EP1907784A1 - Verfahren und vorrichtung zur täuschung infrarot -, radar- als auch dual mode -gelenkter flugkörper - Google Patents
Verfahren und vorrichtung zur täuschung infrarot -, radar- als auch dual mode -gelenkter flugkörperInfo
- Publication number
- EP1907784A1 EP1907784A1 EP06776087A EP06776087A EP1907784A1 EP 1907784 A1 EP1907784 A1 EP 1907784A1 EP 06776087 A EP06776087 A EP 06776087A EP 06776087 A EP06776087 A EP 06776087A EP 1907784 A1 EP1907784 A1 EP 1907784A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- decoys
- decoy
- missile
- chain
- radar
- 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
- 238000000034 method Methods 0.000 title claims abstract description 18
- 230000009977 dual effect Effects 0.000 claims description 6
- 230000000694 effects Effects 0.000 claims description 6
- 239000003380 propellant Substances 0.000 claims description 2
- 238000010304 firing Methods 0.000 abstract description 3
- 238000001514 detection method Methods 0.000 description 2
- 235000015842 Hesperis Nutrition 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000010287 polarization Effects 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
- F41J2/00—Reflecting targets, e.g. radar-reflector targets; Active targets transmitting electromagnetic or acoustic waves
- F41J2/02—Active targets transmitting infrared radiation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/66—Chain-shot, i.e. the submissiles being interconnected by chains or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/70—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies for dispensing radar chaff or infrared material
Definitions
- Infrared, radar and dual mode guided missiles may become a. used for example to combat sea targets, such as ships, or other objects on land and air. After launch, these missiles or rockets initially fly inertially (eg DE 196 01 165 A1) or GPS steered into the target area. The missile then goes into a search phase (search phase) when it has approached the target accordingly. In addition, a missile turns on the target (lock-on) and pursues this until the impact (track phase).
- a "track gate" depth D is about 150 m for older missiles, and only a few meters for modern aircraft.
- decoys are used to prevent the protection of objects missiles by disturbance in / at their function.
- Some decoys emit electromagnetic noise signals (DE 100 16 781 C2) upon detection of a threat, others build up "clouds" of floating dipoles (chaff clouds), which are tuned to the radar frequency of the missile.
- Variants of these floating dipoles are, for example, (radar) confusion decoys, (radar) seduction decoys or (radar) distraction decoys.
- a Confusion decoy is usually deployed at a great distance between the object to be protected (ship) and the attacker before the attack of the missile. Through a variety of these decoys is achieved that the enemy's enlightenment is confused, since in addition to the actual object other goals are generated.
- a seduction decoy is deployed to the target in a missile attack after the missile is "detonated.” For example, to achieve a missile deflection, these decoys have a higher radar beam cross section than the object itself Decoys are brought into action within a "track gate", in order to unfold their effect there.
- Distraction bodies are detected early in a missile attack, in any case before the "lock-on" activated.
- the distance from the object must be greater than the "track gate” of the missile, thereby ensuring that the missile first receives the decoy as its target on its way to the object.
- the use of dipole and flare compounds in a certain ratio ensures that the dipoles are swirled by the flares being burned off.
- the masses are fired in submunitions so that the setting of the delay times of the decomposition or blowing out at a distance of about 10 m to 60 m from the launcher, so that the effective masses within the reduced viewing window of Zielsuchkmü come into effect.
- a corresponding decoy is disclosed in DE 199 51 767 C2.
- Other IR and / or radar reflecting masses etc. are u. a. listed in the prior art of DE 102 30 939 A1.
- the invention has the object of demonstrating a method and a device for deceiving guided missiles, with which a successful distraction is also made possible by modern infrared, radar and dual mode-guided missile.
- the problem is solved by the features of claim 1 and 8.
- Advantageous embodiments are contained in the subclaims.
- the invention is based on the idea of creating a distraction illusion even by modern infrared, radar and dual mode-guided missiles by generating a decoy chain.
- the chain is formed by several, successively connected decoys, for example, by firing individual Chaff submunitions.
- the application occurs before or during the search phase of the missile and can be done, for example, in the reverse walk-off principle or simultaneously or succedan and in the form of a pattern. It is ensured that the decoys with the largest set distance range from the target are the first ones to act.
