Dynamics and control of a biomimetic vehicle using biased wingbeat forcing functions: Part I - Aerodynamic model

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2010, Pages

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

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; BIOMIMETICS; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; FREQUENCY MODULATION; MICRO AIR VEHICLE (MAV); ULTRASONIC DEVICES;

AERODYNAMIC MODELING; BLADE-ELEMENT THEORY; DEGREE OF FREEDOM; DYNAMICS AND CONTROL; FLAPPING WING MICRO AIR VEHICLE; FORCING FUNCTION; MULTI DEGREE-OF-FREEDOM; PITCHING MOMENTS;

WINGS;

EID: 77955917456     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-1023     Document Type: Conference Paper

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