Model based H∞ control for helicopter vibration reduction - Flight tests with active trailing edge flaps

33rd European Rotorcraft Forum 2007, ERF33

Volumn 3, Issue , 2007, Pages 1616-1652

  Dieterich, Oliver ^a   Konstanzer, Peter ^a   Roth, Dieter ^a   Ayadi, Wassef ^b   Reber, Daniel ^b   Well, Klaus H ^b  

^a EUROCOPTER DEUTSCHLAND GMBH   (France)

^b UNIVERSITY OF STUTTGART   (Germany)

Author keywords

Active control; Flight test; H control; Trailing edge flap; Vibration reduction

Indexed keywords

ACTIVE CONTROL; ACTIVE ROTOR; ACTIVE ROTOR CONTROL; ACTIVE TRAILING EDGE FLAP; ADVANCED CONTROL THEORY; AUTOMATIC TRACKING; BLADE VORTEX INTERACTION; CONTROL CONCEPT; CONTROL DESIGN; EUROCOPTERS; FLIGHT CONTROL; FLIGHT MECHANICS; FLIGHT TEST; HELICOPTER VIBRATION; HIGH ORDER MODEL; LOAD REDUCTION; MODEL BASED APPROACH; MODEL REDUCTION; MODEL-BASED; MULTIPLE INPUT MULTIPLE OUTPUT; NOISE REDUCTIONS; PERFORMANCE IMPROVEMENTS; PLANT MODEL; ROTOR STABILITY; ROTOR SYSTEMS; SEMI-EMPIRICAL; SIMULTANEOUS CONTROL; STABILITY ENHANCEMENT; TIME DOMAIN; TRAILING EDGE FLAPS; VIBRATION CONTROLLER; VIBRATION REDUCTIONS;

AIRCRAFT; CONTROL SYSTEM ANALYSIS; CONTROLLERS; DESIGN; EQUIPMENT TESTING; ROTORS (WINDINGS); SYSTEM STABILITY;

HELICOPTER ROTORS;

EID: 77954219862     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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