Radar device for object self-protection
AssigneeDiehl Munitionssysteme GmbH & Co. KG
InventorsGunnar Pappert, Klaus Schluter
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AssigneeDiehl Munitionssysteme GmbH & Co. KG
InventorsGunnar Pappert, Klaus Schluter
Estimating the term…
In regard to radar guidance of a launch container (15) for fragmentation projectiles (16) for defending against an attacking missile (12), from the object (11) to be protected, the present invention affords a radar guidance system which can be inexpensively set up from existing components and which, in the absence of interfaces between the object (11) and the launch container (15), operates in a trouble-free manner if, for space monitoring and target acquisition, provided on the substructure (14) of the launch container (15) which is fixed with respect to the object, there is a planar antenna (20) which transmits its target information to a target-tracking radar (19) which is integrated into the launch container (15), for directly guiding the launch container (15) on to the approach of the missile (12) to be defended against.
A radar device (17) with a planar antenna (20) comprising grouped individual radiating devices (21) for object self-protection against the threat from an attacking missile (12), characterised in that the individual radiating devices (12) are arranged in at least one vertically oriented group as monitoring radar (18) on the substructure (14), which is fixed with respect to the object, of a launch container (15) for fragmentation projectiles (16), which in turn is provided with a target-tracking radar (19) vectored by the monitoring radar (18), for the approach movement (24) of the missile (12) to be defended against.
A radar device according to one of the preceding claims characterised in that the target-tracking radar (19) is a monopulse radar which is vectored by the monitoring radar (18).
A radar device according to the preceding claim characterised in that the monitoring radar (18) and the target-tracking radar (19) are both connected to a positional control device (26) for the drives (27) for spatial orientation and then for target tracking of the launch container (15).
Dependencies are inferred from the claim text.