IL113971A - Day/night heads-up display (hud) - Google Patents

Day/night heads-up display (hud)

Info

Publication number
IL113971A
IL113971A IL113971A IL11397195A IL113971A IL 113971 A IL113971 A IL 113971A IL 113971 A IL113971 A IL 113971A IL 11397195 A IL11397195 A IL 11397195A IL 113971 A IL113971 A IL 113971A
Authority
IL
Israel
Prior art keywords
light
rotating mirror
pilot
light sources
symbol generator
Prior art date
Application number
IL113971A
Other versions
IL113971A0 (en
Original Assignee
Honeywell Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell Inc filed Critical Honeywell Inc
Publication of IL113971A0 publication Critical patent/IL113971A0/en
Publication of IL113971A publication Critical patent/IL113971A/en

Links

Classifications

    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01Head-up displays
    • G02B27/017Head mounted
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01Head-up displays
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01Head-up displays
    • G02B27/0101Head-up displays characterised by optical features
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N5/00Details of television systems
    • H04N5/74Projection arrangements for image reproduction, e.g. using eidophor
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01Head-up displays
    • G02B27/0101Head-up displays characterised by optical features
    • G02B2027/0138Head-up displays characterised by optical features comprising image capture systems, e.g. camera
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01Head-up displays
    • G02B27/0101Head-up displays characterised by optical features
    • G02B2027/014Head-up displays characterised by optical features comprising information/image processing systems
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B27/00Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
    • G02B27/01Head-up displays
    • G02B27/0149Head-up displays characterised by mechanical features
    • G02B2027/0154Head-up displays characterised by mechanical features with movable elements
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N5/00Details of television systems
    • H04N5/74Projection arrangements for image reproduction, e.g. using eidophor
    • H04N5/7408Direct viewing projectors, e.g. an image displayed on a video CRT or LCD display being projected on a screen
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04NPICTORIAL COMMUNICATION, e.g. TELEVISION
    • H04N5/00Details of television systems
    • H04N5/74Projection arrangements for image reproduction, e.g. using eidophor
    • H04N5/7475Constructional details of television projection apparatus
    • H04N5/7491Constructional details of television projection apparatus of head mounted projectors

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Engineering & Computer Science (AREA)
  • Multimedia (AREA)
  • Signal Processing (AREA)
  • Devices For Indicating Variable Information By Combining Individual Elements (AREA)
  • Instrument Panels (AREA)

