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Volumn , Issue , 2007, Pages 5284-5289
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Control of longitudinal flight dynamics of a flapping-wing micro air vehicle using time-averaged model and differential flatness based controller
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Author keywords
[No Author keywords available]
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Indexed keywords
APPLIED (CO);
AVERAGING THEORY;
CONTROL SCHEMES;
DIFFERENTIAL FLATNESS;
FLIGHT CONTROLS;
HIGH-FREQUENCY (HF);
LONGITUDINAL DYNAMICS;
MICRO AIR VEHICLE (MAV);
NON-LINEAR;
ON TIME;
ORIGINAL SYSTEMS;
PAPER ADDRESSES;
SIMPLIFIED MODELS;
TIME AVERAGING;
TIME-AVERAGED;
TIME-VARYING;
TIME-VARYING DYNAMICS;
TRAJECTORY TRACKING;
AEROSPACE VEHICLES;
DYNAMICS;
FLIGHT DYNAMICS;
IMAGE SENSORS;
LINEAR CONTROL SYSTEMS;
PROPULSIVE WING AIRCRAFT;
TIME SHARING SYSTEMS;
TIME VARYING SYSTEMS;
VEHICLES;
WINGS;
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EID: 46449108847
PISSN: 07431619
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1109/ACC.2007.4283052 Document Type: Conference Paper |
Times cited : (68)
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References (8)
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