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Volumn , Issue , 2009, Pages

Neuroadaptive model following controller design for non-affine non-square aircraft system

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTATION LAW; ADAPTIVE CONTROL; ADAPTIVE CONTROL DESIGNS; ADAPTIVE GAIN; AERODYNAMIC DERIVATIVES; AIRCRAFT SYSTEMS; BOUNDEDNESS; CONTROL SIGNAL; DYNAMIC INVERSION; ESTIMATION ERRORS; FAST ADAPTATIONS; HIGH FREQUENCY OSCILLATIONS; IN-CONTROL; LYAPUNOV THEORIES; MATHEMATICAL CHARACTERIZATION; MODEL FOLLOWING CONTROLLER; MODEL-FOLLOWING; NON-LINEAR AERODYNAMICS; NON-LINEARITY; OBSERVER STRUCTURE; PERFORMANCE REQUIREMENTS; SHORT PERIODS; SIMULATION RESULT; STABLE CONTROL; STRUCTURAL DAMAGES; SYSTEM MODELS; UNMODELED DYNAMICS; WEIGHT UPDATE;

EID: 78049317360     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (28)

References (25)
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.