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Vibration reduction in rotorcraft using active control - A comparison of various approaches

https://doi.org/10.2514/3.21445
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What this work says

Outgoing claims: the papers this work cites, builds on, or argues with.

inferredcites →https://doi.org/10.1016/0895-7177(93)90109-copenalex-snapshot
Coupled rotor-fuselage vibration reduction using open-loop blade pitch control
inferredcites →https://doi.org/10.1088/0964-1726/5/1/006openalex-snapshot
Terfenol-D driven flaps for helicopter vibration reduction
inferredcites →https://doi.org/10.1117/12.152777openalex-snapshot
Terfenol-D-driven flaps for helicopter vibration reduction
inferredcites →https://doi.org/10.2514/3.10477openalex-snapshot
Influence of unsteady aerodynamics on rotor blade aeroelastic stability and response
inferredcites →https://doi.org/10.2514/3.19722openalex-snapshot
Frequency-shaped cost functionals - Extension of linear-quadratic-Gaussian design methods
inferredcites →https://doi.org/10.2514/3.21085openalex-snapshot
Performance of higher harmonic control algorithms for helicopter vibration reduction
inferredcites →https://doi.org/10.2514/3.45987openalex-snapshot
Helicopter vibration reduction using structural optimization with aeroelastic/multidisciplinary constraints - A survey
inferredcites →https://doi.org/10.2514/3.56151openalex-snapshot
A New Approach for Active Control of Rotorcraft Vibration
inferredcites →https://doi.org/10.2514/6.1990-1115openalex-snapshot
Rotary-wing aeroelasticity with application to VTOL vehicles
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Rotary-wing aeroservoelastic problems
inferredcites →https://doi.org/10.2514/6.1992-2451openalex-snapshot
Vibration reduction in helicopter rotors using an active control surface located on the blade
inferredcites →https://doi.org/10.2514/6.1993-1361openalex-snapshot
FULL-SCALE WIND TUNNEL INVESTIGATION OF A HELICOPTER INDIVIDUAL BLADE CONTROL SYSTEM
inferredcites →https://doi.org/10.4050/jahs.28.1.63openalex-snapshot
A Numerical Simulation Study of Open‐Loop, Closed‐Loop and Adaptive Multicyclic Control Systems
inferredcites →https://doi.org/10.4050/jahs.28.10openalex-snapshot
Wind Tunnel Results Showing Rotor Vibratory Loads Reduction Using Higher Harmonic Blade Pitch
inferredcites →https://doi.org/10.4050/jahs.28.9openalex-snapshot
A Unified Approach to the Optimal Design of Adaptive and Gain Scheduled Controllers to Achieve Minimum Helicopter Rotor Vibration
inferredcites →https://doi.org/10.4050/jahs.29.3.38openalex-snapshot
Testing of a Stall Flutter Suppression System for Helicopter Rotors Using Individual‐Blade‐Control
inferredcites →https://doi.org/10.4050/jahs.29.30openalex-snapshot
Design and Evaluation of a State‐Feedback Vibration Controller
inferredcites →https://doi.org/10.4050/jahs.29.4openalex-snapshot
Helicopter Vibrations: A Technological Perspective
inferredcites →https://doi.org/10.4050/jahs.30.1.3openalex-snapshot
On Developing and Flight Testing a Higher Harmonic Control System
inferredcites →https://doi.org/10.4050/jahs.34.14openalex-snapshot
Higher Harmonic Control: Wind Tunnel Demonstration of Fully Effective Vibratory Hub Force Suppression
inferredcites →https://doi.org/10.4050/jahs.36.32openalex-snapshot
A Study of Fundamental Issues in Higher Harmonic Control Using Aeroelastic Simulation
inferredcites →https://doi.org/10.4050/jahs.37.3.61openalex-snapshot
New Aspects of Higher Harmonic Control on a Four-Bladed Hingeless Model Rotor
inferredcites →https://doi.org/10.4050/vfs-f39-057openalex-snapshot
THE IMPORTANCE OF NONLINEARITY ON THE HIGHER HARMONIC CONTROL OF HELICOPTER VIBRATION
inferredcites →https://doi.org/10.4050/vfs-f40-1193openalex-snapshot
Development and Evaluation of a Generic Active Helicopter Vibration Controller
inferredcites →https://doi.org/10.4050/vfs-f41-1200openalex-snapshot
Helicopter Gust Alleviation, Attitude Stabilization, and Vibration Alleviation Using Individual-Blade-Control Through a Conventional Swash Plate
inferredcites →https://doi.org/10.4050/vfs-f46-1001openalex-snapshot
AN EVALUATION OF ACTIVE CONTROL OF STRUCTURAL RESPONSE AS A MEANS OF REDUCING HELICOPTER VIBRATION

What points at this work

Incoming claims: where this work appears in other papers’ reference lists and arguments.

