公开(公告)号：EP1218685A1

公开(公告)日：2002-07-03

申请号：EP00952120.4

申请日：2000-08-09

申请人： Saab Bofors Dynamics AB

发明人： REGEBRO, Christer

IPC分类号： F41G7/00 ,  F41G7/24 ,  F41G7/34 ,  F41G3/14

CPC分类号： F41G7/301

摘要： The present invention relates to a method and an arrangement for guiding a missile. In accordance with the prior art, the angle position of a target (9) when the missile (3) is expected to reach the target is predicted on the basis of the angular velocity determined in a preceding time period. In order to improve the strike accuracy, the operator, in a second subsequent time period, tracks the actual position of the missile in relation to the predicted angle position of the target. If a deviation is observed, a correction command is transmitted to the missile in order to correct the missile trajectory. For this purpose, a communications link is provided to transmit the correction command given by the operator.

公开(公告)号：EP1328769A1

公开(公告)日：2003-07-23

申请号：EP01961569.9

申请日：2001-09-03

申请人： Saab Bofors Dynamics AB

发明人： HELANDER, Jyrki

IPC分类号： F42B12/14

CPC分类号： F42B12/14

摘要： The present invention relates to a method for attacking a target by means of a missile (1) with at least one shaped charge, the direction of action of which differs from the direction of flight of the missile, and to a missile (1) comprising at least one shape charge (2) arranged to act in a direction (4) that differs from the direction of flight (5) of the missile. The shaped charge jet is corrected for the speed of the missile (1). According to the invention, the correction of the shaped charge jet is adjustable, whereby the lethality of the missile can be achieved within a wide range of speeds of the missile.

公开(公告)号：EP0932838B1

公开(公告)日：2007-02-14

申请号：EP97909816.7

申请日：1997-10-16

申请人： Saab Bofors Dynamics AB

发明人： TULLSSON, Bert-Eric

IPC分类号： G01S13/34

CPC分类号： G01S7/36 ,  G01S7/023 ,  G01S7/2928 ,  G01S7/352 ,  G01S13/34 ,  G01S13/343 ,  G01S2007/356

摘要： This invention concerns a procedure for the elimination of interferences of short duration, such as pulses, in a radar unit of the FMCW type where the transmitted and received signals are combined to form a useable signal. According to the procedure, the contribution to the Fourier Transform of the interferences of short duration are filtered out of the Fourier Transform in the frequency domain by an FIR filter with complex coefficients. The procedure requires no additional signal processing between sampling and applying the Fourier Transform, gives very little widening of strong contrasts in the Fourier Transform, is quick and is simple to implement in a signal processor.