The invention relates to a method for realizing landtype inertial navigation system movement aiming, belonging to the technical field of initial aiming of an inertial navigation system. On the basis of the dynamic error model of an inertial navigation system and an observational equation, the invention takes GPS output speed as an observed quantity, adopts Kalman filtering to estimate the jerk ofcarrier vehicles and judges whether GPS speed output is a wild value. If the GPS speed output is the wild value, the Kalman filtering flatting is adopted to recur the current state, otherwise a master Kalman filter and a slave Kalman filter are adopted to realize synchronous estimation of inertial navigation system state and noise statistical property; the master Kalman filter estimates the stateof the inertial navigation system, and the information and the variance thereof serve as the observed quantity of the filter; and the slave Kalman filter estimates the mean value and the variance of the observation noise of the master filter, and the estimation result provides noise characteristic input for the next filtering of the master filter so as to realize the landtype inertial navigation system movement aiming.