Description

DAY/NIGHT HEADS-UP DISPLAY (HUD) DAY/NIGHT HE ADS-UP DISPLAY (HUD) BACKGROUND OF THE INVENTION Field of the Invention (Technical Field! The invention relates to visual display, and more particularly to a heads-up display apparatus and method for projecting a display of flight or weapons information to a pilot.
Background Art Since man has flown aircraft, there has been a continual search to keep a pilot informed as to flight display information in addition to keeping his eyes on the flight path. In the early years, these two requirements were diametrically opposing. In recent times, head mounted displays and displays superimposed upon objects in the pilot's line of sight have proliferated.
Many of the display systems use cathode-ray tube (CRT) construction attached to a helmet, or mirrored to a screen or similar device, for heads-up viewing by a pilot. Other known devices teach the use of fiber optic cables for carrying CRT images to a similar viewing device. However, CRT devices have many drawbacks, such as their weight and bulk. Additionally, CRT systems are very expensive. Some of these prior art systems are described below.
U.S. Patent No. Re. 28,847 to Vizenor refers to a light emitting source, but describes no other source than a low light level television (TV) system which is a CRT device. The disclosed device is for superimposing an image on a helmet or helmet mounted device. There is no disclosure of a means for creating a display.
U.S. Patent No. 3,945,716 to Kinder teaches a CRT display apparatus and a fiber optic cable for transmission of an image onto a holographic lens. The device is affixed on a pivoting arm above a pilot's head.
U.S. Patent No. 3,940,204 to Withrington describes another CRT system in conjunction with a holographic lens.
U.S. Patent No. 4,269,476 to Gauthier et al., discloses a helmet mounted display system utilizing a CRT and a spherical mirror.
U.S. Patent No. 3,833,300 to Rymes describes an aiming system for projectiles using a CRT, fiber optic bundles and a visor in the form of two parabolas.
Some prior art devices use driven light emitting diodes (LEDs) to generate a two-dimensional display. The display system developed under U.S. Patent No. 4,311,999 to Upton et al., uses a clamped cantilevered array of vibrating fiber optic filaments to create the two-dimensional display. The array of fiber optic filaments is prone to fracture and has limitations to image quality and resolution.
U.S. Patent No. 3,958,235 to Duffy discloses a system similar to Upton et al., except reeds are used instead of fiber optic cables.
The device developed by Private Eye™ uses a flat vibrating mirror to create the display. The display image is not see-through and the image generator obstructs the user's eyesight.
SUMMARY OF THE INVENTION In accordance with the present invention, there is disclosed a raster-type display apparatus and method whereby an image is created by a plurality of light sources energized in cooperation with a rotating mirror. The preferred apparatus for displaying an image comprises a plurality of light sources, a rotating mirror for receiving light from the light sources and reflecting the light, a symbol generator for synchronously energizing the light sources, a feedback structure for monitoring a rotation state of the rotating mirror and reporting the rotation state to a control of the symbol generator, and structure for projecting the reflected light from the rotating mirror onto a surface.
The preferred plurality of light sources comprises light emitting diodes.
The preferred rotating mirror comprises a polygon. An alternative polygon rotating mirror comprises angled facets. The rotating mirror can also comprise a multifaceted sphere.
The preferred feedback structure comprises a light emitter and light detector. An alternative feedback structure comprises electro-magnetic feedback from a motor for rotating the rotating mirror.
The preferred symbol generator comprises structure for controlling a speed of rotation of the rotating mirror.
The preferred structure for projecting the reflected light comprises a collimating lens.
The preferred surface comprises a surface that displays the reflected light and also allows ambient light to pass through. The preferred surface comprises a combiner element.
The preferred method for displaying an image comprises the steps of providing a plurality of light sources, providing a mirror for receiving light from the light sources and reflecting the light, rotating the mirror, synchronously energizing the light sources from a symbol generator, monitoring a rotation state of the rotating mirror and reporting the rotation state to a control of the symbol generator, and projecting the reflected light from the rotating mirror onto a surface.
The preferred step of providing a plurality of light sources comprises providing light emitting diodes.
The preferred step of providing a mirror comprises providing a polygon. The step of providing a mirror alternatively comprises providing angled facets. The step of providing a mirror can also comprise providing a multifaceted sphere.
The preferred step of monitoring a rotation state of the rotating mirror and reporting the rotation state to a control of the symbol generator comprises providing a light emitter and light detector. The step of monitoring a rotation state of the rotating mirror and reporting the rotation state to a control of the symbol generator alternatively comprises measuring electro-magnetic signals from a motor for rotating the mirror.
