FIELD: expansion of functional capabilities of global navigation satellite systems. SUBSTANCE: proposed method of angular orientation of objects differs from known method based on reception of signals from spacecraft of global navigation satellite systems by two or more antennas spaced apart and placed in parallel to one or two axes of measured object, on measurement of phase shift between received signals from each spacecraft and on determination of angular position of axes of measured object by solving system of equations by change of angular position of axes of bases on which ends antennas are positioned through unspecified angle before start of measurements or in process of measurement of angular positions of axes of object. After this antennas are returned to initial position. This solves problem of precision and decrease of time of measurement of angular position. EFFECT: increased precision and decreased time of measurement of angular positions. 1 dwg