- the deception chain thus created causes the missile to perform a series of time-consuming analyzes on its way to the target, with the false analyzes typically taking approximately 2 to 4 seconds each. By this measure, the method for directing opposing seekers to false targets is already optimized in the search phase before the "lock-on".
- the effectiveness of the chain is determined by its correct training, which can be defined by the parameters application direction, effective distance, number of decoys, time of effective deployment and / or the radar return cross section.
- the number of decoys expands the reaction or analysis time of the missile. Therefore, the number should be as large as possible, in practice, a number of 5 decoys has been found to be sufficient.
- the device for implementing this method can be realized with known decoy systems / carriers. However, in contrast to these known systems u. a. all submunitions 100% filled with chaff or the like.
- FIG. 1 shows a distraction ammunition 1, in this case with a plurality of radar submunitions 2 (2.1-2.5), which serves to protect an object 3, which is also shown in FIG. 2, against a missile 4 that is radar-steered, for example.
- the radar submunitions 2 are 100% filled with chaff.
- the application direction is also important for the effectiveness of a decoy chain 20 thus created. It is envisaged to deploy the decoy chain 20 through the ammunition 1 in the direction of the missile 4 (line of sight) or in the opposite direction after the search phase of the missile 4. If the search process of the missile 4 is unknown, a simultaneous application in both directions is recommended. In order to prevent two (dummy) targets from being located in the "track gate” of the missile 4 at the same time, a minimum distance from object 3 (ship) as well as from one another to greater D must be maintained.
- the time of the active development of the individual decoys 2.1 - 2.5 is governed by the fact that the decoys 2.1 to 2.5 of the decoy chain 20 should be effective at an early stage. It is preferred that the decoys 2.1 - 2.5 are still used preventively in the search phase of the missile 4.
- the Radarschreibstrahlquerrough the individual decoys 2.1 to 2.5 can be kept relatively low, that is, much smaller than the Radarschreibstrahlquerrough the object 3, and must be only above the Aufschaltschwelle the missile 4.
- a return flow cross section of approx. 500 sqm is usually sufficient.
- the decoy chain 20 may be integrated in a known decoy system, here in the 130 mm ammunition 1.
- the decoys 2.1- 2.5 are released, which can be done simultaneously and with a time delay.
- the decoy 2.1 unfolds preferably but not necessarily first as its effect at about 250 m, the decoy 2.2 as the second at 200 m to the decoy 2.5, which in turn unfolds its last effect at about 50 m, ie they are in turn effective.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102005035251A DE102005035251A1 (de) | 2005-07-25 | 2005-07-25 | Verfahren und Vorrichtung zur Täuschung infrarot-, radar- als auch Dual Mode- gelenkter Flugkörper |
PCT/EP2006/006223 WO2007012371A1 (de) | 2005-07-25 | 2006-06-28 | Verfahren und vorrichtung zur täuschung infrarot -, radar- als auch dual mode -gelenkter flugkörper |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1907784A1 true EP1907784A1 (de) | 2008-04-09 |
EP1907784B1 EP1907784B1 (de) | 2012-10-24 |
Family
ID=37153682
