467.600 PEOPLE
| People | Locations | Statistics |
|---|---|---|
| Serhiienko, Serhii |
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| Schmalz, Ulrike |
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| Oliveira, Marisa |
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| Ribeiro Pereira, Maria Teresa |
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| Bellér, Gábor |
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| Araujo, M. |
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| Frey, Michael | Karlsruhe |
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| Coutinho-Rodrigues, João | Coimbra |
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| Wouters, Christian Guillaume Louise | Aachen |
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| Kessel, Paul J. Van Van |
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| Árpád, István |
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| Fontul, Simona |
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| Kocsis, Dénes |
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| Cigada, Alfredo | Milan |
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| Oort, Neils Van | Delft |
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| Agárdi, Anita | Miskolc |
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| Andrews, Gordon E. |
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| Sousa, Nuno |
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| Witlox, Frank Jacomina Albert | Ghent |
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| Dobruszkes, Frederic |
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| Kiss, Judit T. |
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| Hadachi, Amnir | Saint-Étienne-du-Rouvray |
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| Hamilton, Carl J. | Kunovice |
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| Misiura, Serhii |
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| Schimpf, Marina |
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Coppotelli, Giuliano
in Cooperation with on an Cooperation-Score of 37%
Topics
- data
- helicopter
- Statistic
- forecasting
- simulation
- estimating
- procurement
- indicating instrument
- monitoring
- vehicle fleet
- diagnosis
- machinery
- validation
- statistical analysis
- uncertainty
- algorithm
- flight
- health
- modal analysis
- flight test
- automation
- airplane
- rotary wing aircraft
- modernization
- certification
- real time control
- rotor blade
- vibration
- surveillance
- deviation
- inspection
- driveline
- alarm system
- pitting
- train component
- noise
- estimate
- attention
- propeller blade
- time window
- particle beam
- cantilever
- drone
- chemical element
- weight
- behavior
- employed
- laboratory
- rotor
- stiffness
- sensitivity
- frequency response
- vibration control
- vibration test
- beltway
- experiment
- tower
- taxiing
- harmonic
- excitation
- scale model
- aircraft
- data collection
- industry
- driver
- linearity
- contrast
- design
- control system
- lowering
- control panel
- sensor
- friction
- prototype
- actuating system
- actuator
- test facility
- assessment
- recommendation
- variable
- minimisation
- structural model
- dynamic test
- asymmetry
- gust
- show 55 more
Publications
- 2019Impact of pulse time uncertainty on synchronous average: Statistical analysis and relevance to rotating machinery diagnosiscitations
- 2019Real-time system identification for fixed and rotary wing aircraftcitations
- 2018Fault detection in operating helicopter drive train components based on support vector data descriptioncitations
- 2016Modal parameters directly estimated from power spectral densities or correlation functions in output-only analysiscitations
- 2015Updating of an Unmanned Aerial Vehicle Finite Element Model using Experimental Data
- 2015Correlation and Updating of an Unmanned Aerial Vehicle Finite Element Modelcitations
- 2015Identification of the smart spring properties from FRFs measurementscitations
- 2013Ground vibration tests of a helicopter structure using OMA techniquescitations
- 2013Whirl-tower open-loop experiments and simulations with an adaptive pitch link device for helicopter rotor vibrationcitations
- 2013System Identification from GVT and Taxiing of an Unmanned Aerial Vehicle
- 2013Dealing with harmonics and noise for advanced dynamic identification using in-flight helicopter data
- 2012Helicopter in-flight modal analysis: Solutions for dealing with harmonics and noise
- 2012Dynamic identification of helicopter structures using operational modal analysis methods in the presence of harmonic loading
- 2012System identification of a reduced scale model blade with an adaptive pitch link using whirl tower test data
- 2011Advanced shaker excitation signals for aerospace testingcitations
- 2011Operational modal analysis of a helicopter UAV from flight tests
- 2009Experimental identification of the structural properties of an AB 204 helicopter blade and finite element model validationcitations
- 2009Whirl tower demonstrations of the SHARCS hybrid control concept
- 2009Identification of the Dynamic Properties of Active Twist Rotor Model Blade Using Output-Only Data
- 2009Use of Correlation Techniques in Output-Only Analysis
- 2005The SHARCS project: Smart hybrid active rotor control system for noise and vibration attenuation of helicopter rotor blades
- 2005Output-Only Approach for Finite Element Model Updating of AB 204 Helicopter Bladecitations
- 2005Output-Only Approach for Finite Element Model Updating of AB-204 Helicopter Blade
- 2004Identification and Updating of AB204 Helicopter Blade F.E. Model by Means of Static and Dynamic Tests
- 2004Identification and updating of AB 204 helicopter blade F.E. model by means of static and dynamic tests
- 2003Analysis of Helicopter Cabin Vibrations due to Rotor Asymmetry and Gust Encountercitations
Places of action
