Three dimensional imaging millimeter wave tracking and guidance system

• US 5,455,587 A
• Filed: 07/26/1993
• Issued: 10/03/1995
• Est. Priority Date: 07/26/1993
• Status: Expired due to Term

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Schneider, Arthur J.
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US08/097,298
• Time in Patent Office: 799 Days
• Field of Search: 342/62, 244/3.11, 244/3.12, 244/3.14, 244/3.17, 244/3.19
• US Class Current: 342/62
• 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 7/414 Discriminating targets with respect to background clutter

Abstract

An improved imaging system. The inventive imaging system (10) is adapted to transmit a plurality of first radar signals at millimeter wave frequencies at an area including an object along with background clutter. The return signals are processed to provide a three dimensional image for applications demanding visibility through fog, haze, smoke and other obscurants. Such applications include enhanced vision for helicopters, ships, buses, trucks, traffic observation stations for an intelligent highway or security cameras for plants and military installations. In a guidance system application, for example, the inventive system would include an electronically scanning antenna (12) to provide range and amplitude signals representative of a target area. The range and amplitude signals (18, 20) are compared to stored signals (26, 30) to create the three dimensional image. The stored signals are selected for comparison based on the dive angle of the missile (28, 32). The three dimensional image is then processed (22, 24, 34, 36, 38, 40) to derive guidance commands for the missile.

Claims

1. A guidance system for a missile having a velocity vector, said guidance system comprising:

first means for transmitting a plurality of first radar signals at an area including a target and background clutter;

second means mounted on said missile for receiving reflections of said radar signals from said target and said background clutter at first and second angles relative to said velocity vector and generating second signals in response thereto;

third means for processing said second signals and constructing a three dimensional sensed image in response thereto, said third means including;

means for processing said second signals and providing a plurality of third signals representing range as a function of said first and second angles and a plurality of fourth signals representing intensity as a function of said first and second angles,

means for storing said third signals to provide a range image,

means for storing said fourth signals to provide an amplitude image;

fourth means for providing a three-dimensional stored image including;

means for providing a first reference map for elevation profile and

means for providing a second reference map for amplitude;

fifth means for comparing said range image to said first reference map and providing a first error signal in response thereto;

sixth means for comparing said amplitude image to said second reference map and providing a second error signal in response thereto;

seventh means for processing said first and second error signals to provide a third error signal which represents a difference between an aimpoint of said missile in said sensed image and an aimpoint of said missile in said stored image; and

eighth means for generating guidance correction signals for said missile from said third error signal.

2. The invention of claim 1 further including means for providing an indication of a change in the aspect and dive angle of the missile.

3. The invention of claim 2 wherein said means for providing a first reference map for elevation profile includes means for providing plural first reference maps.

4. The invention of claim 3 including means responsive to said means for providing an indication of a change in the aspect and dive angle of the missile for selecting one of said plural first reference maps for comparison to said range image.

5. The invention of claim 2 wherein said means for providing a second reference map for amplitude includes means for providing plural second reference maps.

6. The invention of claim 5 including means responsive to said means for providing an indication of a change in the aspect and dive angle of the missile for selecting one of said plural second reference maps for comparison to said amplitude image.

7. The invention of claim 1 wherein said first means includes a millimeter wave radar transmitter.