Control strategy design for the transitional mode of tiltrotor UAV

IEEE International Conference on Industrial Informatics (INDIN)

Volumn , Issue , 2012, Pages 248-253

  Fang, Xiaoxing ^a   Lin, Qing ^a   Wang, Yingxun ^a   Zheng, Lili ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

dynamic inversion; extended state observer; tiltrotor; transitional mode; UAV

Indexed keywords

CONTROL LOOP; CONTROL STRATEGIES; DYNAMIC CONTROL ALLOCATIONS; DYNAMIC INVERSION; DYNAMIC MODEL INVERSION; EXTENDED-STATE-OBSERVER; MATHEMATIC MODEL; MODE CONVERSIONS; MOMENT BALANCE; REFERENCE MODELS; TILT ROTOR; TIME SCALE SEPARATION; TRANSITIONAL MODE; UNKNOWN DISTURBANCE;

AERODYNAMICS; INFORMATION SCIENCE; MACHINERY; UNMANNED AERIAL VEHICLES (UAV);

STRUCTURAL DESIGN;

EID: 84868252099     PISSN: 19354576     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/INDIN.2012.6300840     Document Type: Conference Paper

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