The preferred method further comprises the step of controlling a speed of rotation of the rotating mirror by the symbol generator.
The preferred step of projecting the reflected light comprises collimating the light through a lens. The step of projecting the reflected light also comprises displaying the reflected light on a surface and allowing ambient light to pass through. The preferred surface for displaying comprises a combiner element.
Also disclosed is an apparatus for displaying an image comprising structure for mounting a combiner element in the field of view of an observer, a plurality of light sources in a linear array, a rotating mirror for receiving light from the light sources and reflecting the light at predetermined angles of reflection, a symbol generator for synchronously energizing the light sources, a feedback structure for monitoring a rotation state of the rotating mirror and reporting the rotation state to a control of the symbol generator, and structure for projecting the reflected light from the rotating mirror through a collimated lens and onto the combiner element.
The preferred structure for mounting a combiner element comprises affixing the combiner element to a helmet. The structure for mounting the combiner element comprises affixing the combiner element to night vision goggles.
Disclosed is an apparatus for displaying an image comprising a combiner element comprising a glass surface coated to enhance reflected light while allowing ambient light to pass through and mounting the combiner element on a helmet, 128 light emitting diodes in a linear array, a rotating polygon mirror for receiving light from the light emitting diodes and reflecting the light at predetermined angles of reflection, a symbol generator for synchronously energizing the light emitting diodes in a selected pattern, a feedback structure comprising a light emitter and light detector for monitoring a rotation state of the rotating polygon mirror and reporting the rotation state to a control of the symbol generator, and a collimating lens for projecting the reflected light from the rotating polygon mirror onto the combiner element.
A primary object of the present invention is to provide a visual display image in the line of sight combined with the background scene.
A primary advantage of the present invention is that it is significantly lighter in weight than CRT based systems.
Another advantage of the present invention is that it does not have a vibrating fiber optic cable that is subject to fracture as in other LED based systems.
Yet another advantage of the present invention is that it is significantly less expensive than CRT based systems.
Other objects, advantages and novel features, and further scope of applicability of the present invention will be set forth in part in the detailed description to follow, taken in conjunction with the accompanying drawings, and in part will become apparent to those skilled in the art upon examination of the following, or may be learned by practice of the invention. The objects and advantages of the invention may be realized and attained by means of the instrumentalities and combinations particularly pointed out in the appended claims.
BRIEF DESCRIPTION OF THE DRAWINGS The accompanying drawings, which are incorporated into and form a part of the specification, illustrate several embodiments of the present invention and, together with the description, serve to explain the principles of the invention. The drawings are only for the purpose of illustrating a preferred embodiment of the invention and are not to be construed as limiting the invention. In the drawings: Fig. 1 schematically illustrates the preferred apparatus and method of the present invention; Fig. 2 illustrates the preferred feedback apparatus; Fig. 3 illustrates the preferred "see through" glass surface; Fig. 4 shows a typical display generated by the invention; Fig. 5 is a perspective view of an alternative embodiment of the rotating mirror; Fig. 6 is another alternative embodiment of the rotating mirror; and Fig. 7 shows the invention mounted on an aviator's helmet.
DESCRIPTION OF THE PREFERRED EMBODIMENTS The heads-up display apparatus and method of the present invention comprise hardware components, providing to a pilot the ability to view information such as navigational data images or weapons data images within the immediate field of view of a pilot. In addition, the apparatus is "see through" so a pilot can see the display image in addition to the background scene.
The preferred display is mounted to the user's head, helmet or other structure in the pilot's line of sight. The preferred apparatus and method are depicted in Fig. 1. The dashed lines in Fig. 1 indicate light paths. The display image is created by an array of visible light sources such as a linear array of light emitting diodes (LEDs) 10. The preferred LED array 10 is mounted to a substrate in a linear fashion. In the preferred embodiment, 128 LEDs are used for LED array 10; however, different numbers of LEDs can be used, as well as different configurations.
Mirror 12 is mounted adjacent to the LED array 10 and is driven by a motor 14, or other device well known in the art. The preferred mirror 12 is polygonal-shaped with each facet at a similar angle. The light from the LEDs is projected onto rotating mirror 12, which is rotating such that the angle of reflection 46 of the light off of the mirror surfaces is continuously changing. The individual LEDs are strobed in a synchronous fashion with respect to the mirror rotation such that a two-dimensional array of pixels is generated. The two-dimensional array of pixels is then collimated through collimating lens 24 and reflected on a glass surface 26 for the creation of a desired image.
