The utility model discloses a rotor unmanned aerial vehicle controls capability test device, including annular base and rotor thrust gage beam, the one end and the annular base of rotor thrust gage beam are connected, and the other end can be connected with rotor unmanned aerial vehicle's rotor shaft, and the middle part of rotor thrust gage beam is equipped with the force sensor who is used for measuring rotor thrust gage beam pulling force size. The utility model provides a rotor unmanned aerial vehicle controls capability test device, utilize annular base for the major structure, through setting up the rotor thrust gage beam, and force sensor has been disposed on the rotor thrust gage beam, the device has guaranteed the security of unmanned aerial vehicle capability test in -process, the damage of device such as rotor among the unmanned aerial vehicle test procedure has been avoided, the unmanned aerial vehicle control capability test cost is greatly reduced, and simultaneously, thedevice application scope is wide, can place in the laboratory, in the special little space testing ring border such as tunnel, rotor shaft to unmanned aerial vehicle is fixed convenient, the operation is thus simple.