Helicopter Vibration Reduction and Damping Enhancement Using Individual Blade Control

Thomas Mannchen; Klaus H. Well

doi:10.2514/1.12598

Helicopter Vibration Reduction and Damping Enhancement Using Individual Blade Control

Journal of Guidance Control and Dynamics ◽

10.2514/1.12598 ◽

2004 ◽

Vol 27 (5) ◽

pp. 760-767 ◽

Cited By ~ 3

Author(s):

Thomas Mannchen ◽

Klaus H. Well

Keyword(s):

Vibration Reduction ◽

Individual Blade Control ◽

Blade Control ◽

Helicopter Vibration

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Rotor Hub Vibration Reduction Analysis Applying Individual Blade Control

Journal of the Korean Society for Aeronautical & Space Sciences ◽

10.5139/jksas.2021.49.8.649 ◽

2021 ◽

Vol 49 (8) ◽

pp. 649-660

Author(s):

Taejoo Kim ◽

Seong-Yong Wie ◽

Minwoo Kim ◽

Dong-geon Lee

Keyword(s):

Vibration Reduction ◽

Individual Blade Control ◽

Blade Control

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Helicopter vibration reduction using periodic robust control

10.2514/6.2001-4034 ◽

2001 ◽

Author(s):

Thomas Mannchen ◽

Klaus Well

Keyword(s):

Robust Control ◽

Vibration Reduction ◽

Helicopter Vibration

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Testing of a Stall Flutter Suppression System for Helicopter Rotors Using Individual‐Blade‐Control

Journal of the American Helicopter Society ◽

10.4050/jahs.29.3.38 ◽

1984 ◽

Vol 29 (3) ◽

pp. 38-44 ◽

Cited By ~ 2

Author(s):

Todd R. Quackenbush

Keyword(s):

Helicopter Rotors ◽

Flutter Suppression ◽

Individual Blade Control ◽

Stall Flutter ◽

Blade Control ◽

Suppression System

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Design Aspects of Helicopter Vibration Reduction

Journal of the American Helicopter Society ◽

10.4050/jahs.2.3.10 ◽

1957 ◽

Vol 2 (3) ◽

pp. 10-11

Author(s):

Glidden S. Doman

Keyword(s):

Vibration Reduction ◽

Helicopter Vibration

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Down-regulation and individual blade control as lifetime extension enablers

Journal of Physics Conference Series ◽

10.1088/1742-6596/1102/1/012026 ◽

2018 ◽

Vol 1102 ◽

pp. 012026 ◽

Cited By ~ 2

Author(s):

Vasilis Pettas ◽

Po Wen Cheng

Keyword(s):

Down Regulation ◽

Individual Blade Control ◽

Blade Control ◽

Lifetime Extension

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Robust design of multiple trailing edge flaps for helicopter vibration reduction: A multi-objective bat algorithm approach

Engineering Optimization ◽

10.1080/0305215x.2014.958734 ◽

2014 ◽

Vol 47 (9) ◽

pp. 1243-1263 ◽

Cited By ~ 18

Author(s):

Rajnish Mallick ◽

Ranjan Ganguli ◽

M. Seetharama Bhat

Keyword(s):

Robust Design ◽

Vibration Reduction ◽

Bat Algorithm ◽

Trailing Edge ◽

Multi Objective ◽

Trailing Edge Flaps ◽

Helicopter Vibration

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Individual blade control of hinged blades using smart structures

Smart Materials and Structures ◽

10.1088/0964-1726/3/2/013 ◽

1994 ◽

Vol 3 (2) ◽

pp. 171-180 ◽

Cited By ~ 1

Author(s):

F Nitzsche ◽

E Breitbach

Keyword(s):

Smart Structures ◽

Individual Blade Control ◽

Blade Control

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Terfenol-D driven flaps for helicopter vibration reduction

Smart Materials and Structures ◽

10.1088/0964-1726/5/1/006 ◽

1996 ◽

Vol 5 (1) ◽

pp. 49-57 ◽

Cited By ~ 27

Author(s):

Ralph C Fenn ◽

James R Downer ◽

Dariusz A Bushko ◽

Vijay Gondhalekar ◽

Norman D Ham

Keyword(s):

Vibration Reduction ◽

Helicopter Vibration

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Robust Individual Blade Control Algorithm for a Dissimilar Rotor

Journal of Guidance Control and Dynamics ◽

10.2514/2.4964 ◽

2002 ◽

Vol 25 (5) ◽

pp. 915-923 ◽

Cited By ~ 8

Author(s):

Beatrice Roget ◽

Inderjit Chopra

Keyword(s):

Control Algorithm ◽

Individual Blade Control ◽

Blade Control

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Helicopter Vibration Reduction Using Discrete Controllable-Stiffness Devices at the Rotor Hub

Journal of Aircraft ◽

10.2514/2.2980 ◽

2002 ◽

Vol 39 (4) ◽

pp. 668-677 ◽

Cited By ~ 1

Author(s):

Farhan Gandhi ◽

Phuriwat Anusonti-Inthra

Keyword(s):

Vibration Reduction ◽

Helicopter Vibration

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