Automatic closed loop scaling and drift correcting system and method particularly for aircraft head up displays

• US 4,847,603 A
• Filed: 05/01/1986
• Issued: 07/11/1989
• Est. Priority Date: 05/01/1986
• Status: Expired due to Fees

• Current Assignee: Jet Electronics and Technology Incorporated
• Original Assignee: Jet Electronics and Technology Incorporated
• Inventors: Blanchard, Clark E.
• Primary Examiner(s): Caldwell, Sr., John W.
• Assistant Examiner(s): Fatahi-yar, Mahmoud
• Application Number:
  US06/859,120
• Time in Patent Office: 1,167 Days
• Field of Search: 340/705, 340/980, 358/139, 358/107, 358/103, 358/109, 358/125, 358/201, 324/74, 350/145, 350/174
• US Class Current: 345/7
• CPC Class Codes: G02B 2027/0138 comprising image capture systems, e.g. camera
• CPC Class Codes: G02B 2027/014 comprising information/image processing systems
• CPC Class Codes: G02B 27/01 Head-up displays
• CPC Class Codes: H04N 3/22 Circuits for controlling dimensions, shape or centering of picture on screen

Abstract

A display system and method, especially for use in an aircraft head up display system, for maintaining an optical image in a predetermined position on a light emitting screen. The system has a beam type image generator controlled by an operating circuit. A controlled beam scans both a central display region and marginal regions of the screen. The marginal regions have beam sensors and the beam is controlled by a sequence of plural coordinate commands in accordance with a plural coordinate search pattern restricted to the marginal regions and in the vicinity of the beam sensors. Signals resulting therefrom are utilized to eliminate beam deflection errors.

Claims

1. An aircraft head up display system for providing a display image for viewing by a pilot in the pilot'"'"'s field of view while looking out of an aircraft at a scene, in a forward direction, comprising:

beam type image generating means having a light emitting screen providing a display region which is optically projected so as to provide a display image in the pilot'"'"'s field of view, and having margin regions which are not optically projected into the pilot'"'"'s field of view, said image generating means having a deflectable beam for deflection over the display region, and capable of being deflected at the margin regions;

real time operating means for controlling said image generating means to cause the generation of a real time display in the display region which varies essentially in real time according to the status of the aircraft in flight, so as to assist the pilot in the control of the aircraft; and

beam position sensing means coupled with respective margin regions of the image generating means so as to provide respective beam actual position signals when the beam is momentarily aligned with the respective beam position sensing means,

said real time operating means while maintaining the generation of the real time display which varies essentially in real time, further providing beam deflection commands to cause the beam to scan the respective margin regions according to a plurality of plural coordinate search patterns, each extending in at least both X and Y directions, said scanning of said beam according to said search pattern being restricted to said margin regions and the real time operating means comparing beam actual position signals received from the beam position sensing means to previously stored beam reference coordinate values to determine beam registration error, and automatically correcting the deflection of the beam to substantially eliminate the beam registration error during further generation of the real time display.

2. In an aircraft head up display system according to claim 1, said real time operating means generating correction signals which are a measure of scaling errors with respect to each of plural coordinates of a coordinate system defining points in said light emitting screen of the image generating means such that image lines generated in the display region are corrected as to position and proportion and are maintained with essentially correct geometry during operation of the aircraft.

3. In an aircraft head up display system according to claim 1, said real time operating means generating correction signals which are a measure of drift of the center of the real time display from a central optical axis corresponding to an aircraft longitudinal axis as seen in the pilot'"'"'s field of view, and maintaining the center o the display image essentially coincident with the aircraft longitudinal axis as viewed by the pilot.

