EP2176618A2 - Visier - Google Patents
VisierInfo
- Publication number
- EP2176618A2 EP2176618A2 EP08801073A EP08801073A EP2176618A2 EP 2176618 A2 EP2176618 A2 EP 2176618A2 EP 08801073 A EP08801073 A EP 08801073A EP 08801073 A EP08801073 A EP 08801073A EP 2176618 A2 EP2176618 A2 EP 2176618A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- visor
- visor according
- combiner
- optical
- sensors
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
- 230000003287 optical effect Effects 0.000 claims description 19
- 238000001228 spectrum Methods 0.000 claims description 5
- 238000005286 illumination Methods 0.000 claims description 4
- 238000001514 detection method Methods 0.000 claims 1
- 230000003595 spectral effect Effects 0.000 description 7
- 238000001931 thermography Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- NIOPZPCMRQGZCE-WEVVVXLNSA-N 2,4-dinitro-6-(octan-2-yl)phenyl (E)-but-2-enoate Chemical compound CCCCCCC(C)C1=CC([N+]([O-])=O)=CC([N+]([O-])=O)=C1OC(=O)\C=C\C NIOPZPCMRQGZCE-WEVVVXLNSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/32—Devices for testing or checking
- F41G3/326—Devices for testing or checking for checking the angle between the axis of the gun sighting device and an auxiliary measuring device
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/14—Indirect aiming means
- F41G3/16—Sighting devices adapted for indirect laying of fire
- F41G3/165—Sighting devices adapted for indirect laying of fire using a TV-monitor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
- F41G7/30—Command link guidance systems
- F41G7/301—Details
- F41G7/303—Sighting or tracking devices especially provided for simultaneous observation of the target and of the missile
Definitions
- the innovation relates to a visor comprising a plurality of optical devices whose optical axes are basically aligned parallel to each other.
- a visor is used to control a missile from launch to finish.
- the visor next to an optical sensor, such as a telescope, a sensor for detecting the position of the missile.
- a visor can also be a
- Thermal imaging device can be provided with the support of the shooter can target the target even in the dark and without the use of lighting.
- a TV camera may be located in the visor.
- a disadvantage of the proposed structure of the visor that at least one sensor must look through at least one beam splitter to the scene and at least one other sensor looks over the back of at least one beam splitter in the scene.
- a beam splitter used in this way usually leads to restrictions with regard to the usable spectrum for the sensors.
- at least one triple mirror for reversing the direction of a beam path is required.
- the entire structure is too bulky for a modern compact visor due to the large number of optical components required. It is therefore an object of the invention to find an arrangement of sensors in a compact visor, which allows a mounting this arrangement in a compact visor while maintaining a non-alignment Achsharmonistechnik all sensors and while avoiding the aforementioned disadvantages.
- the object is achieved with the help of the proposed innovation in that the directional mark generated by a Richtmarkenprocessor is reflected by a combiner in the leading from the scene to the optical devices beam path and leading from the scene to the optical devices beam path after passing through the combiner with the help of a beam splitter or mirror or direct to the optical devices.
- the term "combiner” is understood to mean a specular disk that is translucent and broad in a large spectral range, as used in head-up displays, among others.
- the combiner used instead permits the passage of all spectral ranges relevant to the sensors in the direction of the scene. At the same time, a slight residual reflection of the combiner is sufficient to superimpose the directional mark on the scene image in sufficient intensity for the sensors.
- the center is recessed and contains a small opening, which is illuminated from the back.
- the illumination is advantageously in the form of pulses.
- FIG. 2 shows a side view of an open visor with a corresponding sensor arrangement.
- the reference numeral 1 indicates the remote scene with the destination.
- the coaxial beam path 8 with the image of this scene is guided in the visor via a combiner 2, two beam splitters 3a and 3b and a mirror 4a.
- the signals relevant for the individual sensors 5a, 5b, 5c are coupled out and supplied to them.
- a direction mark 7 generated in the image plane of the aiming mark projector 6 in the direction of the sensors 5a, 5b, 5c is mirrored in by means of the combiner 2. Only one level mark 7 is illuminated in all required spectral ranges in which the existing sensors work.
- the simplest illumination source for the spectral range from visible light to the infrared range is a light bulb. With regard to the intensity of the radiation, other light sources, such as an LED, are more favorable.
- the leveling mark is generated in the image plane 7 of the Richtmarke Sciencesors. Due to the reflection in the beam path 8, it is inevitably in all Sensors exactly at the same point in the image of the scene 1. Even with a possible drift of the adjustment of the sensors with each other over the operating time, the level indicator in all sensors (5a, 5b, 5c) remains in the same place in the scene.
