Robust control design based on sliding mode control for hover flight of a mini tail-sitter unmanned aerial vehicle

IECON Proceedings (Industrial Electronics Conference)

Volumn , Issue , 2009, Pages 2342-2347

  Guerrero, J A ^a   Lozano, R ^a   Romero, G ^b   Lara Alabazares, D ^b   Wong, K C ^c  

^a UNIVERSITÉ DE TECHNOLOGIE DE COMPIÈGNE   (France)

^b Electronic Department   (Mexico)

^c UNIVERSITY OF SYDNEY   (Australia)

Author keywords

Parametric uncertainty; Robust control; Sliding mode control; UAV control

Indexed keywords

ATTITUDE DYNAMICS; CONTROL LAWS; CRUISE PERFORMANCE; FIXED WING; NATURAL FLIGHT; OPERATIONAL FLEXIBILITY; PARAMETRIC UNCERTAINTIES; PARAMETRIC UNCERTAINTY; ROBUST CONTROL DESIGNS; SIMULATION TESTS; UAV CONTROL; VARIABLE PITCH; VERTICAL FLIGHT; VERTICAL MODES;

ATTITUDE CONTROL; AUTOMOBILE ELECTRONIC EQUIPMENT; AUTOMOBILE PARTS AND EQUIPMENT; FIXED WINGS; FLIGHT CONTROL SYSTEMS; INDUSTRIAL ELECTRONICS; NAVIGATION; PROPELLERS; REMOTELY OPERATED VEHICLES; SLIDING MODE CONTROL; SPATIAL VARIABLES CONTROL; UNMANNED AERIAL VEHICLES (UAV);

ROBUST CONTROL;

EID: 77951556653     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/IECON.2009.5415267     Document Type: Conference Paper

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