Dynamic model and attitude control of flapping wing micro aerial vehicle

2009 IEEE International Conference on Robotics and Biomimetics, ROBIO 2009

Volumn , Issue , 2009, Pages 451-456

  Duan, Hongjun ^a   Li, Qingwei ^a  

^a NORTHEASTERN UNIVERSITY AT QINHUANGDAO   (China)

Author keywords

Adaptive robust control; Attitude control; Dynamic model; Flapping wing; Micro aerial vehicle

Indexed keywords

ADAPTIVE CONTROLLERS; ADAPTIVE ROBUST CONTROL; ATTITUDE CONTROLLER; CONTROL STRATEGIES; FEEDBACK CONTROLLER; FLAPPING WING; MICRO AERIAL VEHICLE; NOMINAL MODELS; NON-LINEARITY; ROBUST CONTROLLERS; SIMULATION RESULT; STRUCTURED UNCERTAINTIES; SYSTEM UNCERTAINTIES; UNSTRUCTURED UNCERTAINTY;

AEROSPACE VEHICLES; ATTITUDE CONTROL; BIOMIMETICS; CONTROLLERS; DYNAMIC MODELS; DYNAMICS; NAVIGATION; ROBOTICS; ROBUST CONTROL; SPATIAL VARIABLES CONTROL; VEHICLES;

ADAPTIVE CONTROL SYSTEMS;

EID: 77951429020     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ROBIO.2009.5420689     Document Type: Conference Paper

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