FIELD: radar landing systems of flight vehicles, applicable in air traffic control systems.
SUBSTANCE: the system has a landing radar, information processing unit, co-ordinate computer unit, video transducer, final controller indicator, flight and navigation unit included in the console of the final controller, on-board video transducer, pilot display included in the pilot's console, two-sided data link including ground receiver and transmitter interconnected by a ground antenna system, and on-board receiver and receiver interconnected by an on-board antenna system, on-board drivers of the vectors of the heading and glide-path speeds and a ground divider of vectors of the heading and glide-path speeds, transducer of the parameters of the boundaries of vertical and horizontal visibilities, drivers of the vectors of wind speeds in heading and glide-path, on-board drivers of the vectors of the optimum heading and glide-path speeds, on-board divider of ground information. Provision is made for alignment at pilotage of the flight vehicle of the vectors of the current heading and glide-path speeds with the respective vectors of the optimum speeds.
EFFECT: enhanced safety of flights at bringing landing and at landing.
5 cl, 4 dwg
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Authors
Dates
2004-10-27—Published
2003-04-02—Filed