메뉴 건너뛰기




Volumn , Issue , 2009, Pages 126-130

Design and development of a 5-DOF air-bearing spacecraft simulator

Author keywords

Air bearing; Cold gas propulsion system; Image process; Spacecraft simulator

Indexed keywords

AIR-BEARING; AIR-BEARING SPACECRAFT SIMULATOR; AUTONOMOUS FORMATION FLYINGS; COLD GAS PROPULSION SYSTEM; DEGREES OF FREEDOM; DESIGN AND DEVELOPMENT; EARTH-BOUND LABORATORIES; HARBIN INSTITUTE OF TECHNOLOGY; IMAGE PROCESS; LOW FRICTION; ORBITAL MANEUVERS; RESEARCH PROBLEMS; SPACECRAFT SIMULATOR; WORKING PRINCIPLES;

EID: 67649382960     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/CAR.2009.7     Document Type: Conference Paper
Times cited : (36)

References (2)
  • 2
    • 46449107916 scopus 로고    scopus 로고
    • Design of improved nonlinear tracking differentiator
    • June.
    • Shi Yong-Li, Hou Chao-Zhen, "Design of improved nonlinear tracking differentiator," Control and Decision, Vol. 23, June. 2008, pp. 647-650.a
    • (2008) Control and Decision , vol.23
    • Yong-Li Shi1    Chao-Zhen Hou2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.