저궤도 위성 자세제어용 RLG 전류 안정화 회로 설계

다국어 초록 (Multilingual 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 BeNe 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.

목차 (Table of Contents)

• Abstract
• 1. 서론
• 2. 전류 안정화 회로
• 3. 회로 설계 및 시험
• 5. 결론
• 참고문헌
• 저자소개

참고문헌 (Reference)

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5 H. Malthan, "Test of a Honeywell GG1342 Ring Laser Gyro" 20-, 1982

6 W. G. Albrecht, "State of the Art of German RLG Development : Latest Test Results of the Honeywell Sondertechnik Gyro DGD 800" 110-, 1986

7 T. J. Hutchings, "Scale Factor Nonlinearity of a Body Dither Laser Gyro" IEEE 549-, 1978

8 F. Aronowitz, "Mode Coupling Due to Backscattering in a He-Ne Traveling Wave Ring Laser" 55 : 1966

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12 최용진, "Characteristic Test of Ring Laser Gyro for Inertial Navigation" 7 : 154-, 1997

13 J. B. Matthews, "A High Resolution Laser Gyro" IEEE 556-, 1978