연구동향 분석

우주비행체 기동 및 자세제어 설계 검증을 위한 시뮬레이터의 냉가스 추진시스템 개발 동향

김재훈(Jaehoon Kim) 이균호(Kyun Ho Lee) 홍성경(Sung Kyung Hong) 김해동(Hae-Dong Kim) 2015년

논문상세정보
인용/피인용
' 우주비행체 기동 및 자세제어 설계 검증을 위한 시뮬레이터의 냉가스 추진시스템 개발 동향' 의 주제별 논문영향력
논문영향력 선정 방법
논문영향력 요약
주제
  • 폭발물, 연료공업
  • coldgaspropulsionsystem(냉가스추진시스템)
  • groundsimulator(지상시뮬레이터)
  • spacecraft(우주 비행체)
  • thruster(추력기)
동일주제 총논문수 논문피인용 총횟수 주제별 논문영향력의 평균
153 0

0.0%

' 우주비행체 기동 및 자세제어 설계 검증을 위한 시뮬레이터의 냉가스 추진시스템 개발 동향' 의 참고문헌

  • Using Robots for Advanced Rendezvous and Docking Simulation
    Boge, T. Simulation and EGSE facilites for Space Programmes 2012 (SESP 2012) [2012]
  • Space Debris Removal System Using a Small Satellite
    Nishida, S. I. Acta Astronautica 65 (1) : 95 ~ 102 [2009]
  • Rocket Propulsion Elements, 8th ed.
    Sutton, G. P. John Wiley & Sons Inc. [2010]
  • Propulsion System Characterization for the SPHERES Formation Flight and Docking Testbed
    Chen, A. Massachusetts Institute of Technology [2002]
  • Laboratory Experimentation of Autonomous Spacecraft Approach and Docking to a Collaborative Target
    Romano, M. Journal of Spacecraft and Rockets 44 (1) : 164 ~ 173 [2007]
  • KSLV-I RCS 추력기 개발 및 수행 평가에 대한 연구
    전상운 전자공학회논문지 - SC 47 (3) : 19 ~ 27 [2010]
  • Historical Review of Air-bearing Spacecraft Simulators
    Schwartz, J. L. Journal of Guidance, Control, and Dynamics 26 (4) : 513 ~ 522 [2003]
  • Development Trend of Spacecraft Propulsion System
    Yoo, M. J. Current Industrial and Technological Trends in Aerospace 2 (2) : 70 ~ 83 [2004]
  • Design and Intergration of a Three Degrees-of-Freedom Robotic Vehicle with Control Moment Gyro for the Autonomous Multiagent Physically Interacting Spacecraft(AMPHIS) Testbed
    Hall, J. S. Naval Postgraduate School [2006]
  • Design and Fabrication of a Planar Autonomous Spacecraft Simulator with Docking and Fluid Transfer Capacity
    Shay, T. J. Naval Postgraduate School, [2005]
  • Design and Development of a 5-DoF Air-Bearing Spacecraft Simulator
    Jian, X. 2009International Asia Conference on Informatics in Control, Automation and Robotics : 126 ~ 130 [2009]
  • Control System of a Three DoF Spacecraft Simulator by Vectorable Thrusters and Control Moment Gyros
    Price, W. D. Naval Postgraduate School [2006]
  • 박사
    Analysis of Attitude Synchronization Control for Spacecraft Formation Flying via Hardware-In-the-Loop Simulation
    정준오 Yonsei University [2010]
  • Analysis and Experimentation of Control Strategies for Underactuated Spacecraft
    Hall, J. S. Naval Postgraduate School [2009]
  • A 5-DoF Experimental Platform for Autonomous Spacecraft Rendezvous and Docking
    Cho, D.M AIAA Infotech@Aerospace Conference [2009]
  • A 3-DoF Experimental Test-Bed for Intergrated Attitude Dynamics and Control Research
    Jung, D. W. AIAA Guidance, Navigation, and Control Conference and Exhibit [2003]