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Volumn , Issue , 2011, Pages

Roll control of a UAV using an Adaptive Torsion Structure

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTIC STRUCTURES; CONTROL CONSTRAINT; LOAD PATHS; MULTIDISCIPLINARY DESIGN OPTIMIZATION; OPTIMIZERS; ROLLING MOMENTS; TORSIONAL STIFFNESS;

EID: 80052391816     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2011-1834     Document Type: Conference Paper
Times cited : (10)

References (26)
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    • 64049091690 scopus 로고    scopus 로고
    • Adaptive stiffness structures for air vehicle drag reduction
    • Meeting Proceedings RTO-MP-AVT-141, Paper 15.Nueuilly-sur-Seine, France: RTO
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    • Cooper, J.E.1
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    • A vortex lattice MATLAB implementation for linear aerodynamic wing applications
    • December
    • Melin, T., "A Vortex Lattice MATLAB Implementation for Linear Aerodynamic Wing Applications," Royal Institute of Technology (KTH), December 2000.
    • (2000) Royal Institute of Technology (KTH)
    • Melin, T.1
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    • 37349111674 scopus 로고    scopus 로고
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    • (submitted for review)
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.