FIELD: instrumentation; aviation.
SUBSTANCE: invention relates to aircraft instrumentation and can be used in systems of navigation equipment of aircraft. For this, method uses interconnected inputs-outputs via data exchange channel set multifunctional indicators, set of navigation-piloting means, portable initial data medium, computer system including interconnected at line inputs-outputs of computer information exchange computation-logical modules of integrated database (OBD), formation of navigation-piloting parameters (FNPP), forming displayed information (FOI), generating control signals (FUC), input-output and control of information exchange (VVUIO). Integrated navigation system and aircraft control is additionally equipped with embedded in computer system computation-logical modules of estimation of aircraft position relative to navigation point and formation of apparent drift angle.
EFFECT: broader functional capabilities.
1 cl, 4 dwg
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Authors
Dates
2016-07-10—Published
2015-01-29—Filed