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP06776087A Expired - Fee Related EP1907784B1 (de) | 2005-07-25 | 2006-06-28 | Verfahren und Vorrichtung zur Täuschung Infrarot -, Radar- als auch dual mode -gelenkter Flugkörper |
Country Status (6)
Country | Link |
---|---|
US (1) | US8223061B2 (de) |
EP (1) | EP1907784B1 (de) |
DE (1) | DE102005035251A1 (de) |
DK (1) | DK1907784T3 (de) |
IL (1) | IL189028A (de) |
WO (1) | WO2007012371A1 (de) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102007013676A1 (de) | 2007-03-19 | 2008-09-25 | Oerlikon Contraves Ag | Schutzvorrichtung für ein Lager oder dergleichen mit wenigstens einem zu schützenden Objekt und/oder Personen |
DE102008017725A1 (de) | 2008-04-07 | 2009-10-08 | Rheinmetall Waffe Munition Gmbh | Scheinziel mit einfacher Sicherheitsvorrichtung |
DE102008017722A1 (de) | 2008-04-07 | 2009-10-08 | Rheinmetall Waffe Munition Gmbh | Wirkmassenbehälter |
US8604965B2 (en) * | 2010-02-26 | 2013-12-10 | Federal Aviation Administration/Department of Transportation | Apparatus and method to generate and detect virtual targets |
DE102010032458A1 (de) | 2010-06-11 | 2011-12-15 | Rheinmetall Waffe Munition Gmbh | Aktive Täuschkörper gegen Radarquellen sowie Verfahren zum Schutz von Objekten mit Hilfe derartiger Täuschkörper |
DE102010047860A1 (de) | 2010-10-07 | 2012-04-12 | Rheinmetall Waffe Munition Gmbh | Täuschkörper zum Schutz von Objekten |
DE102011120929A1 (de) | 2011-12-14 | 2013-06-20 | Rheinmetall Waffe Munition Gmbh | Schutzsystem, insbesondere für Schiffe, gegen radargelenkte Bedrohungen |
DE102016121698A1 (de) | 2016-11-11 | 2018-05-17 | Rheinmetall Waffe Munition Gmbh | Verfahren und Abwehrsystem zur Bekämpfung von Zielen und Bedrohungen |
DE102019117801A1 (de) | 2019-07-02 | 2021-01-07 | Rheinmetall Waffe Munition Gmbh | Scheinziel, System und Verfahren zum Schützen eines Objekts |
Family Cites Families (36)
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BE457723A (de) * | ||||
US3068472A (en) * | 1959-06-08 | 1962-12-11 | Aria Paul S Dell | Method of blowing radar-reflective dipoles astern of a moving seagoing ship |
US4149166A (en) * | 1961-05-09 | 1979-04-10 | The United States Of America As Represented By The Secretary Of The Air Force | Doppler countermeasure device |
US3150848A (en) * | 1961-06-28 | 1964-09-29 | Samuel E Lager | Method of decoying a missile from its intended target |
DE977574C (de) * | 1962-02-21 | 1967-04-06 | Messerschmitt A G | Abfangantenne |
US4307665A (en) * | 1965-12-21 | 1981-12-29 | General Dynamics Corporation | Decoy rounds |
FR2383419A1 (fr) | 1977-03-07 | 1978-10-06 | Lacroix E | Valise lance-leurres pour la deception des systemes de guidage d'armes |
US4233605A (en) * | 1979-02-15 | 1980-11-11 | Northrop Corporation | Helicopter radar decoy |
FR2521716B1 (fr) | 1982-02-17 | 1987-01-02 | Lacroix E Tous Artifices | Cartouche lance-leurres electromagnetiques a charges multiples |
GB2138546A (en) * | 1982-09-03 | 1984-10-24 | Wallop Ind Ltd | Decoy systems |
DE3421734A1 (de) * | 1984-06-12 | 1985-12-12 | Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen | Verfahren zum schutz von infrarot-strahlenden zielen, insbesondere von schiffen, vor mit infrarot-lenksuchkoepfen ausgeruesteten flugkoerpern |
US4852455A (en) * | 1987-01-12 | 1989-08-01 | Southwest Aerospace Corporation | Decoy system |
US4808999A (en) * | 1988-02-18 | 1989-02-28 | Loral Corp. | Towed decoy with fiber optic link |
FR2692032B1 (fr) * | 1992-06-05 | 1994-07-22 | Poudres & Explosifs Ste Nale | Cartouches pyrotechniques a plusieurs logements, et munitions correspondantes. |
US6324955B1 (en) * | 1992-04-20 | 2001-12-04 | Raytheon Company | Explosive countermeasure device |
