FIELD: radio navigation. SUBSTANCE: measuring station radiates signal with fref frequency. Reflected signal is received during scanning beam of aerial according to Qrec(t) law. Time interval ts is measured between start point of scanning for reception and moment of start point of reception of reflected signal. Doppler frequency fd is measured. Then the signal is received and angle γ of viewing is determined from the relation g =arctg [(dQrec(t)/d(t)·(fref/fdτn)]- Qrec(t) + Qrec(ts), where τn is time interval between start point of radiation and start point of scanning of aerial beam for reception of reflected signal. EFFECT: improved precision. 5 dwg
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