4. In an aircraft head up display system according to claim 1, said real time operating means generating correction signals which are a measure of scaling errors with respect to each of plural coordinates of a coordinate system defining points in said light emitting screen of the image generating means such that image lines generated in the display region are corrected as to position and proportion and are maintained with essentially correct geometry during operation of the aircraft, and said real time operating means generating correction signals which are a measure of drift of the center of the real time display from a central optical axis corresponding to an aircraft longitudinal axis as seen in the pilot'"'"'s field of view, and maintaining the center of the display image essentially coincident with the aircraft longitudinal axis as viewed by the pilot.

5. In an aircraft head up display system according to claim 1, said real time operating means generating said sequences of beam deflection commands within a time interval of not more than twenty milliseconds.

6. In an aircraft head up display system according to claim 1, said real time operating means generating a plurality of successive beam deflection commands for each of said search patterns.

7. In an aircraft head up display system according to claim 1, said real time operating means during approach for a landing, generating said sequences of beam deflection commands at intervals of not greater than thirty seconds while maintaining said real time display without flicker.

8. In an aircraft head up display system according to claim 1, said beam position sensing means comprising photosensitive elements coupled with margin regions at diametrically opposite margins of the display region so as to provide for correction of both scaling and drift errors of said display image.

39. The aircraft head up display system according to claim 1, wherein each of said beam position sensing means is a single photodetector.

40. The aircraft head up display system according to claim 39, wherein each of said margin regions has only one beam position sensing means.

9. A real time display system, comprising

beam type image generating means having first and second beam activated regions,

real time operating means controlling said image generating means to effect the generation of a real time display in the first beam activated region which varies essentially in real time according to a physical process, and

beam position sensing means coupled with said second beam activated region of the image generating means so as to provide beam actual position signals representing an actual instantaneous position of the beam with respect to at least two coordinate axes of a coordinate system,

said real time operating means while maintaining the real time display which varies essentially in real time, further providing beam deflection signals causing the beam to scan said second beam activated region so as to produce said beam actual position signals, and said real time operating means supplying a sequence of plural coordinate digital commands for effecting deflection of the beam in accordance with a plurality of plural coordinate search patterns, each extending in at least both X and Y directions and only within said second beam activated region and in the vicinity of the coupling of said beam position sensing means with said second beam activated region and said real time operating means correcting the deflection of the beam so as to tend to maintain a constant relationship between respective coordinate reference values of the beam deflection signals with respect to the two coordinate axes, and beam activation of the beam position sensing means.

10. In a real time display system according to claim 9, said real time operating means storing a plural coordinate digital command value at which the search pattern activates the beam position sensing means.

11. In a real time display system according to claim 10, said real time operating means providing a sequence of digital commands in generating a subsequent search pattern based on a stored plural coordinate digital command value from a preivous search pattern.

12. In a real time display system according to claim 10, said real time operating means providing a further sequence of digital commands in generating a further search pattern, beginning at a stored digital command value corresponding to the position of the beam which produced the beam position signal in a previous search pattern.

13. In a real time display system according to claim 9, said operating means effecting deflection of said beam in said first and second beam activated regions by means of a common stroke type deflection control.

14. In a real time display system according to claim 9, said operating means effecting deflection of said beam over said light emitting screen by means of a common raster-type deflection control.

15. In a real time display system according to claim 14, said raster-type deflection control effecting scanning of the second beam activated region along successive linear beam paths which reliably cover the vicinity of the coupling of the beam position sensing means with said second beam activated region.

16. In a real time display system according to claim 15, said beam position sensing means defining a beam sensing point radially offset outwardly of the first beam activated region and lying at a distance from a beam undeflected position which is larger than a maximum beam deflection from the undeflected position which is required to generate said real time display.

17. In a real time display system according to claim 9, said beam position sensing means defining not more than four beam sensing locations.

18. In a real time display system according to claim 9, said beam position sensing means being coupled with only two beam sensing locations at diametrically opposite margins of the first beam activated region.

41. The aircraft head up display system according to claim 9, wherein said beam position sensing means is a single photodetector.

42. The aircraft head up display system according to claim 41, wherein said second beam activated region has only one beam position sensing means.