- the sensors do not necessarily have to be arranged vertically around the central beam splitter, as is the case with known embodiments. It is sufficient a coaxial guidance of the beam path using a combiner, which is permeable to all required by the sensors wavelengths of light and reflects the leveling with little residual reflection in the direction of the sensors.
- a slight residual reflection on the combiner is completely sufficient for generating sufficiently bright alignment marks in the sensors, in particular if, for example, a colored LED is used to illuminate the alignment mark in the visible spectral range.
- a low residual reflection is even necessary, since otherwise due to high temperature differences not only the benchmark but also the Richtmarkenschreiborpatented would be seen in the thermal imaging device.
- the sensors also have switchable optics for different field of view sizes.
- the visual field offset usually occurring during a field of view change does not have a negative effect in the case of the arrangement according to the invention. Even in this case, the aiming mark remains in exactly the same position in the scene in all sensors and in all field of view sizes.
- the geometric shape of the leveling mark is freely selectable. If the sensors work in different spectral ranges, the Richtmarkeform by Illumination of different parts of the landmark by different light sources in each sensor look different.
- the sighting mark 7 for the telescope 5c, 5d and the thermal imaging device 5b has the form of a crosshair which is open in the middle so as not to obscure the target and gives the gunner a target size estimate and thus also a distance estimation enable.
- the crosshairs are continuously illuminated for the visible spectral range with a red LED and a few degrees warm source for the thermal imager.
- In the middle of the reticle is an opening, behind which a very small LED is mounted to project a spot on the missile location sensor 5a. This point is illuminated only pulsewise. This is where the missile location sensor detects where the target is in its field of view.
- Such a method has proven to be favorable when a sensor image is evaluated only by image processing.
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200720010552 DE202007010552U1 (de) | 2007-07-28 | 2007-07-28 | Visier |
PCT/DE2008/001235 WO2009015649A2 (de) | 2007-07-28 | 2008-07-26 | Visier |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2176618A2 true EP2176618A2 (de) | 2010-04-21 |
EP2176618B1 EP2176618B1 (de) | 2013-02-13 |
Family
ID=38580529
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08801073A Active EP2176618B1 (de) | 2007-07-28 | 2008-07-26 | Visier |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2176618B1 (de) |
DE (1) | DE202007010552U1 (de) |
WO (1) | WO2009015649A2 (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014001211A1 (de) | 2014-01-30 | 2015-07-30 | Roderich Rüger | Lenkflugkörper-System auf Klein-Helicopter |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102009050163A1 (de) | 2009-10-21 | 2011-04-28 | Lfk-Lenkflugkörpersysteme Gmbh | Optische Einrichtung für ein Visier |
US8117780B2 (en) | 2010-05-24 | 2012-02-21 | Surefire, Llc | Gun sight |
US9010012B2 (en) | 2010-05-24 | 2015-04-21 | Surefire, Llc | Gun sight |
US9057583B2 (en) | 2010-10-28 | 2015-06-16 | Surefire, Llc | Sight system |
US8474173B2 (en) | 2010-10-28 | 2013-07-02 | Surefire, Llc | Sight system |
DE102011118045B4 (de) * | 2011-11-09 | 2015-12-31 | Diehl Bgt Defence Gmbh & Co. Kg | Optisches Erfassungssystem |
DE102014015025B4 (de) | 2014-10-08 | 2018-03-29 | Mbda Deutschland Gmbh | Visieranlage und Verfahren zum Betreiben einer Visieranlage |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3930564A1 (de) * | 1989-09-13 | 1991-03-21 | Messerschmitt Boelkow Blohm | Optronisches visier |
IL107969A (en) * | 1992-12-11 | 1997-04-15 | Hughes Aircraft Co | Common aperture multi- sensor boresight mechanism |
US6396647B1 (en) * | 2000-04-03 | 2002-05-28 | Raytheon Company | Optical system with extended boresight source |
US6765663B2 (en) * | 2002-03-14 | 2004-07-20 | Raytheon Company | Efficient multiple emitter boresight reference source |
-
2007
- 2007-07-28 DE DE200720010552 patent/DE202007010552U1/de not_active Expired - Lifetime
-
2008
- 2008-07-26 EP EP08801073A patent/EP2176618B1/de active Active
- 2008-07-26 WO PCT/DE2008/001235 patent/WO2009015649A2/de active Application Filing
Non-Patent Citations (1)
Title |
---|
See references of WO2009015649A3 * |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014001211A1 (de) | 2014-01-30 | 2015-07-30 | Roderich Rüger | Lenkflugkörper-System auf Klein-Helicopter |
Also Published As
Publication number | Publication date |
---|---|
WO2009015649A3 (de) | 2009-04-02 |
WO2009015649A2 (de) | 2009-02-05 |
DE202007010552U1 (de) | 2007-10-11 |
EP2176618B1 (de) | 2013-02-13 |
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