The method uses an IR search head (10), with an IR optical system (13), directing incident IR radiation onto an IR sensor, provided by a matrix detector (14) with point detector elements (15). The amplitude and frequency of the resulting electrical signals are evaluated for identifying the helicopter type and controlling a missile fired against the helicopter (16). The matrix detector is periodically pivoted about an axis parallel to the flight direction during a target region scanning phase and is stabilised upon target detection, for a subsequent target identification phase.
申请公布号
DE19610032(C1)
申请公布日期
1997.07.10
申请号
DE19961010032
申请日期
1996.03.14
申请人
BUCK WERKE GMBH & CO., 73337 BAD UEBERKINGEN, DE
发明人
GAUGGEL, ROLAND, PROF. DR., 88682 SALEM, DE;KRUEGER, REINHARD, DR.RER.NAT., 83317 RUECKSTETTEN, DE