FIELD: flight vehicle attitude and heading control systems. SUBSTANCE: in the process of aircraft-to- target approach the method of guidance requires displacement of the aircraft-dummy target line in parallel with the original position of this line in contradistinction to the method of parallel approach providing for parallel displacement of the aircraft- target line. The device for realization of the method is described with the aid of the device block diagram, with employment of discriptions of self-contained units of displacement dummy target, range unit, approach rate unit and lead angle unit. EFFECT: enhanced efficiency. 2 cl, 5 dwg
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Authors
Dates
1999-08-27—Published
1994-01-26—Filed