| 摘要 |
FIELD: aircraft instrument manufacture. SUBSTANCE: invention specifically refers to information support of navigation, sighting and piloting of aircraft. Proposed complex navigation system incorporates air signal system, unit of coordinate conversion, unit of algebraic summation, correction system, correction unit, unit forming coordinates, delay unit, unit identifying errors, unit of optimal filtration, unit forming components of wind velocity. EFFECT: increased accuracy of determination of air parameters ( true air speed, angles of attack and sideslip, isolation of components of wind velocity ) fed to sighting, indication and control systems of aircraft. 1 cl, 2 dwg
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