I. Introduction
Composite materials are gaining more and more attention and applications in the aerospace field due to their excellent comprehensive performance. Due to the inherent mechanical properties of composites, composite structures are susceptible to the formation of barely visible impact damage (BVID) caused by low-velocity impact loads [1], [2], [3]. During the service process, BVID will extend to progressively reduce the load carrying capacity of the structure [4], [5]. Impact monitoring of composite structures is an enduring subject of structural health monitoring (SHM) in engineering applications.