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

저궤도 위성 자세제어용 RLG 전류 안정화 회로 설계

  • Published : 2008.01.01

Abstract

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.

Keywords

References

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