Abstract:In this paper, a new method of high precision celestial navigation was introduced, with the method, a calculation model of attitude and course was constructed about celestial navigation in the celestial sphere coordinate system. The model conducted attitude calculation and course calculation on the premise of not using INS attitude data, conducted precise attitude and course of carrier by the evolution of the model being constructed, and it could correct attitude error and course error as a result of inertia gyro drift of inertial navigation equipment.