FIELD: aircraft instrumentation engineering. SUBSTANCE: proposed system includes multi-functional color displays, collimator indicator on windshield and multi-functional control console connected with on-board digital computer by means of multiplex and reserve radial information exchange channels. On-board digital computer is also connected with mode parameter sensors. Multifunctional color displays (no less than three displays) are fully interchangeable; they provide pilot with complete pilotage navigational information in case of failure of one of them and minimum scope of information in case of failure of two of them. EFFECT: enhanced operational reliability. 3 cl, 2 dwg
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Authors
Dates
2003-12-20—Published
2002-11-11—Filed