Polarization controlled map matcher missile guidance system

• US 4,490,719 A
• Filed: 11/27/1981
• Issued: 12/25/1984
• Est. Priority Date: 11/27/1981
• Status: Expired due to Term

• Current Assignee: Westinghouse Norden Systems Inc (Northrop Grumman Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Kosowsky, Lester H., Botwin, Leo
• Primary Examiner(s): Tubbesing, T. H.
• Application Number:
  US06/325,520
• Time in Patent Office: 1,124 Days
• Field of Search: 343/5 MM, 343/7 ED
• US Class Current: 342/64
• CPC Class Codes: F41G 7/2226 comparing the observed data with stored target data, e.g. target configuration data
• CPC Class Codes: F41G 7/2246 Active homing systems, i.e. comprising both a transmitter and a receiver
• CPC Class Codes: F41G 7/2286 using radio waves
• CPC Class Codes: G01S 13/883 for missile homing, autodirectors missile guidance systems F41G7/22
• CPC Class Codes: G01S 13/9023 combined with interferometric techniques
• CPC Class Codes: G01S 13/9076 Polarimetric features in SAR

Abstract

A reference grid for a map matching missile guidance system is generated from a vertically polarized radar map and a horizontally polarized radar map, both of which represent radar returns from a preselected ground area. In generating this reference grid, illuminating radar pulses are alternately fed to a horizontal aperture and vertical aperture of a mapping radar. Horizontal radar returns and vertical radar returns are processed in separate channels to form a radar map of the ground area containing the target to which the missile is to be directed. A pixel-by-pixel comparison of the data in each map is performed to create a polarization diverse map which is essentially those returns from man-made objects. This map is then used by the missile guidance system as a reference grid for a final fix by which the missile obtains its final course orientation enroute to the target.

Claims

1. A method of providing a H-V reference grid for the guidance system of a missile, comprising the steps of:

providing a radar with horizontal aperture and a vertical aperture;

switching alternate illuminating pulses from the transmitter of said radar first to said horizontal aperture and then to said vertical aperture;

providing a separate receiver channel for horizontal radar returns and for vertical radar returns;

generating a horizontal map from said horizontal radar returns and a vertical map from said vertical radar returns, each of which has said radar returns organized in an array corresponding to various ground locations;

generating a polarization discriminant map by comparing on a pixel-by-pixel basis the location and intensity of radar returns in said vertical map with those in said horizontal map to identify only those returns which are colocated and have equal polarization intensity; and

feeding the polarization discriminant to the guidance system of the missile.