EP0822383A1 - Missile seeker for use in a jamming environment - Google Patents
Missile seeker for use in a jamming environment Download PDFInfo
- Publication number
- EP0822383A1 EP0822383A1 EP97112411A EP97112411A EP0822383A1 EP 0822383 A1 EP0822383 A1 EP 0822383A1 EP 97112411 A EP97112411 A EP 97112411A EP 97112411 A EP97112411 A EP 97112411A EP 0822383 A1 EP0822383 A1 EP 0822383A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- target
- filter
- interference
- transparent
- missile
- 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.)
- Withdrawn
Links
Images
Classifications
-
- 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
- F41G7/22—Homing guidance systems
- F41G7/2213—Homing guidance systems maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
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- 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
- F41G7/22—Homing guidance systems
- F41G7/224—Deceiving or protecting means
-
- 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
- F41G7/22—Homing guidance systems
- F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
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- 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
- F41G7/22—Homing guidance systems
- F41G7/2273—Homing guidance systems characterised by the type of waves
- F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
Definitions
- Infrared homing heads of all types - such as reticle, scan, or FPA seekers - are affected by targeted malfunctioning, such as lamp or laser interference. This impairment ranges from the output of various incorrect information about the target storage, about the loss of target through glare and saturation effects up to destruction of the detectors.
- the present invention has for its object to demonstrate a method with which it is possible to pursue flawless target tracking despite ensure massive disruption.
- the general idea of the invention is based on the consideration since the mentioned interference systems are always on board the one to be attacked Aim to take advantage of this interference radiation in such a way that it itself is used as a target, roughly similar to that from microwave technology well-known "home-on-jam" process.
- This is now done in the beam path a controllable damping filter is arranged on the IR target seeker head, for example an electrochromic filter.
- This filter is normally transparent, but is open within a short time a selectable through loss can be set as soon as the signal evaluation the homing head detects that there are interference signals or that saturation effects occur due to glare in the detector.
- the passage damping of the filter according to the invention is corresponding the interference radiation is set appropriately, so the target is not provide more signal, but the source of interference itself, which is integrated in the target is, will come to rest in the linear part of the detector characteristic and can therefore be easily tracked and thus the missile into Bring goal.
- Target-typical filing signal is controlled to make the fact To take into account that the meeting point should be where it is on the is most vulnerable and not where the interferer is located.
Abstract
Description
Infrarot-Zielsuchköpfe aller Typen - wie beispielsweise Reticle-, Scan-, oder FPA-Sucher - werden in ihrer Leistungsfähigkeit durch gerichtete Störmaßnahmen, wie Lampen- oder Laserstörer, beeinträchtigt. Diese Beeinträchtigung reicht von der Ausgabe diverser Falschinformationen über die Zielablage, über den Zielverlust durch Blend- und Sättigungseffekte bis hin zur Zerstörung der Detektoren.Infrared homing heads of all types - such as reticle, scan, or FPA seekers - are affected by targeted malfunctioning, such as lamp or laser interference. This impairment ranges from the output of various incorrect information about the target storage, about the loss of target through glare and saturation effects up to destruction of the detectors.
Der vorliegenden Erfindung liegt die Aufgabe zugrunde, ein Verfahren aufzuzeigen, mit dem es ermöglicht wird, eine einwandfreie Zielverfolgung trotz massiver Störung sicherzustellen.The present invention has for its object to demonstrate a method with which it is possible to pursue flawless target tracking despite ensure massive disruption.
Diese Aufgabe wird in überraschender Weise durch die im Anspruch 1 aufgezeigten Maßnahmen gelöst. In den Unteransprüchen sind Ausgestaltungen und Weiterbildungen angegeben und in der nachfolgenden Beschreibung ist ein Ausführungsbeispiel erläutert, das in der einzigen Figur der Zeichnung skizziert ist, die einen IR-Suchkopf in schematischer Darstellung zeigt, der gemäß der Erfindung ausgestaltet ist.This object is surprisingly demonstrated by those in claim 1 Measures solved. Refinements are in the subclaims and further developments are given and in the description below an embodiment explained in the single figure of the drawing is sketched, which shows an IR seeker head in a schematic representation is designed according to the invention.
Dem allgemeinen Erfindungsgedanken liegt nun die Überlegung zugrunde, da sich die genannten Störsysteme ja immer an Bord des anzugreifenden Zieles befinden, diese Störstrahlung nun in der Weise auszunutzen, daß sie selbst als Ziel herangezogen wird, ungefähr ähnlich dem aus der Mikrowellentechnik bekannten "Home-on-Jam"-Verfahren. Hierzu wird nun im Strahlengang des IR-Zielsuchkopfes ein steuerbares Dämpfungsfilter angeordnet, beispielsweise ein elektrochromes Filter.The general idea of the invention is based on the consideration since the mentioned interference systems are always on board the one to be attacked Aim to take advantage of this interference radiation in such a way that it itself is used as a target, roughly similar to that from microwave technology well-known "home-on-jam" process. This is now done in the beam path a controllable damping filter is arranged on the IR target seeker head, for example an electrochromic filter.
