Visual display apparatus

• US 4,347,508 A
• Filed: 12/21/1979
• Issued: 08/31/1982
• Est. Priority Date: 12/21/1978
• Status: Expired due to Term

• Current Assignee: Redifon Simulation Limited
• Original Assignee: Redifon Simulation Limited
• Inventors: Spooner, Archer M.
• Primary Examiner(s): Groody, James J.
• Application Number:
  US06/105,877
• Time in Patent Office: 984 Days
• Field of Search: 340/27 R, 340/27 NA, 340/366 F, 340/706, 340/712, 340/805, 340/814, 340/724, 340/709, 340/705, 358/103, 358/104, 358/88-90, 358/250, 434/43, 434/44, 350/298, 455/605, 455/606, 455/609, 455/612, 356/152
• US Class Current: 345/8
• CPC Class Codes: G02B 2027/0118 comprising devices for improving the contrast of the display / brillance control visibility
• CPC Class Codes: G02B 2027/0132 comprising binocular systems
• CPC Class Codes: G02B 2027/0136 with a single image source for both eyes
• CPC Class Codes: G02B 2027/014 comprising information/image processing systems
• CPC Class Codes: G02B 2027/0143 the two eyes not being equipped with identical nor symmetrical optical devices
• CPC Class Codes: G02B 2027/0154 with movable elements
• CPC Class Codes: G02B 2027/0187 slaved to motion of at least a part of the body of the user, e.g. head, eye
• CPC Class Codes: G02B 2027/0198 System for aligning or maintaining alignment of an image in a predetermined direction
• CPC Class Codes: G02B 27/017 Head mounted
• CPC Class Codes: G02B 27/0172 characterised by optical features

Abstract

The invention provides head-coupled area-of-interest visual display apparatus particularly for ground-based craft-flight simulators. The apparatus provides binocular, three-dimensional vision of a display, projected onto a part-spherical retro-reflective screen, for one pilot, covering an area of interest centered upon the pilot'"'"'s line of view. The image generator used may be of the computer generated image, laser-scanned model or closed-circuit television type. For the three-dimensional viewing, a modified image is provided for each eye and the two images are separately projected from points on a pilot'"'"'s helmet horizontally in line but vertically displaced above the pilot'"'"'s eye positions. Line scan apparatus is mounted in the pilot cockpit; line image transmission is by a pair of fibre optic light guide ribbons; and frame scan apparatus is mounted on the pilot'"'"'s helmet. A position sensor detects head/helmet movements to permit voluntary scanning of a wide angle of simulated pilot view from the craft.

Claims

1. Head-coupled, area-of-interest, visual display apparatus providing three-dimensional viewing for one viewer, comprising a part-spherical retro-reflective screen of area greater than a viewer'"'"'s instantaneous field of view, a helmet, sensing means for sensing the orientation of the viewer'"'"'s head and helmet, visual image generating means (CGI) for generating an image representing a simulated view in the direction of the viewer'"'"'s instantaneous line of view according to the viewer'"'"'s simulated position and heading and under control of the said sensing means, the said image generating means being adapted for providing two visual images corresponding respectively to the viewer'"'"'s left eye and right eye views, a laser light source for supplying a laser beam which is split to pass through separate laser beam modulators for the left eye and right eye views, separate line scanners for each said view for scanning the modulated laser beam over the input ends of respective fibre optic light guides, the said fibre optic light guides having their output ends at spaced-apart positions on the viewer'"'"'s helmet, and frame scanning means mounted on the said helmet for receiving light from the light guide outputs and projecting the light as a scanned image upon the said screen.

2. Head-coupled, area-of-interest, visual display apparatus as claimed in claim 1, in which the visual image generating means is of the computer-generated image type and simultaneously computes corresponding left-eye and right-eye images and provides corresponding modulation signals for the said left-eye and right-eye laser beam modulators.

3. Head-coupled, area-of-interest, visual display apparatus as claimed in claim 2, in combination with a ground-based craft flight simulator, in which the computer-generated image generating means is provided with input signals from a craft flight computer defining craft position and altitude and is also provided, by way of a summing unit, with input signals from the craft flight simulator defining craft attitude and with input signals from the said sensing means defining the viewer'"'"'s head attitude.

4. Head-coupled, area-of-interest, visual display apparatus as claimed in claim 3, wherein said line scanners and frame scanning means are each provided with control means and wherein the computer-generated image generating means is of a form subject to perceptible delay in computing said simulated image upon change of viewer'"'"'s instantaneous line of view from a first line of view to a new line of view, including throughput delay error compensation means which is supplied with an input signal from the viewer'"'"'s head and helmet orientation sensing means and is operative to compensate the line scan control means and the frame scan control means so as to project the scanned image upon the screen in said first line of view for the period of said delay.

5. Head-coupled, area-of-interest visual display apparatus as claimed in claim 1, in which the retroreflective screen has a reflective characteristic such that it reflects a lesser proportion of light along the line of incidence from the frame scanning means to the screen and a greater proportion of light along the viewer'"'"'s line of view from the screen to the viewer'"'"'s eyes.