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Stabilization Control Method Development for Single Axis Unstable System Using SGCMG

SGCMG를 이용한 단축 불안정 시스템의 안정화 제어 기법 개발

  • 이준식 (한국항공대학교 항공우주기계공학과) ;
  • 이준용 (한국항공대학교 항공우주기계공학과) ;
  • 유지훈 (한국항공대학교 항공우주기계공학과) ;
  • 김지철 (한국항공대학교 항공우주기계공학과) ;
  • 전동익 (한국항공대학교 항공우주기계공학과) ;
  • 오화석 (한국항공대학교 항공우주기계공학과)
  • Received : 2013.11.27
  • Accepted : 2013.12.20
  • Published : 2013.12.31

Abstract

Control Moment Gyroscope(CMG) is one of the most efficient momentum exchange devices for satellite attitude control and essential device for agile maneuver system. This paper presents the details of a designed Single Gimbal CMG with a constant speed momentum wheel and single axis attitude control unstable to stable. In order to keep the naturally unstable equivalent point, it should be controlling the gimbal constantly. The experimental data are compared with theoretical result and requirements are used to verify their performance specifications.

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