GB2266285B (en) * | 1992-04-25 | 1995-11-29 | British Aerospace | Towed aerodynamic bodies |
US5400690A (en) * | 1992-06-05 | 1995-03-28 | Societe Nationale Des Poudres Et Explosifs | Multi-receptacle pyrotechnic cartridges and corresponding ammunition |
US5249527A (en) * | 1992-07-01 | 1993-10-05 | Westinghouse Electric Corp. | High speed, inflating bag infrared countermeasure |
US5452640A (en) * | 1993-05-06 | 1995-09-26 | Fmc Corporation | Multipurpose launcher and controls |
US5497156A (en) * | 1994-04-15 | 1996-03-05 | Lockheed Corporation | Towed target |
DE4437729C1 (de) * | 1994-10-21 | 1996-04-25 | Buck Chem Tech Werke | Verfahren zum Schützen von eine IR-Strahlung abgebenden Objekten, insbesondere Schiffen, gegen Flugkörper |
DE19543489C1 (de) * | 1995-11-22 | 1997-06-26 | Buck Chem Tech Werke | Schutzeinrichtung für sich rasch bewegende Objekte |
DE19601165A1 (de) | 1996-01-15 | 1997-07-17 | Bodenseewerk Geraetetech | Täuschkörper zum Ablenken von zielsuchenden Lenkflugkörpern |
DE19617701C2 (de) | 1996-05-03 | 2000-01-13 | Buck Werke Gmbh & Co I K | Verfahren zum Bereitstellen eines Scheinziels |
US5814754A (en) * | 1997-01-09 | 1998-09-29 | Foster-Miller, Inc. | False target deployment system |
US5786786A (en) * | 1997-03-17 | 1998-07-28 | Raytheon Company | Photonic radar decoy |
SE520836C3 (sv) * | 1998-11-18 | 2003-10-01 | Saab Ab | Repeterstörsändare samt hylsarrangemang för densamma |
DE19951767C2 (de) | 1999-10-27 | 2002-06-27 | Buck Neue Technologien Gmbh | Dual-Mode-Täuschkörper |
GB9928220D0 (en) * | 1999-11-30 | 2000-05-24 | Roke Manor Research | Autonomous off-board defensive aids system |
DE10016781C2 (de) | 2000-04-05 | 2003-07-03 | Eads Deutschland Gmbh | Schutzvorrichtung |
DE10102599A1 (de) | 2001-01-20 | 2002-08-14 | Comet Gmbh Pyrotechnik Appbau | Düppel |
US6804495B2 (en) * | 2001-10-05 | 2004-10-12 | Northrop Grumman Corporation | Wireless communicator link from towed/surrogate decoy transmitter to the host aircraft |
US6662700B2 (en) * | 2002-05-03 | 2003-12-16 | Raytheon Company | Method for protecting an aircraft against a threat that utilizes an infrared sensor |
DE10230939A1 (de) | 2002-07-09 | 2004-02-12 | Buck Neue Technologien Gmbh | Verfahren und Vorrichtung zum Schutz von Gefechtsfeldfahrzeugen |
US8066218B2 (en) * | 2003-06-13 | 2011-11-29 | Bae Systems Information And Electronic Systems Integration Inc. | Anti-missile defense suite |
US7028947B2 (en) * | 2004-04-30 | 2006-04-18 | Mlho, Inc. | Self-powered tethered decoy for heat-seeking transport aircraft missile defense |
-
2005
- 2005-07-25 DE DE102005035251A patent/DE102005035251A1/de not_active Withdrawn
-
2006
- 2006-06-28 EP EP06776087A patent/EP1907784B1/de not_active Expired - Fee Related
- 2006-06-28 US US11/988,824 patent/US8223061B2/en not_active Expired - Fee Related
- 2006-06-28 DK DK06776087.6T patent/DK1907784T3/da active
- 2006-06-28 WO PCT/EP2006/006223 patent/WO2007012371A1/de active Application Filing
-
2008
- 2008-01-24 IL IL189028A patent/IL189028A/en not_active IP Right Cessation
Non-Patent Citations (1)
Title |
---|
See references of WO2007012371A1 * |
Also Published As
Publication number | Publication date |
---|---|
EP1907784B1 (de) | 2012-10-24 |
US8223061B2 (en) | 2012-07-17 |
DK1907784T3 (da) | 2013-02-04 |
US20090251353A1 (en) | 2009-10-08 |
WO2007012371A1 (de) | 2007-02-01 |
IL189028A0 (en) | 2008-08-07 |
IL189028A (en) | 2015-06-30 |
DE102005035251A1 (de) | 2007-02-01 |
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