FIELD: instrument engineering.
SUBSTANCE: according to the measurements of current navigation parameters for the short measured interval the iterative alignment of vector of the state on the set of correctness is carried out, using the checking sequence of test iterations under conditions of incomplete implementation of operational scheme of carrying out the radio control of the orbit. At that the procedures of statistical processing of sessions of measurements of current navigation parameters are used. The conditions of stability and reliability of the measurements are provided on the basis of formation of checking sequence of alternative solutions containing the optimal solution, which is chosen on the basis of conformity to it of projection of vector of measuring error of current navigation parameters on the space of adjustable parameters not exceeding the specified error of the defined vector of parameters of motion of artificial satellite of the Earth.
EFFECT: improvement of accuracy and operational efficiency of the artificial satellite of the Earth positioning.
1 dwg
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