19. A display system, comprising:

beam type image generating means for producing a beam and having a light-emitting screen including a central display region and marginal regions radially offset from the central display region,

operating means controlling said image generating means to effect the generation of an optical image in said central display region,

photosensor means coupled with plural individual points at respective marginal regions of the image generating means so as to detect both horizontal and vertical beam deflection errors, the beam when in substantial alignment with the respective individual points causing the photosensor means to produce respective beam actual position signals,

said operating means having beam deflection driver means for effecting deflection of the beam both in the central display region and in the marginal regions, and having deflection control means coupled with said deflection drive means for effecting generation of an optical image in said central display region and for effecting scanning of the beam over said marginal regions so as to activate said photosensor means to generate the respective beam actual position signals, said operating means supplying a sequence of plural coordinate commands for effecting deflection of the beam in accordance with a plurality of plural coordinate search patterns, each extending in at least both X and Y directions and only within said marginal regions and in the vicinity of the plural individual points coupled with said photosensor means,

said operating means correcting the deflection of the beam based on the values of driving signals applied to the beam deflection driver means which are required to cause the beam to activate the photosensor means via the respective individual points thereby maintaining the optical image in a predetermined position on said light emitting screen.

20. In a display system according to claim 19, said operating means correcting the deflection of the beam based on a comparison of the values of driving signals required to cause the beam to impinge on individual points at diametrically opposite sides of an undeflected position of the beam so as to tend to maintain a fixed relationship between a center of the optical image and a center of the light-emitting screen.

21. In a display system according to claim 19, said operating means correcting the deflection of the beam based on a comparison of the values of driving signals required to activate respective points which are substantially spatially separated with respect to a given coordinate system axis so as to tend to maintain a constant scale of the optical image with respect to such coordinate system axis.

22. In a display system according to claim 19, said operating means correcting the deflection of the beam based on a comparison of the values of driving signals required to cause the beam to impinge on individual points at diameterically opposite sides of an undeflected position of the beam so as to tend to maintain a fixed relationship between a center of the optical image and a center of the light-emitting screen, and so as to tend to maintain a constant scale of the optical image.

23. In a display system according to claim 19, with said beam type image generating means producing a substantial field in the vicinity of the light-emitting screen, and said photosensor means being located remote from said light-emitting screen and being optically coupled with respective individual points at the light emitting screen.

24. In a display system according to claim 23, said photosensor means having respective fiber optic cable means of substantial length coupling said photosensor means with the respective individual points at the respective marginal regions of the light-emitting screen.

25. In a display system according to claim 24, said operating means comprising operational amplifier means having a given open circuit gain, and capacitive coupling means coupling said photosensor means with said operational amplifier means such that said operational amplifier means transmits a signal with substantially said open circuit gain when the photosensor means is activated by the beam.

26. In a display system according to claim 25, said photosensor means comprising PIN diodes having respective first terminals at ground potential and having a common capacitor connecting second terminals thereof with an input of said operational amplifier means.

27. In a display system according to claim 25, with said operational amplifier means having first input means coupled with said photosensor means, and having second input means, and test pulse generator means connected with said second input means of said operational amplifier means for effecting a test activation of said operational amplifier means simulating the activation of said photosensor means.

28. In a display system according to claim 27, said operational amplifier means having means for maintaining said operational amplifier means unresponsive to activation of said photosensor means for so long as a test signal is supplied to said second input means.

43. The aircraft head up display system according to claim 19, wherein said photosensor means is a single photodetector coupled to one individual point in each margin region.

