연구동향 분석

CMG를 이용한 쿼드-로터의 자세제어

오경현(Kyung-Hyun Oh) 최호림(Ho-Lim Choi) 2014년

논문상세정보
인용/피인용
' CMG를 이용한 쿼드-로터의 자세제어' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • 전자공학
  • cmg
  • gyroscopicmoments
  • quad-rotor
  • reactionwheel
  • state feedback controller
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
2,328 0

0.0%

' CMG를 이용한 쿼드-로터의 자세제어' 의 참고문헌

  • 모멘텀 바이어스 인공위성의 2축 자세제어 시스템 설계
    이승우 한국항공우주학회지 34 (4) : 40 ~ 46 [2006]
  • Torque amplication of control moment gyros
    V. Lappas Electronics Letters 38 (15) : 837 ~ 839 [2002]
  • Steering law design for redun-dant single gimbal control moment gyro systems
    N. S. Bedrossian Massachusetts Inst. of Technology [1987]
  • Singularity robust steering logic for gyros
    W. Bong Journal of Guidance, Control and Dynamics 24 (5) : 865 ~ 872 [2002]
  • Redundant single-gimbal control moment gyroscope singularity analysis
    N. S. Bedrossian Journal of Guidance, Control, Dynamics 13 (6) : 1096 ~ 1101 [1990]
  • Real-time stabilization and tracking of a four-rotor mini rotorcraft control systems technology
    P. Castillo IEEE Transactions on Control Systems Technology 12 (4) : 510 ~ 516 [2004]
  • Rapid multi target acquisition and pointing control of agile spacecraft
    W. Bong Journal of Guidance, Control and Dynamics 25 (1) : 96 ~ 104 [2002]
  • PinkWink
  • Multi-copter
  • Manual for model 750 control moment gyroscope
    T. R. Parks ECP Educational Control Products [1999]
  • Feedback control and steer-ing laws for spacecraft using single gimbal control moment gyros
    H. S. Oh The Journal of the Astronautical Sciences 39 (2) : 183 ~ 203 [1991]
  • Design and control of quadrotors with application to autonomous flying
    S. Bouabdallah Ecole Polytechnique Federale de Lausanne [2007]
  • Attitude stabilization of rigid spacecraft using two momentum wheels
    S. P. Kim Journal of the Korean Society for Aeronautical and Space Sciences 29 (4) : 78 ~ 85 [2001]
  • Attitude stabilization of a four-rotor aerial robot
    McGilvray, S. Tayebi, A. Proc. IEEE Int. Conf. on Decision and Control : 1216 ~ 1221 [2004]