The invention provides an analysis method for predicting pneumatic load and movement rules of a reentry process of a booster. According to the method, a three-dimensional unsteady flow field of the reentry process of the booster is carried out, on the basis of a multiple reference coordinate system principle and a sliding mesh technique, a dynamic boundary condition is combined, and analysis of the reentry motion of the booster is carried out. According to the Newton's laws of motion and a theorem of moment of momentum, and user programs used for calculating height, speed, pitch angle speed and other parameters of the reentry process of the booster are written. The user programs can control rotation of a rotation field to achieve pitching motions of the booster, and the physical environment in the reentry process of the booster is simulated through changes of inlet, outlet and far field boundary condition parameters of a static field. In the process that time advance is used for solving the unsteady flow field, a solver calls the user programs in real time, real-time updating of boundary conditions and the rotation speed of the rotation field is achieved, calculation is never stopped until the booster arrives at the ground, and accordingly the transient pneumatic load and the motion parameters of the booster are obtained.