The invention discloses an integrated navigation information fusion method. The method is mainly divided into a GNSS satellite signal processing module, a SINS attitude, velocity and position updatingmodule, a SINS error compensation module, a SINS/GNSS information fusion module, a SINS error correction module and a result output module. According to the method, by means of high-frequency SINS attitude, velocity and position updating and low-frequency GNSS information measurement, the elevation angle and navigation information carrier-to-noise ratio of all visible satellites tracked by an integrated navigation receiver are combined, a SINS/GNSS integrated navigation Kalman filter observation noise matrix is adaptively adjusted in real time, by means of GNSS and SINS pseudorange and a pseudorange rate measuring value, an integrated navigation Kalman filter state equation and an error covariance matrix are updated, and finally by means of SINS and GNSS information infusion feedback, aninertial device measuring error is corrected. According to the integrated navigation information fusion method, the purpose that under the complex electromagnetic environment, the integrated navigation receiver completes robust information fusion resolving can be achieved, and the method has high integrated navigation receiver design theory value and engineering application value.