Terminal sliding mode control for aeroelastic systems

Nonlinear Dynamics

Volumn 70, Issue 3, 2012, Pages 2015-2026

  Chen, Chieh Li ^a   Chang, Chung Wei ^a   Yau, Her Terng ^b  

^a NATIONAL CHENG KUNG UNIVERSITY   (Taiwan)

^b NATIONAL CHIN YI UNIVERSITY OF TECHNOLOGY   (Taiwan)

Author keywords

Aeroelastic system; Limit cycle oscillation; Terminal sliding mode control

Indexed keywords

AEROELASTIC SYSTEM; CHATTERING PHENOMENON; CONTROL INPUTS; CONTROL LAW DESIGN; CONTROL LAWS; CONTROL SIGNAL; CONTROLLER DESIGNS; DYNAMIC SYSTEM MODELS; EXTERNAL DISTURBANCES; FLIGHT SPEED; INTERNAL DYNAMICS; LIMIT CYCLE OSCILLATION (LCO); MODERN CONTROL; MULTIPLE-INPUT CHANNELS; NONLINEAR EFFECT; PITCH ANGLE; RESEARCH ISSUES; RESPONSE DESIGNS; ROBUST CONTROL DESIGNS; SATURATION FUNCTION; STRUCTURE PARAMETER; TERMINAL SLIDING MODE CONTROL; TIME FRAME; TRAILING EDGES; UNCERTAINTY EFFECTS; UNKNOWN UNCERTAINTY;

CONTROLLERS; DESIGN; DYNAMICS; FLIGHT CONTROL SYSTEMS; NONLINEAR CONTROL SYSTEMS; ROBUST CONTROL; SLIDING MODE CONTROL;

AEROELASTICITY;

EID: 84870888680     PISSN: 0924090X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11071-012-0593-x     Document Type: Article

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