FIELD: radar ranging and radio navigation.
SUBSTANCE: invention relates to radar ranging, in particular, to systems for determining location of aircrafts by a multi-position non-radiating observation system "navigation satellites – aerial targets – receiver", in which signals of navigation satellites of global navigation satellite systems (GNSS) are used to illuminate aerial targets. In a multi-position surveillance system consisting of N satellites and a receiver, determining coordinates of aerial targets is carried out based on measurements on scattered signals of distances Rnm=rnm+rm (rnm is distance from n-th satellite, n = 1, 2, …, N, to m-th air target, m = 1, 2, …, M, rm is distance from m-th target to receiver), along propagation path "n-th navigation satellite – m-th air target – navigation receiver" is calculated NM possible versions of coordinates of aerial targets xcm, ycm, zcm using corresponding system of equations, estimating unknown coordinates xcm, ycm and zcm is found by solving system of equations using apparatus of pseudoinverse matrices. After calculating NM possible versions of coordinates of targets associated with NM possible combinations of distances, according to a certain criterion, a decision is made on whether the true coordinates of a target are true.
EFFECT: determining location of several air targets by multi-position radar system based on measurements of sums of distances from targets to satellites and receiver, coordinates of which are known, by direct, non-iterative method, using direct solution of system of nonlinear equations for coordinates calculation.
1 cl, 1 dwg
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Authors
Dates
2019-06-26—Published
2018-12-03—Filed