연구동향 분석

LMI 방법을 이용한 방사형 인공위성 제어로직 설계 및 강건성 분석

이승우(Seung-Wu Rhee) 2015년

논문상세정보
인용/피인용
' LMI 방법을 이용한 방사형 인공위성 제어로직 설계 및 강건성 분석' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • controller(h
  • lmi(선형 행렬 부등식)
  • radial type satellite(방사형 인공위성)
  • robust performance(강건한 성능)
  • robust stability(강건한 안정성)
  • spacecraft attitude control(위성자세제어)
  • μ-analysis(뮤 해석)
  • 제어기)
  • h
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
19 0

0.0%

' LMI 방법을 이용한 방사형 인공위성 제어로직 설계 및 강건성 분석' 의 참고문헌

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