Model reference adaptive control for a flexible launch vehicle

Proceedings of the Institution of Mechanical Engineers. Part I: Journal of Systems and Control Engineering

Volumn 222, Issue 1, 2008, Pages 49-55

  Khoshnood, A ^a   Roshanian, J ^a   Khaki Sedig, A ^a  

^a K N TOOSI UNIVERSITY OF TECHNOLOGY   (Iran)

Author keywords

Bending vibration; Flexible launch vehicle (FLV); MIT rule; Model reference adaptive system; Notch filter

Indexed keywords

ADAPTIVE FILTERS; CATAPULTS (AIRCRAFT LAUNCHERS); CONTROL SYSTEM STABILITY; ELECTRIC FILTERS; LAUNCHING; MISSILE LAUNCHING SYSTEMS; SULFATE MINERALS; SYSTEM STABILITY; TELECOMMUNICATION NETWORKS; VEHICLES;

ADAPTIVE CONTROL; ADAPTIVE CONTROLLERS; BENDING VIBRATION; CENTRAL PROCESSING UNITS; FILTER METHODS; FLEXIBLE LAUNCH VEHICLE (FLV); GAIN SCHEDULING; LAUNCH VEHICLE STRUCTURE; LAUNCH VEHICLES; MASSACHUSETTS INSTITUTE OF TECHNOLOGY; MIT RULE; MODEL REFERENCE ADAPTIVE; MODEL REFERENCE ADAPTIVE CONTROL; MODEL REFERENCE ADAPTIVE SYSTEM; NOTCH FILTER; REAL-TIME APPLICATIONS; SINGLE PARAMETER;

ADAPTIVE CONTROL SYSTEMS;

EID: 46049104197     PISSN: 09596518     EISSN: None     Source Type: Journal    
DOI: 10.1243/09596518JSCE469     Document Type: Article

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