TS-062490 — An exemplary parametric flutter margin method and associated system that can be used to identify the structural dynamic characteristics
of an Unmanned Aerial Vehicle’s wing in a series
of Ground Vibration Tests (GVTs) and initial flight-testing study.
The Need
In the aerospace industry, ensuring the safety and certification of aircraft is of paramount importance. One critical challenge faced during the certification process is aeroelastic flutter, an unstable phenomenon that can lead to catastrophic consequences. Conventional flight-testing meth…