Unmanned aerial vehicle attitude control testing arrangement

The utility model provides an unmanned aerial vehicle attitude control testing arrangement, joint, slide bar, the above joint of two -degree -of -freedom, installing module, unmanned aerial vehicle module and simulation software module more than base, three degrees of freedom, wherein: the base is fixed in ground or table surface, through being connected in joint more than three degrees of freedom between slide bar and the base, is connected through two -degree -of -freedom above joint between installing module and the slide bar, and the unmanned aerial vehicle module is installed on installing module to make the unmanned aerial vehicle module possess around the rotational degree of freedom of X, Y, the three direction of Z axle and the movement freedom who follows X, Y, the three direction of Z axle, amount to six degrees of freedom. Dynamic response when moving on this device unmanned aerial vehicle adjusts control strategy and relevant parameter in real time, makes things convenient for scientific research