Wingbeat shape modulation for flapping-wing micro-air-vehicle control during hover

Journal of Guidance, Control, and Dynamics

Volumn 33, Issue 3, 2010, Pages 724-739

  Doman, David B ^a,b   Oppenheimer, Michael W ^a,b   Sigthorsson, David O ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Building 146   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR; AIRCRAFT CONTROL; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; CONTROL SYSTEM SYNTHESIS; HORIZONTAL WELLS; MODULATION; WINGS;

AERODYNAMIC FORCES; ANALYTICAL TREATMENT; BLADE-ELEMENT THEORY; FLAPPING WING MICRO AIR VEHICLE; INDEPENDENT CONTROL; KINEMATIC PARAMETERS; OSCILLATORY MOTION; UNSTEADY AERODYNAMICS;

MICRO AIR VEHICLE (MAV);

EID: 77953790048     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.47146     Document Type: Article

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