Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 2001, Pages 1877-1887

  Roget, B ^a   Chopra, I ^a   Gessow, A ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CONTROL SYSTEMS; ROTORS; VIBRATIONS (MECHANICAL);

HIGHER HARMONIC CONTROL; INDIVIDUAL BLADE CONTROL; ROTOR BLADES; TRAILING EDGE FLAP CONTROL; VIBRATION REDUCTION;

HELICOPTERS;

EID: 0035017287     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)