메뉴 건너뛰기




Volumn 16, Issue 5-6, 1996, Pages 291-296

Three-axis reaction wheel attitude control system for KITSAT-3 microsatellite

Author keywords

[No Author keywords available]

Indexed keywords


EID: 0242538176     PISSN: 08929270     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0892-9270(96)00026-7     Document Type: Article
Times cited : (17)

References (5)
  • 4
    • 0024656129 scopus 로고
    • Quaternion feedback regulator for spacecraft eigenaxis rotations
    • Wie, B., Weiss H. and Arapostathis, A., Quaternion feedback regulator for spacecraft eigenaxis rotations. Journal of Guidance, 1989, 12, 375-380.
    • (1989) Journal of Guidance , vol.12 , pp. 375-380
    • Wie, B.1    Weiss, H.2    Arapostathis, A.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.