EP0777100B1 - Système d'arme missile - Google Patents
Système d'arme missile Download PDFInfo
- Publication number
- EP0777100B1 EP0777100B1 EP96119417A EP96119417A EP0777100B1 EP 0777100 B1 EP0777100 B1 EP 0777100B1 EP 96119417 A EP96119417 A EP 96119417A EP 96119417 A EP96119417 A EP 96119417A EP 0777100 B1 EP0777100 B1 EP 0777100B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- target
- head
- homing
- image
- correlation
- 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.)
- Expired - Lifetime
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
- F41G7/2273—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
-
- 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
- F41G7/2206—Homing guidance systems using a remote control station
-
- 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
-
- 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
- F41G7/2226—Homing guidance systems comparing the observed data with stored target data, e.g. target configuration data
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Telescopes (AREA)
Claims (1)
- Système missile comportant une tête chercheuse de cible suspendue par une liaison à cardan et un processeur d'alignement (processeur de poursuite) qui compare l'image de visée et l'image de la tête chercheuse mises en concordance, en appliquant un procédé de corrélation, de manière continue, pour déterminer son objectif,
caractérisé en ce quea) le cadre de marquage de l'objectif est introduit dans l'image de visée pour réduire l'influence du parallaxe sur la corrélation en réduisant ou en augmentant la taille de l'objectif, par adaptation, et en introduisant les grandeurs choisies de l'optique de la tête chercheuse,b) la tête chercheuse de cibles est équipée d'un objectif zoom adapté à la portée du système d'armement qui réduit le champ de visée dans la mesure où la cible est représentée avec chevauchement pour tous les éloignements de cibles, toujours pratiquement de manière à remplir l'image,c) le niveau des vibrations influençant la tête chercheuse de cibles ou son optique zoom, peut être éliminé dans une très large mesure par la mise en oeuvre du dispositif de poursuite de l'arrière-plan, installé à bord, etd) pour la transmission de l'objectif, on prédétermine une valeur pour la grandeur de corrélation, en adaptant la résolution des deux capteurs
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19546017A DE19546017C1 (de) | 1995-12-09 | 1995-12-09 | Flugkörper-Waffensystem |
DE19546017 | 1995-12-09 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0777100A2 EP0777100A2 (fr) | 1997-06-04 |
EP0777100A3 EP0777100A3 (fr) | 1999-09-01 |
EP0777100B1 true EP0777100B1 (fr) | 2002-07-24 |
Family
ID=7779680
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP96119417A Expired - Lifetime EP0777100B1 (fr) | 1995-12-09 | 1996-12-04 | Système d'arme missile |
Country Status (4)
Country | Link |
---|---|
US (1) | US5785275A (fr) |
EP (1) | EP0777100B1 (fr) |
DE (2) | DE19546017C1 (fr) |
ES (1) | ES2179146T3 (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4239277A1 (fr) * | 2022-03-01 | 2023-09-06 | Diehl Defence GmbH & Co. KG | Appareil et procédé de transfert de cible |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6181988B1 (en) * | 1998-04-07 | 2001-01-30 | Raytheon Company | Guidance system having a body fixed seeker with an adjustable look angle |
DE19828644C2 (de) * | 1998-06-26 | 2001-12-06 | Lfk Gmbh | Verfahren zum ferngesteuerten Bekämpfen bodennaher und/oder bodengebundener Ziele |
FR2830078B1 (fr) * | 2001-09-25 | 2004-01-30 | Sagem | Procede de guidage d'une roquette |
DE10158666A1 (de) * | 2001-11-28 | 2003-06-18 | Lfk Gmbh | Vorrichtung und Verfahren zur autarken Zielführung eines Flugkörpers mit Hilfe außerhalb des Zielpunktes liegender Orientierungsmerkmale |
PL1913557T3 (pl) | 2005-06-23 | 2016-12-30 | System i metoda śledzenia poruszających się obiektów | |
US9229230B2 (en) | 2007-02-28 | 2016-01-05 | Science Applications International Corporation | System and method for video image registration and/or providing supplemental data in a heads up display |
IL219639A (en) | 2012-05-08 | 2016-04-21 | Israel Aerospace Ind Ltd | Remote object tracking |
US10212396B2 (en) | 2013-01-15 | 2019-02-19 | Israel Aerospace Industries Ltd | Remote tracking of objects |
IL224273B (en) | 2013-01-17 | 2018-05-31 | Cohen Yossi | Delay compensation during remote sensor control |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3923273A (en) * | 1967-01-30 | 1975-12-02 | Us Navy | Aim point correlator |
US3986682A (en) * | 1974-09-17 | 1976-10-19 | The United States Of America As Represented By The Secretary Of The Navy | Ibis guidance and control system |
GB1568058A (en) * | 1975-11-21 | 1980-05-21 | Emi Ltd | Tracking and/or huidance systems |
DE3334729A1 (de) * | 1983-09-26 | 1985-04-11 | Siemens AG, 1000 Berlin und 8000 München | Verfahren zur ausrichtung eines zielsuchkopfes eines selbstgesteuerten flugkoerpers |
GB2148465B (en) * | 1983-10-20 | 1987-05-28 | Nader Dadabhoy Daroga | Missile control systems |
DE3435634A1 (de) * | 1984-09-28 | 1986-04-10 | Diehl GmbH & Co, 8500 Nürnberg | Zielerfassungseinrichtung fuer flugkoerper |
US5341142A (en) * | 1987-07-24 | 1994-08-23 | Northrop Grumman Corporation | Target acquisition and tracking system |
USH796H (en) * | 1989-11-27 | 1990-07-03 | The United States Of America As Represented By The Secretary Of The Army | Open loop seeker aiming guiding system |
US5274236A (en) * | 1992-12-16 | 1993-12-28 | Westinghouse Electric Corp. | Method and apparatus for registering two images from different sensors |
US5323987A (en) * | 1993-03-04 | 1994-06-28 | The Boeing Company | Missile seeker system and method |
-
1995
- 1995-12-09 DE DE19546017A patent/DE19546017C1/de not_active Expired - Fee Related
-
1996
- 1996-11-25 US US08/758,144 patent/US5785275A/en not_active Expired - Fee Related
- 1996-12-04 ES ES96119417T patent/ES2179146T3/es not_active Expired - Lifetime
- 1996-12-04 EP EP96119417A patent/EP0777100B1/fr not_active Expired - Lifetime
- 1996-12-04 DE DE59609477T patent/DE59609477D1/de not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4239277A1 (fr) * | 2022-03-01 | 2023-09-06 | Diehl Defence GmbH & Co. KG | Appareil et procédé de transfert de cible |
Also Published As
Publication number | Publication date |
---|---|
US5785275A (en) | 1998-07-28 |
ES2179146T3 (es) | 2003-01-16 |
DE59609477D1 (de) | 2002-08-29 |
DE19546017C1 (de) | 1997-04-24 |
EP0777100A3 (fr) | 1999-09-01 |
EP0777100A2 (fr) | 1997-06-04 |
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