The mirror rotation and LED strobe are controlled by display generator 22, comprising a computer or other known symbol generators, which generates video images. The synchronization of rotating mirror 12 and the strobed LEDs is accomplished by a feedback mechanism 16, such as a light emitter/detector. The mirror rotation and LED strobe are controlled by a symbol generator computer 22 which creates a video image. The LED light is reflected into the user's eye 52. The reflecting surface 26 allows light to pass through or around such that the user is able to see beyond the reflecting image superimposed over the background scene as observed by the user. The display light is collimated through a lens 24 to create the appearance of coming from infinity.
The display quality is controlled by the revolutions per minute (RPM) of the motor that rotates polygon mirror 12 cooperatively with the strobing of the LEDs. The preferred RPM is approximately 600 RPM and the preferred strobe rate is approximately 80 Hz.
To coordinate mirror 12 rotation and the strobing of the individual LEDs, mirror 12 rotation is monitored and controlled by a feedback apparatus 16. The preferred feedback apparatus as shown in Fig. 2, is a feedback LED emitter 18 that continuously emits a beam to mirror 12. Light is reflected off mirror 12 onto a light detecting apparatus 20, such as a transistor detector. As mirror 12 rotates, the angle of reflection of the light results in a pulsed signal from the transistor detector 20 and is fed back to symbol generator 22. Symbol generator 22 counts the pulsed detector signal and synchronizes LED array 10 information with the rotation of mirror 12.
Alternative feedback apparatuses 16, such as mechanical counters or electromagnetic feedback from the motor, could also be utilized in a similar fashion.
Individual LEDs from LED array 10 are strobed synchronously by symbol generator 22 that are well known in the art with modifications to accept the feedback signal from feedback apparatus 16. The strobed light from the individual LEDs is reflected off mirror 12 and is collimated by collimating lens 24 and reflected off a glass surface 26 or the like. The preferred glass surface 26 as shown in Fig. 3 is a combiner element 56 which is coated with a selectively reflective optical coating 54. The use of such coatings is well known in the art. The preferred coating material 54 reflects light in the bandwidth of the LEDs to enhance the reflection of the display light while allowing ambient light to pass through. In this embodiment, the user can see the combined display symbology and the background scene.
Alternative embodiments for mirror 12 can also be utilized. The display size can be increased by changing the angle of every other facet of mirror 12 with respect to the drive shaft angle of the motor as shown in Fig. 5. Thus, the reflected light from the strobed LEDs 10, off the angled facets, would create a larger display. The display size is proportional to the angle of the facets. As shown in Fig. 6, another alternative embodiment is for mirror 12 to comprise a spherical surface with multiple facets at predetermined angles to increase the display pattern for a fixed number of LEDs. In these alternative embodiments LED array 10 can consist of fewer individual LEDs. Additionally, different color LEDs can be positioned for reflection on certain facets for color displays. ~ Fig. 4 shows a typical display symbology 28 generated by the preferred embodiment as seen by the pilot.
Fig. 7 illustrates the preferred mounting position of a display unit 30 mounted to an aviator's helmet 32. The display combiner element is positioned such that the display symbology is centered in the user's field of view 34. The display 30 is fastened with an adjustment mechanism 36 to allow positioning for individual preference. The adjustment mechanism 36 can be a ball 40 and socket 42 mounted to an attachment arm 38. The ball 40 is allowed to pivot in the socket 42 until alignment is obtained and then secured with a set screw or the like. The attachment arm 38 can be flexible to allow final adjustment.
The display unit 30 can also be mounted to a night vision imaging system by directing the reflected symbology into the objective lens of the night vision system (not shown).
This invention has been described herein in considerable detail in order to comply with the Patent Statutes and to provide those skilled in the art with the information needed to apply the novel principles and to construct and use such specialized components as are required. However, it is to be understood that the invention is. not restricted to the particular embodiment that has been described and illustrated, but can be carried out by specifically different equipment and devices, and that various modifications, both as to the equipment details and operating procedures, can be accomplished without departing from the scope of the invention itself.
Variations and modifications of the present invention will be obvious to those skilled in the art and it is intended to cover in the appended claims all such modifications and equivalents. The entire disclosures of all references, applications, patents, and publications cited above, and of the corresponding application(s), are hereby incorporated by reference. 113971/2 - 9 -

