Open loop pitch control of a flapping wing micro-air vehicle using a tail and control mass

Proceedings of the 2010 American Control Conference, ACC 2010

Volumn , Issue , 2010, Pages 536-541

  Orlowski, Christopher ^a   Girard, Anouck ^a   Shyy, Wei ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROL; AUTOMOBILE BODIES; LONGITUDINAL CONTROL; RIGID STRUCTURES; RIGID WINGS;

CONTROL METHODS; D' ALEMBERT'S PRINCIPLE; FLAPPING WING MICRO AIR VEHICLE; LONGITUDINAL ORIENTATION; LONGITUDINAL OSCILLATIONS; MULTIPLE RIGID BODIES; OPEN-LOOP METHOD; PITCH CONTROL;

MICRO AIR VEHICLE (MAV);

EID: 77957792345     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/acc.2010.5530878     Document Type: Conference Paper

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