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Volumn 38, Issue 10, 2002, Pages 1719-1726

Output attitude tracking for flexible spacecraft

Author keywords

Dynamic control; Flexible spacecraft; Nonlinear control; Output tracking

Indexed keywords

COMPUTER SIMULATION; DYNAMICS; PARAMETER ESTIMATION; PROBLEM SOLVING; SPACECRAFT; STIFFNESS MATRIX; TRACKING (POSITION); VECTORS;

EID: 0036779229     PISSN: 00051098     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0005-1098(02)00082-1     Document Type: Article
Times cited : (104)

References (27)
  • 13
    • 84977389734 scopus 로고
    • A new method for performing digital control system attitude computations using quaternions
    • (1970) AIAA Journal , vol.8 , Issue.1 , pp. 13-17
    • Ickes, B.P.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.