Claims (16)

CLAIMS The embodiments of the invention in which an exclusive property or right is claimed are defined as follows:
1. An apparatus for displaying an image to a pilot of a vehicle, comprising: a helmet which the pilot wears while operating the vehicle; an image generating apparatus mounted on the pilot's helmet comprising: a plurality of light sources; rotating mirror means for receiving light from said light sources and reflecting said light; symbol generator means for synchronously energizing said light sources which receives image information from remote source; feedback means for monitoring a rotation state of said rotating mirror means and reporting said rotation state to a control of said symbol generator means; and means for projecting said reflected light from said rotating mirror means ; and a reflective surface in the field of vision of the pilot which displays said reflective light to the pilot while allowing the pilot to view outside the vehicle.
2. The invention of claim 1 wherein said plurality of light sources comprises light emitting .diodes. 113971/2 - 10 -
3. The invention of claim 1 wherein said rotating mirror means comprises a polygon.
4. The invention of claim 3 wherein said rotating mirror comprises angled facets .
5. The invention of claim 1 wherein said rotating mirror means comprises a multifaceted sphere.
6. The invention of claim 1 wherein said feedback means comprises a light emitter and light detector means.
7. The invention of claim 1 wherein said feedback means comprises an electromagnetic feedback means from a motor for rotating said rotating mirror means.
8. The invention of claim 1 wherein said symbol generator means comprises a means for controlling a speed of rotation of said rotating mirror means.
9. The invention of claim 1 wherein said means for projecting said reflected light comprises a collimating lens.
10. The invention of claim 1 wherein said reflective surface comprises a surface that displays said reflected light and also allows ambient light to pass through.
11. 1. The invention of claim 1 wherein said reflective surface comprises a combiner element. 113971/2 - 11 -
12. An apparatus for displaying an image to a pilot of a vehicle, comprising: a helmet which the pilot wears while operating the vehicle; means for mounting a combiner element on the helmet in the field of view of an observer; means for generating an image mounted on the pilot's helmet comprising: a plurality of light sources in linear array; rotating mirror means for receiving light from said light sources and reflecting said light at predetermined angles of reflection; symbol generator means for synchronously energizing said light sources, where said symbol generator means receives image information from a remote source; feedback means for monitoring a rotation state of said rotating mirror means and reporting said rotation state to a control of said symbol generator means; and means for projecting said reflected light from said rotating mirror means through a collimated lens and onto said combiner element.
13. The invention of claim 12 wherein said means for mounting said combiner element comprises affixing said combiner element to night vision goggles.
14. The apparatus for displaying an image of claim 12 wherein the plurality of light sources in a linear array comprises 128 light emitting diodes. 113971/2 - 12 -
15. An apparatus in accordance with any of claims 1-14 and substantially as described in conjunction with any of Figs. 1-7.
16. An apparatus in accordance with any of claims 1-14 and substantially as shown in any of Figs. 1-7.
IL113971A 1994-06-02 1995-06-01 Day/night heads-up display (hud) IL113971A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US25271194A 1994-06-02 1994-06-02

Publications (2)

Publication Number Publication Date
IL113971A0 IL113971A0 (en) 1995-10-31
IL113971A true IL113971A (en) 1998-02-08

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ID=22957196

Family Applications (1)

Application Number Title Priority Date Filing Date
IL113971A IL113971A (en) 1994-06-02 1995-06-01 Day/night heads-up display (hud)

Country Status (4)

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EP (1) EP0763217A2 (en)
JP (1) JPH10501348A (en)
IL (1) IL113971A (en)
WO (1) WO1995034014A2 (en)

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US6654158B2 (en) 2001-04-20 2003-11-25 Microvision, Inc. Frequency tunable resonant scanner with auxiliary arms
US7516896B2 (en) 1999-08-05 2009-04-14 Microvision, Inc. Frequency tunable resonant scanner with auxiliary arms
US6882462B2 (en) 2002-11-01 2005-04-19 Microvision, Inc. Resonant scanner with asymmetric mass distribution
US6285489B1 (en) 1999-08-05 2001-09-04 Microvision Inc. Frequency tunable resonant scanner with auxiliary arms
EP1330673B1 (en) * 2000-11-03 2009-07-22 Microvision, Inc. Frequency tunable resonant scanner with auxiliary arms
US20020120916A1 (en) * 2001-01-16 2002-08-29 Snider Albert Monroe Head-up display system utilizing fluorescent material
KR101220894B1 (en) * 2004-02-04 2013-01-11 마이크로비젼, 인코퍼레이티드 Scanned-beam heads-up display and related systems and methods
JP2006276078A (en) * 2005-03-28 2006-10-12 Calsonic Kansei Corp Display device for vehicle
EP1889112B1 (en) 2005-05-25 2009-07-22 Koninklijke Philips Electronics N.V. Device for projecting a pixelated lighting pattern
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RU2531766C2 (en) * 2012-11-23 2014-10-27 Открытое акционерное общество "Российская самолетостроительная корпорация "МиГ" (ОАО "РСК "МиГ") Method to assess image of collimator aviation indicator and diaphragm for its realisation
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Also Published As

Publication number Publication date
WO1995034014A2 (en) 1995-12-14
WO1995034014A3 (en) 1996-01-25
JPH10501348A (en) 1998-02-03
EP0763217A2 (en) 1997-03-19
IL113971A0 (en) 1995-10-31

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