Experimental and operational modal analysis: Automated system identification for safety-critical applications. (15th January 2023)

• Record Type: Journal Article
• Authors: Volkmar, Robin; Soal, Keith; Govers, Yves; Böswald, Marc
• Is Part Of: Mechanical systems and signal processing. Volume 183(2023)
• Publication Date: 2023-01-15
• Subjects: Automated modal analysis -- Parametric system identification -- Bayesian optimization -- Supervised learning -- Experimental modal analysis -- Operational modal analysis; Structural dynamics -- Periodicals; Vibration -- Periodicals; Constructions -- Dynamique -- Périodiques; Vibration -- Périodiques; Structural dynamics; Vibration; Periodicals; 621
• DOI: 10.1016/j.ymssp.2022.109658
• Languages: English
• ISSNs: 0888-3270

Abstract

Highlights: Autonomous method learns how to perform modal analysis optimally. Modal damping of test object automatically identified with high accuracy. Automatic modal parameter identification method universally usable. Autonomous implementation facilitates modal analysis quasi in real-time. Abstract: Safety-critical applications like the evaluation of aeroelastic stability during aircraft flight require modal parameters identified with high accuracy. Promising methods of automated modal identification exist. Nevertheless, these methods are not yet chosen for safety–critical applications. The reason is either insufficient accuracy of modal parameters or significant adaptions for each individual application. In this work, a new method is presented that not only enables fully automated modal analysis, but also learns an optimal way to analyze the data in a supervised manner. Based on the result of a single manual modal analysis, the self-learning method finds optimal parameters for the automated analysis. In an iterative process, new analysis parameters are chosen by Bayesian Optimization with a Gaussian Process as surrogate model and Expected Improvement as the acquisition function. With these parameters, the method can analyze additional datasets as accurately as a manual expert. The presented method is evaluated on ground vibration test data (i.e., experimental modal analysis) as well as flight vibration data (i.e., operational modal analysis) of an aircraft structure. In contrast to previous methods, the presented method can be easily used for various modal tests, since it can learn by itself to perform optimally with respect to a specific target function like for example the one provided in this work. Due to its robustness, the method is promising also for industrial test cases and safety–critical applications.