Rigid multi-body equations-of-motion for flapping wing MAVs using Kane's Equations

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2009, Pages

  Bolender, Michael A ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AUTOMOBILE BODIES; EQUATIONS OF MOTION; FLIGHT DYNAMICS; RIGID STRUCTURES; RIGID WINGS;

AERODYNAMIC FORCES; FLAPPING WING MICRO AIR VEHICLE; INERTIAL EFFECT; KANE'S EQUATION; MECHANICAL COMPLEXITY; MULTIPLE JOINTS; OPEN LOOP DYNAMICS; VEHICLE CONFIGURATION;

MICRO AIR VEHICLE (MAV);

EID: 78049263011     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-6158     Document Type: Conference Paper

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