Dieses Filter ist im Normalfall transparent, ist aber innerhalb kurzer Zeit auf eine wählbare Durchgangsdämpfung einstellbar, sobald die Signalauswertung des Zielsuchkopfes erkennt, daß Störsignale vorhanden sind oder daß Sättigungseffekte infolge Blendung im Detektor auftreten.This filter is normally transparent, but is open within a short time a selectable through loss can be set as soon as the signal evaluation the homing head detects that there are interference signals or that saturation effects occur due to glare in the detector.
Wird die Durchgangsdämpffing des erfindungsgemäßen Filters entsprechend der Störstrahlung geeignet eingestellt, so wird zwar das angepeilte Ziel nicht mehr genügend Signal liefern, aber die Störquelle selbst, die ja im Ziel integriert ist, wird in dem linearen Teil der Detektorkennlinie zu liegen kommen und kann daher problemlos verfolgt werden und damit den Flugkörper ins Ziel bringen. If the passage damping of the filter according to the invention is corresponding the interference radiation is set appropriately, so the target is not provide more signal, but the source of interference itself, which is integrated in the target is, will come to rest in the linear part of the detector characteristic and can therefore be easily tracked and thus the missile into Bring goal.
In einer Weiterbildung ist vorgesehen, daß der Endanflug mit einem zusätzlichen zieltypischen Ablagesignal gesteuert wird, um damit der Tatsache Rechnung zu tragen, daß der Treffpunkt dort am Ziel liegen sollte, wo es am meisten verwundbar ist und nicht dort, wo der Störer angebracht ist.In a further development it is provided that the final approach with an additional Target-typical filing signal is controlled to make the fact To take into account that the meeting point should be where it is on the is most vulnerable and not where the interferer is located.
Claims (3)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19631435 | 1996-08-03 | ||
DE1996131435 DE19631435C1 (en) | 1996-08-03 | 1996-08-03 | Procedures for tracking failures |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0822383A1 true EP0822383A1 (en) | 1998-02-04 |
Family
ID=7801732
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97112411A Withdrawn EP0822383A1 (en) | 1996-08-03 | 1997-07-19 | Missile seeker for use in a jamming environment |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0822383A1 (en) |
DE (1) | DE19631435C1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2407745A1 (en) * | 2010-07-15 | 2012-01-18 | LFK-Lenkflugkörpersysteme GmbH | Seeker for a missile |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102013014192B4 (en) * | 2013-08-24 | 2022-05-12 | Diehl Defence Gmbh & Co. Kg | Method of protecting a protected object |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4531814A (en) * | 1981-10-29 | 1985-07-30 | Carl-Zeiss-Stiftung | Method and apparatus for temporarily increasing the absorptance of optical transmitting components |
US4554587A (en) * | 1982-02-22 | 1985-11-19 | Tokyo Shibaura Denki Kabushiki Kaisha | Image pickup apparatus |
US4843235A (en) * | 1973-02-23 | 1989-06-27 | United States Of America As Represented By The Secretary Of The Navy | Devices for protection of sensors from damaging and interrogating radiation |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3141524C1 (en) * | 1981-10-20 | 1983-02-24 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Method and device for filtering out interfering emitters in a device for optical guidance of missiles |
DE3923489A1 (en) * | 1989-07-15 | 1991-01-24 | Messerschmitt Boelkow Blohm | location imaging and missile guiding device - has receiver with several image sensors, operated in time parallel and liq. crystal allocated to respective sensor |
-
1996
- 1996-08-03 DE DE1996131435 patent/DE19631435C1/en not_active Expired - Fee Related
-
1997
- 1997-07-19 EP EP97112411A patent/EP0822383A1/en not_active Withdrawn
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4843235A (en) * | 1973-02-23 | 1989-06-27 | United States Of America As Represented By The Secretary Of The Navy | Devices for protection of sensors from damaging and interrogating radiation |
US4531814A (en) * | 1981-10-29 | 1985-07-30 | Carl-Zeiss-Stiftung | Method and apparatus for temporarily increasing the absorptance of optical transmitting components |
US4554587A (en) * | 1982-02-22 | 1985-11-19 | Tokyo Shibaura Denki Kabushiki Kaisha | Image pickup apparatus |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2407745A1 (en) * | 2010-07-15 | 2012-01-18 | LFK-Lenkflugkörpersysteme GmbH | Seeker for a missile |
Also Published As
Publication number | Publication date |
---|---|
DE19631435C1 (en) | 1998-03-12 |
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