FIELD: radio engineering.
SUBSTANCE: invention relates to radio engineering, namely to passive radio monitoring systems, and can be used in systems for monitoring proper location of a navigation object as an alternative method of determining coordinates, in particular, in conditions of malfunction or failure of a receiver of signals of global navigation satellite systems (GLONASS, GPS, etc.). In the disclosed method, the navigation object proper location in space is determined by receiving radio signals from N≥2 independent radio-emitting objects with known coordinates using a tri-orthogonal frame antenna system (TOFAS) installed on a navigation object and measuring triplets of orthogonal components using it at times t1 and t2 Hx,n(t1), Hy,n(t1), Hz,n(t1) and Hx,n(t2), Hy,n(t2), Hz,n(t2), electric field strength vectors Hn(t1) and Hn(t2) of received signals from independent radio-emitting objects with known coordinates. Further, orientation angles of TOFAS in space are measured, orientation of electric field intensity vectors Hn t(t1) and Hn t(t2) in the topocentric DCS OXYZ taking into account the measured orientation angles of TOFAS ξα, ξβ, ξγ. Auxiliary planes are formed Ωn(t1) and Ωn(t2) so that they are perpendicular to vectors Hn t(t1) and Hn t(t2) and passed through corresponding radio-emitting objects with known coordinates. Object location lines ln are determined at intersections of said planes and coordinates of navigation object proper location are calculated as points of object location ln intersection.
EFFECT: wider field of use of the navigation system with high accuracy of determining the proper location of a navigation object by providing polarization matching between the receiving antenna system and the field of the incoming electromagnetic wave from radio-emitting objects with known coordinates.
2 cl, 4 dwg, 1 ex
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Authors
Dates
2024-09-23—Published
2023-12-18—Filed