29. In a method for automatically maintaining a desired geometrical relationship between beam deflection commands and the location of a resultant image display on a beam activated display screen in spite of variable influences due to temperature changes, component aging effects, and the like, said method comprising:

establishing reference beam deflection command values for representing respective beam position sensing locations within the range of deflection of the beam,

supplying beam deflection commands causing the beam to trace a resultant image display and to maintain the image display according to real time changes in physical events, and while maintaining said image display without perceptible flicker also causing scanning of the beam in the vicinity of respective beam position sensing locations, by supplying a sequence of plural coordinate commands for effecting deflection of the beam in accordance with a plurality of plural coordinate search patterns, each extending in at least both X and Y directions and only within said beam position sensing locations,

comparing the beam deflection commands actually corresponding to the beam position sensing locations with reference beam deflection command values to obtain beam deflection correction values, and

thereafter modifying the commands in accordance with said beam deflection correction values to substantially maintain the desired geometrical relationship between the resultant image display and the beam deflection commands.

30. In a method according to claim 29, with a display screen having an electrostatic field in the vicinity thereof which would tend to interfere with electronic sensing of the beam at the beam position sensing locations, said method including conducting light pulses produced at the display screen by impingement of the beam at the beam position sensing locations to remotely located photosensor means disposed out of the effective range of the electrostatic field.

31. In a method according to claim 30, said method comprising supplying beam deflection commands maintaining the image display at a central region of the display screen, and conducting light pulses to the photosensor means from beam position sensing locations outside of the central region.

32. In a method according to claim 31, said method comprising conducting light pulses to the photosensor means from not more than four point-like beam position sensing locations at the margin of the display screen.

33. In a method according to claim 31, said method comprising conducting light pulses to the photosensor means from only two point-like beam position sensing locations arranged generally diametrically opposite each other at the margin of the display screen.

34. In a method according to claim 29, said method comprising supplying beam deflection commands to cause scanning of the beam in the vicinity of the respective beam position sensing locations at least every thirty seconds while maintaining the image display without perceptible flicker.

35. In a method according to claim 29, said method comprising

supplying beam deflection commands causing the beam to trace along beam paths of various slopes in a direct stroke generating fashion in producing the image display, and supplying respective sets of beam deflection commands defining respective beam search patterns in the vicinity of the respective beam position sensing locations also in a direct stroke generating fashion.

44. The aircraft head up display system according to claim 29, wherein said beam sensing location has only one photodetector.

36. A method of maintaining a selected scanning relationship between information to be displayed and magnitudes of corresponding beam deflections over a beam activated display screen, said method comprising:

(a) establising at least two beam position sensing locations within the range of deflection of the beam,

(b) causing the beam to produce an image display on the display screen, and also causing the beam to scan the display screen in the vicinity of each of the beam position sensing locations contemporaneously with the production of the image display, and effecting deflection of the beam in accordance with a plural coordinate search pattern in at least both x and Y directions and only within said beam position sensing location for each beam sensing location,

(c) producing a deflection command signal in response to scanning the beam position sensing location,

(d) sensing the magnitude of said deflection command signal required to cause the beam to register with the beam position sensing location, and

(e) correcting subsequent deflection command signals based on the sensed magnitude of step (d) to establish a fixed scanning relationship between the information to be displayed and the resultant magnitudes of corresponding beam deflections.

37. A method according to claim 36, with said method comprising

causing the beam to produce an image display at a central region of the display screen and also causing the beam to scan the display screen at a margin region thereof, the beam position sensing location being in such margin region of the display screen and being reliably offset from the central region, and blocking transmission of light from such margin region of the display screen to a viewer who is observing the image display so that steps (b), (c) and (d) may be carried out while a viewer is observing the image display without being distracted by the beam scanning at the margin region of the display screen.

38. A method according to claim 37, with said method comprising

establishing beam position sensing locations at diametrically opposite margin regions of the display screen,

causing the beam to scan the diametrically opposite margin regions,

sensing the magnitudes of deflection command signals required to cause the beam to register with the respective beam position sensing locations,

and correcting the subsequent deflection command signals so that the image display tends to remain centered with respect to the display screen.

45. The aircraft hed up display system according to claim 36, wherein said beam sensing location has only one photodetector.