Provided is an aircraft component digitized flexible assembling measuring method based on a
laser tracking measuring technique. The assembling measuring method comprises the following steps of (1) carrying out preparation work of assembling measurement, (2) carrying out work of the assembling measurement, and (3) carrying out parallel collaborative measurement in real time. The aircraft component digitized flexible assembling measuring method based on the
laser tracking measuring technique relates to the combination of an assembling technique and the measuring technique, the theoretical position information of
engineering data concentrated product digital analogy is compared with the coordinates, obtained by a
laser tracking instrument in real time, of reference points of
assembly parts to form positional deviation, the positional deviation is transmitted to a
movement control system, the
movement control system generates tool
pose control instructions by analyzing the positional deviation and transmits the tool
pose control instructions to a flexible tool, the flexible tool drives a workpiece to adjust poses together, and through the coordinated operation of the
movement control system, the flexible tool and the workpiece, a
closed loop control system is formed to complete the assembling work. The aircraft component digitized flexible assembling measuring method based on the laser tracking measuring technique has good practical value and wide application prospect in the laser tracking measuring technique and the aircraft digitalized assembling field.