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Volumn 4, Issue , 2002, Pages 4078-4083

A satellite attitude controller using nonlinear H∞ approach

Author keywords

[No Author keywords available]

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; HAMILTONIANS; OPTIMAL CONTROL SYSTEMS; PARTIAL DIFFERENTIAL EQUATIONS; SATELLITES; STATE FEEDBACK; SYSTEM STABILITY; VECTORS;

EID: 0036991390     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (7)

References (9)
  • 1
    • 0242712746 scopus 로고
    • Space station attitude control and momentum management: A nonlinear look
    • S.R. Vadali and H.S.Oh, "Space station attitude control and momentum management: a nonlinear look", J. Guidance, Control and Dynamics, Vol.16, pp 1-8, 1991.
    • (1991) J. Guidance, Control and Dynamics , vol.16 , pp. 1-8
    • Vadali, S.R.1    Oh, H.S.2
  • 2
    • 0024731418 scopus 로고
    • New approach to attitude/momentum control for the space station
    • B.Wie, K.W Byun and V. W Warren, "New approach to attitude/momentum control for the space station", J. Gudance. Control and Dynamics, vol. 12, No. 5, pp 714-722, 1989.
    • (1989) J. Gudance. Control and Dynamics , vol.12 , Issue.5 , pp. 714-722
    • Wie, B.1    Byun, K.W.2    Warren, V.W.3
  • 4
    • 0029342198 scopus 로고
    • ∞ control and its application to rigid spacecraft
    • ∞ control and its application to rigid spacecraft", IEEE Trans. on Automatic Control, Vol. 40, pp1281-1285, 1995.
    • (1995) IEEE Trans. on Automatic Control , vol.40 , pp. 1281-1285
    • Kang, W.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.