Missile tracking systems

• US 5,147,088 A
• Filed: 04/16/1987
• Issued: 09/15/1992
• Est. Priority Date: 04/29/1986
• Status: Expired due to Term

• Current Assignee: MBDA UK Ltd. (MBDA SAS)
• Original Assignee: British Aerospace, Inc. (BAE Systems Plc)
• Inventors: Smith, James M., Busby, Peter W.
• Primary Examiner(s): Jordan, Charles T.
• Application Number:
  US07/041,124
• Time in Patent Office: 1,979 Days
• Field of Search: 244/3.11
• US Class Current: 244/3.11
• CPC Class Codes: F41G 7/303 Sighting or tracking devices especially provided for simultaneous observation of the target and of the missile

Abstract

A missile tracking system includes a target image sensor and a missile image sensor which record image data during respective target image exposure periods and missile image exposure periods. The missile is provided with an image enhancer such as a beacon or a corner reflector illuminated from the ground, which enhances the missile image only during the missile image exposure periods.

Claims

1. A tracking system including target image sensor means for imaging the viewed scene for a predetermined controllable first series of exposure periods at predetermined intervals, and for outputting data to enable the location of a target within the viewed scene to be determined, missile image sensor means for repetitively imaging the viewed scene for a predetermined controllable second series of exposure periods interspersed with said first series of exposure periods and for outputting data to enable the location of a missile within the viewed scene to be determined, and means for enhancing the image of the missile or a part thereof only during at least part of each exposure period of said second series of exposure periods.

2. A tracking system according to claim 1, wherein said target image sensor means and said missile image sensor means comprise a single charge-coupled device controlled to output alternate TV field fames having sensitivities adjusted for target tracking and missile tracking respectively.

3. A tracking system according to claim 1, wherein said means for enhancing the image of the missile comprises a missile beacon switched on during each missile tracking field of the image sensor.

4. A tracking system according to claim 3, wherein said beacon comprises an electric gas discharge lamp.

5. A tracking system according to claim 3, wherein said beacon comprises a pulsed laser.

6. A tracking system according to claim 3, wherein said beacon comprises a series of magnesium flash lamps.

7. A tracking system according to claim 1, wherein said means for enhancing the image of the missile includes a reflector associated with said missile and a ground-based laser arranged to illuminate said reflector.

8. A tracking system according to claim 7, wherein said reflector comprises a corner reflector.

9. A tracking system according to claim 7, wherein said laser is adapted to emit a pulse-coded beam during said missile tracking field, said pulse-coded beam containing command data for reception by a command link receiver associated with said missile.

10. A tracking system according to claim 1, wherein said means for enhancing said missile image includes means associated with said missile for emitting closely spaced beacon pulses, means associated with said missile image sensor means for moving the image plane between the first and second pulse, and means for determining the separation between the image of said first pulse and the image of said second pulse.

11. A tracking system according to claim 2, wherein said charge coupled device is operated to provide at least three partial fields during a TV field frame period, one of said partial fields being arranged to provide positional information of a target, another of said partial fields being arranged to provide positional information of a first missile, a yet further partial field being arranged to provide position information of a second missile, means associated with said first missile to enhance its image only during the exposure periods corresponding to said further partial field and means associated with said second missile to enhance its image only during the exposure periods corresponding to said yet further partial field.