Parallax correction apparatus for a head-up display

• US 4,752,824 A
• Filed: 03/20/1987
• Issued: 06/21/1988
• Est. Priority Date: 03/20/1986
• Status: Expired due to Fees

• Current Assignee: GEC Marconi Limited (Gooding Consumer Electronics Ltd.)
• Original Assignee: Rank Pullin Control Limited
• Inventors: Moore, William T.
• Primary Examiner(s): Britton, Howard W.
• Assistant Examiner(s): Kostak, Victor R.
• Application Number:
  US07/028,505
• Time in Patent Office: 459 Days
• Field of Search: 358/103, 358/113, 358/250, 358/104, 358/107, 358/109, 358/139, 350/174, 340/705, 340/980
• US Class Current: 348/115
• CPC Class Codes: H04N 5/33 Transforming infrared radiation cameras or camera modules for generating image signals from infrared radiation H04N23/20; circuitry of SSIS for transforming infrared radiation into image signals H04N25/20
• CPC Class Codes: H04N 7/183 for receiving images from a single remote source

Abstract

Thermal imaging apparatus particularly but not exclusively for use on an aircraft with a head-up display is provided with signal processing means which progressively expands or compresses the image in the vertical and/or horizontal direction to compensate for parallax arising from the difference in the positions of the observer and the scanner. The adjustment is performed, in the preferred embodiment, as a function of height of the aircraft.

Claims

1. Imaging apparatus for producing a video signal for display on a head-up display, comprising imaging means for providing a first video signal corresponding to an image of a field of view, and signal processing means operable to process said first video signal to derive a second video signal for display by the head-up display in which the dimension of the image in at least one direction is progressively varied to compensate at least partially for a difference between the location of the imaging means and the location of the head-up display.

2. Apparatus according to claim 1, wherein said progressive variation is an expansion which is progressively less for each successively higher portion of the image.

3. Apparatus according to claim 1 wherein said signal processing means is operable to derive said second video signal by interpolation from adjacent pairs of lines of said first video signal.

4. Apparatus according to claim 1, for use in an aircraft wherein said signal processing means is arranged to receive a signal representing aircraft height and said variation is carried out as a function of said height representing signal.

5. Apparatus according to claim 1, for use in an aircraft wherein said signal processing means is arranged to receive a signal representing aircraft tilt angle and said variation is carried out as a function of said tilt angle.

6. Apparatus according to claim 1, wherein said image processing means is operable to compress the image horizontally in successive lines progressively.

7. Apparatus according to any preceding claim, in combination with a head-up display arranged to display an image corresponding to said second video signal.

8. Apparatus according to claim 1, wherein said imaging means includes scanning means for scanning a field of view in line scan and frame scan directions.