Attitude simulation device for rotor unmanned aerial vehicle

• Main Authors: SANG CHEN, HAN DONG, SANG TAO, HUANG GUOXIAN, SONG XIAODONG, WU BIN, SHUI XIAOBING
• Format: Patent
• Language: Chinese; English
• Published: 08.11.2019
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; PERFORMING OPERATIONS; TRANSPORTING

The utility model belongs to the technical field of unmanned aerial vehicle simulation/test devices, and discloses an attitude simulation device for a rotor unmanned aerial vehicle, which is providedwith a rotary inner ring; the rotary inner ring is connected with the supporting device through a bolt, the rotary inner ring is located in the rotary outer ring, and the rotary inner ring and the rotary outer ring form a structure similar to a bearing and can rotate relatively; the rotary outer ring is connected with the rotating device base through bolts and screws, the V-shaped pulleys are fixed to the rotating device base through fixing screws, and the V-shaped pulleys are fixed to the upper side and the lower side of the guide rail base and used for clamping the guide rail base. Accordingto the utility model, the simulation of three rotational degrees of freedom of the rotor unmanned aerial vehicle can be realized, and the rotational centers of the three degrees of freedom are superposed, so that the simulati