Improving Health Operation of Flapping-Wing Robotic Aircraft Systems Using Event-Triggered Vibration Control Technology

In this paper, the application of event-triggered vibration control technology for enhancing the health operation of Flapping-Wing Robotic Aircraft Systems (FWRAs) is studied. Based on the dynamic model constructed by partial differential equations, event-triggered controllers are designed. The controllers can not only accurately suppress the bending and torsional deformations vibrations generated during flight, prolong the life of the systems and improve the overall health operation level, but also reduce unnecessary communication frequency, significantly reduce energy consumption and optimize communication flexibility, which provides strong technical support for the health operation of FWRAs. In addition, the boundedness of the signals is ensured through meticulous parameter selection and comprehensive stability analysis. Moreover, the proposed method effectively avoids the Zeno phenomenon. Simulation results verify the effectiveness of the proposed control scheme in improving the systems stability, prolonging the health service cycle and optimizing energy efficiency.