Using the Complete Authority of Multiple Active Trailing-edge Flaps for Helicopter Vibration Control

DOI10.1177/1077546307081323zbMath1229.74106OpenAlexW1964441329MaRDI QIDQ3110991

Sathyamangalam Ramanarayanan Viswamurthy, Ranjan Ganguly

Publication date: 17 January 2012

Published in: Journal of Vibration and Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1177/1077546307081323

zbMATH Keywords

optimal controlvibrationhelicoptermultiple trailing-edge flaps

Mathematics Subject Classification ID

Control, switches and devices (``smart materials) in solid mechanics (74M05) Vibrations in dynamical problems in solid mechanics (74H45)

Related Items (1)

REDUCED-ORDER-MODEL-BASED PLACEMENT OPTIMIZATION OF MULTIPLE CONTROL SURFACES FOR ACTIVE AEROELASTIC CONTROL

Cites Work

• An optimization approach to vibration reduction in helicopter rotors with multiple active trailing edge flaps
• Smart Spring Impedance Control Algorithm for Helicopter Blade Harmonic Vibration Suppression
• New developments in vibration reduction with actively controlled trailing edge flaps.

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