Flight dynamic stability of a flapping wing Micro Air Vehicle in hover

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn , Issue , 2011, Pages

  Su, Weihua ^a   Cesnik, Carlos E S ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BODY FRAMES; DYNAMIC FORMULATION; EULER ANGLES; FLAPPING WING; FLAPPING WING MICRO AIR VEHICLE; FLOQUET THEORY; GEOMETRICALLY NONLINEAR; GOVERNING EQUATIONS; LATERAL STABILITY; LOAD CALCULATION; STABILITY ANALYSIS; TRANSITION MATRICES; WING FLAPPING;

FLEXIBLE WINGS; FLIGHT DYNAMICS; RIGID WINGS; STRUCTURAL DYNAMICS;

NONLINEAR EQUATIONS;

EID: 84872432103     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2011-2009     Document Type: Conference Paper

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