Robust control of a 3-DOF flapping wing micro air vehicle

AIAA Guidance, Navigation, and Control Conference

Volumn , Issue , 2010, Pages

  Serrani, Andrea ^a   Keller, Benjamin E ^a   Bolender, Michael A ^b   Doman, David B ^b  

^a The Ohio State University   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATION MECHANISM; AVERAGING THEORY; BOUNDED FEEDBACK; CONTROL DESIGN; FIXED STRUCTURE; FLAPPING WING MICRO AIR VEHICLE; FLAPPING-WING; PLANE ANGLES; SET-POINT CONTROL; STABILITY ANALYSIS; VEHICLE POSITION;

ROBUST CONTROL; WINGS;

LONGITUDINAL CONTROL;

EID: 84867076353     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-7709     Document Type: Conference Paper

References (11)

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