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Identification of Linear Time-Periodic Systems from Rotorcraft Flight-Test Data
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Order Reduction and Closed-Loop Vibration Control in Helicopter Fuselages
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Generalized Active Control of Vibrations in Helicopters
inferred← citeshttps://doi.org/10.2514/2.4964openalex-snapshot
Robust Individual Blade Control Algorithm for a Dissimilar Rotor
inferred← citeshttps://doi.org/10.2514/2.838openalex-snapshot
Coupled Helicopter Rotor/Flexible Fuselage Aeroelastic Model for Control of Structural Response
inferred← citeshttps://doi.org/10.2514/6.1996-1547openalex-snapshot
ACSR system for vibration suppression in coupled helicopter rotor/flexible fuselage model
inferred← citeshttps://doi.org/10.2514/6.1996-4177openalex-snapshot
Integrated design of an adaptive neurocontroller for a 2-D aeroelastic system
inferred← citeshttps://doi.org/10.2514/6.1997-1083openalex-snapshot
Unsteady compressible aerodynamics of a flapped airfoil with application to helicopter vibration reduction
inferred← citeshttps://doi.org/10.2514/6.1997-1283openalex-snapshot
Advanced servo flap rotor using variable blade index angle control
inferred← citeshttps://doi.org/10.2514/6.1998-2098openalex-snapshot
Rotary-wing aeroelastic scaling and its application to adaptive materials based actuation
inferred← citeshttps://doi.org/10.2514/6.1999-1220openalex-snapshot
BVI alleviation using active control
inferred← citeshttps://doi.org/10.2514/6.2000-1500openalex-snapshot
Durability characterization of piezoelectric stack actuators under combined electro-mechanical loading
inferred← citeshttps://doi.org/10.2514/6.2000-1687openalex-snapshot
Vibration reduction in rotorcraft using an enhanced ACSR model
inferred← citeshttps://doi.org/10.2514/6.2000-1710openalex-snapshot
Design and manufacturing of a second-generation integral twist-actuated rotor blade
inferred← citeshttps://doi.org/10.2514/6.2000-2475openalex-snapshot
Rotorcraft retreating blade stall control
inferred← citeshttps://doi.org/10.2514/6.2000-4299openalex-snapshot
Advanced helicopter flight and aeroelastic simulation based on general purpose multibody code
inferred← citeshttps://doi.org/10.2514/6.2001-1433openalex-snapshot
Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades
inferred← citeshttps://doi.org/10.2514/6.2001-1467openalex-snapshot
Actuator saturation and its influence on vibration reduction by actively controlled flaps
inferred← citeshttps://doi.org/10.2514/6.2001-4034openalex-snapshot
Helicopter vibration reduction using periodic robust control
inferred← citeshttps://doi.org/10.2514/6.2001-427openalex-snapshot
Rotary-wing aeroelasticity-current status and future trends
inferred← citeshttps://doi.org/10.2514/6.2002-1431openalex-snapshot
Reduction of Vibrations due to Dynamic Stall in Helicopters using an Actively Controlled Flap
inferred← citeshttps://doi.org/10.2514/6.2002-1446openalex-snapshot
Induced-Shear Piezoelectric Actuators for Active Twist Rotor Blades
inferred← citeshttps://doi.org/10.2514/6.2002-1720openalex-snapshot
Roll Maneuver Control of UCAV Wing Using Anisotropic Piezoelectric Actuators
inferred← citeshttps://doi.org/10.2514/6.2003-1543openalex-snapshot
Active Load Control of an Articulated Composite Rotor Blade via Dual Trailing Edge Flaps
inferred← citeshttps://doi.org/10.2514/6.2003-1785openalex-snapshot
Rotorcraft Vibration and Noise Prediction Using a Unified Aeroelastic Analysis
