Abstract
A wavelet-based method is presented to analyze flight flutter test data. The procedure utilizes the filter action of the continuous wavelet transform to enable damping estimation. An indication of the overall stability is obtained from changes in the shape of the wavelet transform amplitude cross sections. The method is illustrated using simple simulated examples and real flight-test data. A good agreement was achieved compared to classical parameter estimation techniques.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
