Design of attitude control system for an UAV type-quadrotor based on dynamic contraction method

IEEE/ASME International Conference on Advanced Intelligent Mechatronics, AIM

Volumn , Issue , 2009, Pages 644-649

  Czyba, Roman ^a  

^a SILESIAN UNIVERSITY OF TECHNOLOGY   (Poland)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE STABILIZATION; CONTINUOUS TIME; CONTROL TASK; EULER ANGLES; EXTERNAL DISTURBANCES; INCOMPLETE INFORMATION; LINEAR DYNAMICAL SYSTEMS; ON DYNAMICS; QUADROTORS; REFERENCE SIGNALS; ROBUST REGULATION; TRACKING PROBLEM; VARYING PARAMETERS;

ASYMPTOTIC ANALYSIS; CONTROLLERS; DYNAMICAL SYSTEMS; LINEAR CONTROL SYSTEMS; MECHATRONICS; REMOTELY OPERATED VEHICLES; SHRINKAGE; UNMANNED AERIAL VEHICLES (UAV);

INTELLIGENT MECHATRONICS;

EID: 70350455538     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AIM.2009.5229940     Document Type: Conference Paper

References (10)

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