Nonlinear modeling and control design of active helicopter blades 012002

Journal of the American Helicopter Society

Volumn 57, Issue 1, 2012, Pages

  Althoff, Matthias ^a   Patil, Mayuresh J ^b   Traugott, Johannes P ^c  

^a CARNEGIE MELLON UNIVERSITY   (United States)

^b VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^c TECHNICAL UNIVERSITY OF MUNICH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE BEAMS; AEROELASTIC MODES; BEAM MODEL; CONTROL DESIGN; CROSS SECTIONAL ANALYSIS; GALERKIN APPROACH; HELICOPTER BLADES; HIGH ORDER; INTEGRATED BLADES; LINEAR QUADRATIC GAUSSIAN; NON-LINEAR MODEL; NONLINEAR MODELING; QUASI-STEADY AERODYNAMICS; REDUCED ORDER MODELS; STRUCTURAL MODELS; THEORETICAL BASIS;

AERODYNAMICS; CONTROL; GAUSSIAN BEAMS; MODEL STRUCTURES; NONLINEAR SYSTEMS; STRUCTURAL DYNAMICS; TURBOMACHINE BLADES;

COMPUTER SIMULATION;

EID: 84862567775     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/JAHS.57.012002     Document Type: Conference Paper

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