLG Current Stabilizer Circuit for Attitude Control in the Satellite

Jun 2006

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2006jass...23..161k&link_type=abstract

Journal of Astronomy and Space Sciences. Vol. 23, no. 2, 161-166

Astronomy and Astrophysics

Astronomy

Rlg, Attitude Control, Current Stabilizer, Bias Error

Scientific paper

In this paper, we describe the RLG current stabilizer circuit for attitude control in the satellite. The RLG makes use of the Sagnac effect within a resonant of a HeNe laser. The difference between two discharge currents causes one of the gyro bias errors. The theoretical background and current stabilizer are introduced. It is verified that the circuit designed is applicable to the test of input voltage and temperature.

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