FIELD: instrument engineering.
SUBSTANCE: corresponding system (dwg. 3) and the sequence of operations for work on two orbit groups (dwg. 4) are proposed. In addition, a special-purpose control unit is introduced, in which in the system of navigation equations the fifth time parameter is considered responsible for the divergence of hours of the navigation receiver from the system time of the second orbit group. At that a conversion to a certain linear vector space is carried out, in which the solution of navigation equations system is determined in the parametric form relatively two unknowns, with subsequent determination of these unknowns by calculation of the roots of a polynomial equation.
EFFECT: enhanced functionality.
3 cl, 6 dwg
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