Variable structure attitude control for an UAV with parameter uncertainty and external disturbance

Procedia Engineering

Volumn 15, Issue , 2011, Pages 408-415

  Yang, Yueneng ^a   Wu, Jie ^a   Zheng, Wei ^a  

^a NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY   (China)

Author keywords

Attitude control; Boudary layer; Sliding mode; Uncertainty; Unmanned aerial vehicle; Varible structure control

Indexed keywords

ATTITUDE ANGLE; ATTITUDE CONTROLLER; ATTITUDE MOTIONS; BOUDARY LAYER; CHATTERING PROBLEMS; DOUBLE-LOOP; EXTERNAL DISTURBANCES; INNER LOOPS; KINEMATICS AND DYNAMICS; MULTI-INPUT MULTI-OUTPUT; NEWTON EULER FORMULATION; OUTER LOOP; PARAMETER UNCERTAINTY; SLIDING MODES; UNCERTAINTY; VARIABLE STRUCTURES; VARIBLE STRUCTURE CONTROL;

ATTITUDE CONTROL; CONTROL THEORY; CONTROLLERS; EULER EQUATIONS; INFORMATION SCIENCE; MATHEMATICAL MODELS; MIMO SYSTEMS; UNCERTAINTY ANALYSIS; UNMANNED AERIAL VEHICLES (UAV); UNMANNED VEHICLES; VARIABLE STRUCTURE CONTROL;

ADVANCED VEHICLE CONTROL SYSTEMS;

EID: 84055190579     PISSN: 18777058     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1016/j.proeng.2011.08.078     Document Type: Conference Paper

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