The dynamic properties of the thrust test system for the attitude control rocket motor have great influence on the accuracy of the thrust measurement. The piezoelectric thrust test system was dynamically calibrated by using square impulse to simulate the engine thrust. Based on the frequency response curve, a high order transfer function model was established to obtain the dynamic performance indexes of the measurement system. Aiming at the overshooting and the vibration occurred in the process of the thrust measurement, the damping compensation was used to compensate the output of the thrust test system, according to the high order transfer function model. The results showed that the error could be decreased by the damping compensation, and the dynamic performance of the piezoelectric thrust test system was improved.