Multi-point coordinated airplane hoisting device

The invention belongs to the technical field of airplane static tests, and particularly relates to a multi-point coordinated airplane hoisting device. Comprising a first upper frame, a second upper frame and a third upper frame, a front undercarriage is fixedly installed in the first upper frame, a left main undercarriage is fixedly installed in the second upper frame, and a right main undercarriage is fixedly installed in the third upper frame; the first double-position control actuator cylinder assembly is installed on the first upper frame in the spanwise direction, the second double-position control actuator cylinder assembly is installed on the second upper frame in the heading direction, and the third double-position control actuator cylinder assembly is installed on the third upper frame in the heading direction. The third double-position control actuator cylinder assembly is installed on the third upper frame in the course direction. The full-floating support assembly comprises a first full-floating s