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Ground test for vibration control demonstrator
C. Meyer, J. Prodigue, G. Broux, O. Cantinaud, Charles Poussot-Vassal

Ground test for vibration control demonstrator

Science & Mathematics Published 2016 Verification Pending

Overview & Synopsis

In the objective of maximizing comfort in Falcon jets, Dassault Aviation is developing an innovative vibration control technology. Vibrations of the structure are measured at several locations and sent to a dedicated high performance vibration control computer. Control laws are implemented in this computer to analyse the vibrations in real time, and then elaborate orders sent to the existing control surfaces to counteract vibrations. After detailing the technology principles, this paper focuses on the vibration control ground demonstration that was performed by Dassault Aviation in May 2015 on Falcon 7X business jet. The goal of this test was to attenuate vibrations resulting from fixed forced excitation delivered by shakers. The ground test demonstrated the capability to implement an efficient closed-loop vibration control with a significant vibration level reduction and validated the vibration control law design methodology. This successful ground test was of primary importance before the flight test demonstration that is now being prepared. This study has been partly supported by the JTI CleanSky SFWA-ITD.

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Document Information

Document Title Ground test for vibration control demonstrator
Author / Organization C. Meyer, J. Prodigue, G. Broux, O. Cantinaud, Charles Poussot-Vassal
Subject & Discipline Multidisciplinary Academic Open Research
Categories Science & Mathematics
Publication Year 2016
License / Rights Open Access / Creative Commons
Resource Verification Listed PDF (Verification Pending)
Original Host Website HAL Open Science (hal.science)
File Format application/pdf (Portable Document Format)
Language EN
Catalog ID DOC-156777
Original Source Link Visit Source Page on hal.science »