FIELD: transport.
SUBSTANCE: invention relates to data display systems used as flying aids. Proposed system comprises unit of transducers to measure current data on aircraft, robot pilot that can receive data required for aircraft flight in preset path, display to visualise aircraft flight conditions and control device composed of the following components: unit to generate the preset angle of attack, unit to generate preset gliding angle and display control unit. Said unit to generate the preset angle of attack allows determination of preset angle of attack for approach to preset flight pass proceeding from pitch angle measured by said unit of transducers and angle of path that makes the angle between horizontal plane and preset flight direction to be obtained with the help of robot pilot. Said unit to generate preset gliding angle allows determination of preset gliding angle for approach to preset flight path proceeding from heading measured by the unit of transducers and course angle for preset flight direction provided by robot pilot. Display unit visualises relative difference between preset spatial position relative to airflow represented by preset angle of attack and obtained preset gliding angle and current spatial position relative to airflow represented by current gliding angle.
EFFECT: higher accuracy of holding the preset flight path.
6 cl, 7 dwg
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Authors
Dates
2015-03-20—Published
2011-06-24—Filed