inferred← citeshttps://doi.org/10.2514/6.2004-1633openalex-snapshot
Pseudo-Active Control of Helicopter Blade Vibration Using Piezoelectric Actuators
inferred← citeshttps://doi.org/10.2514/6.2004-1948openalex-snapshot
The HHC Algorithm for Helicopter Vibration Reduction Revisited
inferred← citeshttps://doi.org/10.2514/6.2004-1951openalex-snapshot
Swashplateless Helicopter Rotor System with Active Trailing-Edge Flaps for Primary and Vibration Controls
inferred← citeshttps://doi.org/10.2514/6.2005-2038openalex-snapshot
Improved Dynamic Response of Piezoelectric Composite Shells using Multiobjective Optimization and Closed Loop Control
inferred← citeshttps://doi.org/10.2514/6.2005-2245openalex-snapshot
Simultaneous Vibration and Noise Reduction in Rotorcraft - Practical Implementation Issues
inferred← citeshttps://doi.org/10.2514/6.2005-2246openalex-snapshot
Refined Analysis of the Piezoelectric Pseudo-Active Control for Helicopter Blades Vibration
inferred← citeshttps://doi.org/10.2514/6.2005-2247openalex-snapshot
Effect of Piezoelectric Hysterisis Nonlinearity on Helicopter Vibration Control Using Trailing Edge Flaps
inferred← citeshttps://doi.org/10.2514/6.2005-2904openalex-snapshot
Helicopter Noise Reduction By Actively Controlled Flaps
inferred← citeshttps://doi.org/10.2514/6.2006-1821openalex-snapshot
Surrogate Based Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward Flight
inferred← citeshttps://doi.org/10.2514/6.2006-1861openalex-snapshot
Vibration Reduction and Performance Enhancement in Rotorcraft Using Active Flaps at High Advance Ratios
inferred← citeshttps://doi.org/10.2514/6.2006-6997openalex-snapshot
Efficient Global Optimization of Helicopter Rotor Blades for Vibration Reduction in Forward Flight
inferred← citeshttps://doi.org/10.2514/6.2007-1898openalex-snapshot
Application of a Weighted Average Surrogate Approach to Helicopter Rotor Blade Vibration Reduction
inferred← citeshttps://doi.org/10.2514/6.2008-2178openalex-snapshot
Vibration Reduction and Performance Enhancement of Helicopter Rotors Using an Active/Passive Approach
inferred← citeshttps://doi.org/10.2514/6.2009-2601openalex-snapshot
The AVINOR Aeroelastic Simulation Code and Its Application to Reduced Vibration Composite Rotor Blade Design
inferred← citeshttps://doi.org/10.2514/6.2009-2604openalex-snapshot
A Computational Study of Microflaps with Application to Vibration Reduction in Helicopter Rotors
inferred← citeshttps://doi.org/10.2514/6.2010-2994openalex-snapshot
Hysteresis Characterization in Piezoceramic Stack Actuators and Its Influence on Vibration and Noise Reduction in Helicopters Using Actively Controlled Flaps
inferred← citeshttps://doi.org/10.2514/6.2011-1873openalex-snapshot
Numerical Evaluation of Microflaps for On Blade Control of Noise and Vibration
inferred← citeshttps://doi.org/10.2514/6.2012-1477openalex-snapshot
Actuator Saturation in Individual Blade Control of Rotorcraft
inferred← citeshttps://doi.org/10.2514/6.2015-1854openalex-snapshot
Active Control on Helicopter Blades with a L-Shaped Gurney Flap
inferred← citeshttps://doi.org/10.2514/6.2016-4244openalex-snapshot
Numerical Investigation of Helicopter Blade Section Undergoing Time-Periodic Motions
inferred← citeshttps://doi.org/10.2514/6.2020-1301openalex-snapshot
Preliminary Design of a TE Morphing Surface for Rotorcraft
inferred← citeshttps://doi.org/10.3182/20140824-6-za-1003.00191openalex-snapshot
Improving the positioning bandwidth of the Integral Resonant Control Scheme through strategic zero placement.
