本发明提供了一种新的飞行器曳航试验方法。首先根据第1图A、B说明过去的飞行器曳航方法。a为被试飞行器,b为固定在外壳上的吊具(固定环)、c为嵌入吊具b内的滑环,d为连结在滑环c上的吊索。另外,按图1C、D说明其它用例。e为安装在飞行器a的重心位置横切面上的支承棒,f为安装在支承棒e The present invention provides a new aircraft towing test method. First of all, based on Figure 1, Figure 1, B shows the past method of aircraft towing. a is the tested aircraft, b is a spreader (fixed ring) fixed on the housing, c is a slip ring embedded in the spreader b, and d is a sling attached to the slip ring c. In addition, the other use cases are demonstrated by FIG. 1C, D. FIG. e is a support rod mounted on the cross section of the center of gravity a of the aircraft a, f is a support rod mounted on the support rod e