FIELD: navigation equipment. SUBSTANCE: proposed system is designed for use in mix of complexes of navigation equipment of aircraft. System comprising autonomous navigation system, satellite navigation system, two integrators, two correction filters and four adders is supplemented with two amplifiers, two adders, two integrators, delay line and differential element which ensures increase of precision of determination of coordinates of position and speed of aircraft. EFFECT: increased precision of complex navigation system. 2 cl, 5 dwg
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Authors
Dates
2002-01-10—Published
2000-10-03—Filed