The invention discloses a helicopter rotor blade movement parameter measurement method based on vibration correction and belongs to the technical field of vision measurement. The helicopter rotor blade movement parameter measurement method based on vibration correction comprises the following steps of placing a certain number of coded mark points on a hub and blades of a helicopter rotor; constructing a binocular stereo vision system to obtain helicopter rotor image data; calculating three-dimensional coordinates of the coded mark points and constructing a rotor coordinate system; calculatinga transient vibration displacement vector of the rotor in a high speed rotation state to correct the three-dimensional coordinates of the coded mark points; and on the basis of the corrected three-dimensional information of the coded mark points, calculating movement parameters of the rotor blades in the current transient state according to definitions of the movement parameters of the rotor blades. The helicopter rotor blade movement parameter measurement method based on vibration correction, disclosed by the invention, has the advantages that the movement parameters of the rotor blades can be accurately measured by correcting vibration displacement errors caused by rotor high speed rotation, the operation is simple, the method is in the non-contact form, the accuracy is high, and the safety is good.