Modeling and control design for a flapping-wing nano air vehicle

AIAA Guidance, Navigation, and Control Conference

Volumn , Issue , 2010, Pages

  Geder, Jason D ^a,d   Ramamurti, Ravi ^a,d   Sandberg, William C ^b,d   Flynn, Anita ^c,e  

^a NAVAL RESEARCH LABORATORY   (United States)

^b SCIENCE APPLICATIONS INTERNATIONAL CORPORATION   (United States)

^c MicroPropulsion Corporation   (United States)

^d Laboratory for Computational Physics and Fluid Dynamics   (United States)

^e Modeling and Analysis Division   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR VEHICLE; ATTITUDE ESTIMATION; CONTROL MODULE; FLAPPING-WING; FORWARD FLIGHT; MODELING AND CONTROL; PLANE ANGLES; SIX-DEGREE-OF-FREEDOM; VEHICLE DYNAMICS; VEHICLE MODEL; VEHICLE RESPONSE; WING KINEMATICS;

SENSORY FEEDBACK;

ACTUATORS;

EID: 84867051633     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-7556     Document Type: Conference Paper

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