HIDDEN SELF-GUIDANCE METHOD OF AIRCRAFTS TO AIR OBJECTS Russian patent published in 2011 - IPC G01C21/00 

Abstract RU 2408845 C1

FIELD: instrument making.

SUBSTANCE: trajectory of aircraft is always in sector of invisible movement directions, the sizes of which are determined with zone of Doppler resection, in which the aircraft is not determined and not followed. Hidden self-guidance can be performed both in active and in passive operating modes of the aircraft. At active operating mode the aircraft simultaneously measures relative bearing, angular speed of observing line, target range and speed of approach to it, on the basis of processing of which the mismatching parametre shall be determined as per the specified law.

EFFECT: enlarging functional capabilities.

7 dwg

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RU 2 408 845 C1

Authors

Verba Vladimir Stepanovich

Gandurin Viktor Aleksandrovich

Kirsanov Aleksandr Petrovich

Merkulov Vladimir Ivanovich

Suzanskij Dmitrij Nikolaevich

Dates

2011-01-10Published

2009-12-24Filed