inferred← citeshttps://doi.org/10.3182/20140824-6-za-1003.02740openalex-snapshot
Baseline vibration attenuation in helicopters: robust MIMO-HHC control
inferred← citeshttps://doi.org/10.33795/eltek.v21i1.380openalex-snapshot
Desain kontrol adaptif L1 dengan band pass filter orde dua untuk pengendali vibrasi pada rotor helikopter
inferred← citeshttps://doi.org/10.3389/fmech.2016.00002openalex-snapshot
Butterworth Pattern-based Simultaneous Damping and Tracking Controller Designs for Nanopositioning Systems
inferred← citeshttps://doi.org/10.3390/aerospace11110875openalex-snapshot
Identification of High-Order Linear Time-Invariant Models from Periodic Nonlinear System Responses
inferred← citeshttps://doi.org/10.3390/app11031041openalex-snapshot
Optimal Segment Control of Active Twist Rotor for Power Reduction in Forward Flight
inferred← citeshttps://doi.org/10.3390/app16031319openalex-snapshot
Modelling, Parametric Study, and Optimisation of 3D Model-Scale Helicopter’s Rotor Blade with Piezoelectric Actuators
inferred← citeshttps://doi.org/10.3390/engproc2026133191openalex-snapshot
Modelling of a Rotor Blade with Piezoelectric MFC Actuators
inferred← citeshttps://doi.org/10.3390/jmmp9070209openalex-snapshot
Static Analysis of a Composite Box Plate with Functionally Graded Foam Core
inferred← citeshttps://doi.org/10.3390/pr11102941openalex-snapshot
A Topological Valley Stamping Plate for Low-Frequency-Vibration Isolation and Wave Manipulation in Helicopters
inferred← citeshttps://doi.org/10.4018/978-1-5225-4766-2.ch019openalex-snapshot
Robust Design of Helicopter Rotor Flaps Using Bat Algorithm
inferred← citeshttps://doi.org/10.4028/www.scientific.net/amr.1044-1045.877openalex-snapshot
Study on Vibratory Loads of Rotor with Trailing Edge Excitation
inferred← citeshttps://doi.org/10.4050/1.3092846openalex-snapshot
Rotorcraft Vibration Reduction and Noise Prediction Using a Unified Aeroelastic Response Simulation
inferred← citeshttps://doi.org/10.4050/f-0070-2014-9498openalex-snapshot
Gain-Scheduled Higher Harmonic Control for Full Flight Envelope Vibration Reduction
inferred← citeshttps://doi.org/10.4050/jahs.46.192openalex-snapshot
Aeroelastic Analysis of Rotors with Trailing Edge Flaps Using Comprehensive Codes
inferred← citeshttps://doi.org/10.4050/jahs.46.32openalex-snapshot
Application of a New Compressible Time Domain Aerodynamic Model to Vibration Reduction in Helicopters Using an Actively Controlled Flap
inferred← citeshttps://doi.org/10.4050/jahs.48.176openalex-snapshot
Individual Blade Control Methodology for a Rotor with Dissimilar Blades
inferred← citeshttps://doi.org/10.4050/jahs.48.18openalex-snapshot
Effects of Two/rev Higher Harmonic Control on Rotor Performance
inferred← citeshttps://doi.org/10.4050/jahs.48.244openalex-snapshot
Helicopter Vibration Induced by Highly Structured Turbulence
inferred← citeshttps://doi.org/10.4050/jahs.49.318openalex-snapshot
On the Role of Zeros in Rotorcraft Aeromechanics
inferred← citeshttps://doi.org/10.4050/jahs.49.54openalex-snapshot
Active-Passive Hybrid Optimization of Rotor Blades with Trailing Edge Flaps
inferred← citeshttps://doi.org/10.4050/jahs.51.127openalex-snapshot
Simultaneous Vibration and Noise Reduction in Rotorcraft Using Aeroelastic Simulation
inferred← citeshttps://doi.org/10.4050/jahs.53.338openalex-snapshot
Rotor Performance Enhancement and Vibration Reduction in Presence of Dynamic Stall Using Actively Controlled Flaps
inferred← citeshttps://doi.org/10.4050/jahs.54.012007openalex-snapshot
Helicopter Vibration Reduction throughout the Entire Flight Envelope Using Surrogate-Based Optimization
inferred← citeshttps://doi.org/10.4050/jahs.55.012009openalex-snapshot
Closed-Loop Test of a Rotor with Individually Controlled Trailing-Edge Flaps for Vibration Reduction
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