Adaptive control of pitch angle for laas "Helicopter" benchmark

12th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2005

Volumn , Issue , 2005, Pages 33-39

  Andrievsky, B R ^a   Arzelier, D ^b   Fradkov, A L ^a   Peaucelle, D ^b  

^a INSTITUTE OF PROBLEMS OF MECHANICAL ENGINEERING   (Russian Federation)

^b LAAS CNRS   (France)

Author keywords

Adaptive control; Autopilot design; Experimental results; Helicopter benchmark

Indexed keywords

AIRCRAFT CONTROL; CLOSED LOOP SYSTEMS; CONTROL THEORY; ENVIRONMENTAL REGULATIONS; HELICOPTERS; MATLAB; NAVIGATION SYSTEMS;

ADAPTIVE CONTROL; ADAPTIVE CONTROL LAW; AUTOPILOT DESIGNS; EXPERIMENTAL RESULTS; HELICOPTER BENCHMARK; PARAMETRIC UNCERTAINTIES; REAL WORLD EXPERIMENT; SOFTWARE ENVIRONMENTS;

MODEL REFERENCE ADAPTIVE CONTROL;

EID: 84913585750     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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