I. Introduction
In many engineering measurements, we need to monitor readings of multiple sensors. A typical example is the health monitoring test of machinery and structures –– airplanes, artificial satellites and civil engineering structures - to detect damage and malfunction before a fatal failure. In a health monitoring of machinery, single or multiple vibration sources are applied to a target and the transient responses at multiple points are synchronously measured in terms of magnitude and phase. Simultaneous data collection from multiple points is essential to detect the phase which shows the indication of resonance. Wiring of sensors is a serious problem particularly in rotating machinery, lightweight or large scale structures. For example, vibration testing of an artificial satellite as shown in Fig. 1 needs a large number of accelerometers whose data is collected with wire harnesses. The preparation of wire harnesses takes time and labor, and there are some positions that wired accelerometers can not be attached.