Attitude control test device for unmanned aerial vehicle

The invention provides an attitude control test device for an unmanned aerial vehicle. The attitude control test device comprises a base, a joint with more than three degrees of freedom, a sliding rod, a joint with more than two degrees of freedom, a mounting module, an unmanned aerial vehicle module and a simulation software module, wherein the base is fixed on the ground or a work surface; the sliding rod is connected with the base through the joint with more than three degrees of freedom; the mounting module is connected with the sliding rod through the joint with more than two degrees of freedom; the unmanned aerial vehicle module is mounted on the mounting module, so that the unmanned aerial vehicle module has degrees of freedom for rotating around the X axis, the Y axis and the Z axis, and degrees of freedom for moving along the X axis, the Y axis and the Z axis, namely six degrees of freedom in space in total. Through the dynamic response of the running unmanned aerial vehicle on the attitude control test device, control strategies and relevant parameters are adjusted in real time, so that scientific research personnel and engineers can conveniently develop and debug flight control products of unmanned aerial vehicles; besides, debugging can be safely performed indoors, so that the level of difficulties in research and development of products of unmanned aerial vehicles is lowered, and the industry of the unmanned aerial vehicles is promoted to quickly develop.