FIELD: aircraft instrumentation engineering. SUBSTANCE: information landing system is provided in addition with correction unit, corrected range shaping unit, and correction shaping unit which provides for accurate correction of altitude and horizontal range due to provision for satellite coordinate sensor, reference-point polar coordinates sensor, and reference-point lock-on modes determined by control console. EFFECT: improved accuracy of information support for landing conditions. 4 dwg
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Authors
Dates
1994-11-30—Published
1992-05-18—Filed