Adaptive Nonlinear Model Predictive path tracking control for a fixed-wing unmanned aerial vehicle

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2009, Pages

  Yang, Kwangjin ^a   Sukkarieh, Salah ^a   Kang, Yeonsik ^b  

^a UNIVERSITY OF SYDNEY   (Australia)

^b Korea Institute of Science and Technology   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ACCURATE TRACKING; ACTUATOR SATURATIONS; CLUTTERED ENVIRONMENTS; CONTROL HORIZON; CONTROL INPUTS; COST METRICS; GRADIENT DESCENT METHOD; LINEAR CONTROLLERS; MAXIMUM ERROR; MULTIPLE OBJECTIVES; NON-LINEAR MODEL; NON-LINEARITY; NONLINEAR MODEL PREDICTIVE CONTROL; OBJECTIVE FUNCTIONS; OPTIMIZATION ALGORITHMS; PATH CURVATURE; PATH TRACKING CONTROL; PHYSICAL LIMITATIONS; REAL-TIME IMPLEMENTATIONS; REFERENCE TRAJECTORIES; SIMULATION RESULT; SPEED-UPS; STATE CONSTRAINTS; SYSTEM DYNAMICS; TERMINATION CONDITION; TRACKING PERFORMANCE; UNMANNED AIRCRAFTS;

ACTUATORS; AIRCRAFT CONTROL; COMPUTATIONAL COMPLEXITY; FIXED WINGS; LINEAR CONTROL SYSTEMS; NAVIGATION; OPTIMIZATION; PREDICTIVE CONTROL SYSTEMS; REMOTELY OPERATED VEHICLES;

MODEL PREDICTIVE CONTROL;

EID: 78049264007     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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