Visual display apparatus

• US 4,315,240 A
• Filed: 01/11/1980
• Issued: 02/09/1982
• Est. Priority Date: 01/11/1979
• 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:
  US06/111,282
• Time in Patent Office: 760 Days
• Field of Search: 340/380, 340/712, 340/706, 340/805, 340/814, 340/27 R, 340/27 AT, 340/27 NA, 340/709, 340/705, 340/755, 340/724, 35/12 G, 35/12 N, 35/12 F, 358/103, 358/104, 358/88-90, 358/250, 356/152, 250/203 R, 455/605, 455/606, 455/609, 455/612, 434/43, 434/44, 434/38
• US Class Current: 340/980
• 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 a stereoscopic pair of images for both a pilot and co-pilot, projected onto the inside of a part-spherical shell, which carries a concave retro-reflective screen and surrounds the two pilots. The display scenes cover an area of interest centered upon each pilot'"'"'s line of view. A separate image generator is used for each pilot and may be of the computer generated image, laser-scanned model or closed-circuit television type. For stereoscopic viewing a modified image is provided for each eye of each pilot and for each pilot the two images are separately projected from points on a respective pilot helmet above the eye positions. Line scan apparatus is mounted in the pilots'"'"' cockpit; line image transmission is by two pairs of fibre optic light guide ribbons; and frame scan apparatus is mounted on the two pilots'"'"' helmets. A sensor measures head/helmet movements of each pilot to permit voluntary individual scanning of a wide angle of simulated view from the craft.

Claims

1. Head-coupled, area-of-interest, visual display apparatus providing stereoscopic viewing for more than one viewer comprising a part-spherical retro-reflective/concave screen of area greater than a viewer'"'"'s instantaneous field of view and, for each viewer, a helmet, sensing means for sensing the orientation of the respective viewer'"'"'s head and helmet, visual image generating means for generating a simulated scene in the direction of the respective viewer'"'"'s instantaneous line of view according to a common simulated vehicle position and orientation and under control of the respective sensing means, the said respective image generating means being adapted for providing a stereoscopic pair of images corresponding to the respective viewer'"'"'s left eye and right eye views, a laser beam source for producing laser beams, separate laser beam modulators for the left eye and right eye views for modulating said laser beam, separate line scanners for each said view for scanning the modulated laser beams 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 respective 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 as the stereoscopic pair of images for each viewer and provides corresponding video modulation signals for the said left-eye and right-eye laser beam modulators of each viewer.

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

4. Head-coupled, area-of-interest, visual display apparatus as claimed in claim 3, wherein the computer-generated image generating means is of a form subject to perceptible delay in computing the respective simulated image upon change of any 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 respective viewer'"'"'s head and helmet orientation sensing means and is operative to control the line scanners and the frame scanning means of the respective visual image generating means so as to project the respective 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 retro-reflective screen has a reflective characteristic such that it reflects a lesser proportion of light along the line of incidence from the respective frame scanning means to the screen and a greater proportion of light along the respective viewer'"'"'s line of view from the screen to the respective viewer'"'"'s eyes.