Visual display apparatus

• US 4,263,726 A
• Filed: 04/12/1979
• Issued: 04/28/1981
• Est. Priority Date: 04/22/1978
• Status: Expired due to Term

• Current Assignee: Redifon Simulation Limited
• Original Assignee: Redifon Simulation Limited
• Inventors: Bolton, Martin J. P.
• Primary Examiner(s): Atkinson, Charles E.
• Assistant Examiner(s): Chin, Gary
• Application Number:
  US06/029,467
• Time in Patent Office: 747 Days
• Field of Search: 35/10.23, 35/10.24, 35/12 N, 35/12 P, 364/515, 364/521, 364/522, 364/731, 358/103-105
• US Class Current: 434/43
• CPC Class Codes: G09B 9/302 the image being transformed by computer processing, e.g. updating the image to correspond to the changing point of view

Abstract

Visual display apparatus for ground-based craft flight simulation apparatus using a raster scan display for viewing by the trainee pilot and providing an image comprising a target or other craft, together with cloud extending to the simulated horizon. The cloud image part has repetitively patterned features and is displayed in correct perspective, according to the simulated flight position relatively thereto, for providing speed and altitude cues. This part of the image is provided by digital means, a single cycle of the repetitive pattern being held in a digital store and perspective being computed continuously. The whole apparatus includes three generators providing respectively sky, horizon and patterned cloud surface all controlled by a general purpose computer receiving flight data from the simulator flight computer. Outputs from the three generators are selected appropriately during the raster scan of the display and also appropriately combined with a high-definition image of the target or other craft.

Claims

1. Visual display apparatus for a ground-based craft flight simulator including a flight computer, comprising raster scan type display means for viewing by a trainee pilot observer, synthetic image generating means for supplying to the display means a signal representing an image of sky, horizon and a simulated patterned surface extending to the horizon, said patterned surface being displayed in true perspective in accordance with the simulated altitude and position in space relative thereto of the craft simulated and a general purpose programmable computer connected to interface the said flight computer and the said synthetic image generating means, said synthetic image generating means including discrete surface pattern generator, sky image generator and horizon logic units, the general purpose computer receiving as an input flight related data from the flight computer, being programmed to continuously compute functions of said flight related data and being connected to supply values of said functions to each of the units of the synthetic image generating means, said surface pattern generator including an inverse perspective transformation computer and a digital pattern store, the pattern store holding a single pattern cycle of a repetitive pattern for patterning said patterned surface in one dimension thereof, said sky image generator providing a signal output for the display means representative of a variable brightness portion of sky, both surface pattern and sky image generators supplying signals to switch means for selectively supplying to the display means either the signal representative of the patterned surface or the signal representative of the variable brightness portion of sky, continuously during the raster scan of the display means.

2. Visual display apparatus as claimed in claim 1, in which X and Y vector information relating to the two dimensions of the said simulated patterned surface is supplied by the inverse perspective transform unit to address the pattern store, the output from which is supplied to the image modification unit.

3. Visual display apparatus as claimed in claim 2, in which the image modification unit receives data defining a perspective-transformed simulated pattern image from the said pattern store, the data output of the said general purpose computer, and raster display timing pulses and supplies simulated patterned surface signals suitable for the said display means, by way of the said switch means.

4. Visual display apparatus as claimed in claim 3, in which the said inverse perspective transform unit for X vector information comprises two function generators, both receiving the data output of the said general purpose computer, both receiving the said raster display timing pulses and both supplying outputs to a divider, the output from which divider is added to the earlier value of X (X_o) in a following adder, which adder is supplied with the data output of the said general purpose computer and supplies the incremented value of the X vector for addressing the said pattern store.

5. Visual display apparatus as claimed in claim 4, in which, as the X vector value increases so that the simulated pattern surface diminishes in size in the said perspective display of raster scan display means, the said image modification unit functions to prevent the generation of a Moire pattern.

6. Visual display apparatus as claimed in claim 5, in which the image modification unit comprises a function generator, which receives the data output of the said general purpose computer and the raster display timing pulses, is followed by a limiter and by a multiplier, which multiplier receives an input from the said pattern store, the multiplier output being supplied to an adder, which adder also receives the data output of the said general purpose computer, the adder output being supplied to the said switch means.