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Volumn 2, Issue , 2004, Pages 802-827

Design and simulation of sailcraft attitude control systems using the solar sail control toolbox

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER AIDED DESIGN; COMPUTER GRAPHICS; COMPUTER SIMULATION; COMPUTER SOFTWARE; CONTROL THEORY; DEGREES OF FREEDOM (MECHANICS); MATHEMATICAL MODELS; MATHEMATICAL TRANSFORMATIONS; SOLAR SYSTEM; SPACECRAFT; VECTORS;

EID: 19644389494     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-4890     Document Type: Conference Paper
Times cited : (17)

References (8)
  • 1
    • 0028405279 scopus 로고
    • Radiative force model performance for topex/poseidon precision orbit determination
    • April-June
    • Scott B. Luthcke Andrew Marshall. Radiative force model performance for topex/poseidon precision orbit determination. The Journal of the Astronautical Sciences, 42(2):229-246, April-June 1994.
    • (1994) The Journal of the Astronautical Sciences , vol.42 , Issue.2 , pp. 229-246
    • Scott, B.1    Marshall, L.A.2
  • 6
    • 0014821437 scopus 로고
    • A set of r dynamical attitude equations for an arbitrary n-body satellite having r rotational degrees of freedom
    • July
    • W. W. Hooker. A set of r dynamical attitude equations for an arbitrary n-body satellite having r rotational degrees of freedom. AIAA Journal, July 1970.
    • (1970) AIAA Journal
    • Hooker, W.W.1
  • 7
    • 0003843842 scopus 로고
    • Earth radiation pressure effects on satellites
    • number 88-4292-CP
    • B. D. Tapley P. C. Knocke, J. C. Ries. Earth radiation pressure effects on satellites. In AIAA. number 88-4292-CP, 1988.
    • (1988) AIAA
    • Tapley, B.D.1    Knocke, P.C.2    Ries, J.C.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.