EP0260191A1 - Verfahren und Vorrichtung zur Darstellung von Zielen oder der Lage von Zielen mit Hilfe der Datenempfangseinrichtung des Waffensystems - Google Patents

Verfahren und Vorrichtung zur Darstellung von Zielen oder der Lage von Zielen mit Hilfe der Datenempfangseinrichtung des Waffensystems Download PDF

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Publication number
EP0260191A1
EP0260191A1 EP19870401992 EP87401992A EP0260191A1 EP 0260191 A1 EP0260191 A1 EP 0260191A1 EP 19870401992 EP19870401992 EP 19870401992 EP 87401992 A EP87401992 A EP 87401992A EP 0260191 A1 EP0260191 A1 EP 0260191A1
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EP
European Patent Office
Prior art keywords
data acquisition
target
seeker
acquisition means
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.)
Granted
Application number
EP19870401992
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English (en)
French (fr)
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EP0260191B1 (de
Inventor
Jacques Perrin
Pascal Sinaud
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thales SA
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Thomson CSF SA
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Publication date
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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
    • F41G7/007—Preparatory measures taken before the launching of the guided missiles

Definitions

  • the invention relates mainly to a method and a device for viewing targets and / or target positions using data acquisition means of a weapon system.
  • These data acquisition means allowed the identification of the target as friends or enemies and the choice among the enemies of the target that we want to destroy as a priority; - the attachment of the missile data acquisition means to the chosen target; - checking that the missile data acquisition means are properly attached to the targeted target.
  • the device according to the present invention makes it possible, before the launch of the missile, to collect information coming from the missile data acquisition means to supplement the information collected by the data acquisition means of the launch platform (in particular the means fire control).
  • the device according to the present invention makes it possible in particular to collect additional information on the target, for example information from a detector in another frequency band, to collect information when the data acquisition devices of the launch site do not are not pointed towards the target or when said data acquisition means have been destroyed.
  • the main object of the invention is a lan device seeker missile cement including directing means, essentially characterized by the fact that it comprises means allowing the visualization on display on the means of visualization of the targets and / or of the positions of the targets provided by the missile.
  • the subject of the invention is also a method for viewing targets and / or positions of targets on means for viewing a missile launch platform, characterized in that the data acquisition means are used of a weapon system.
  • FIGS. 1 to 5 the same references have been used to designate the same elements.
  • FIG 1 we can see a launch pad 7 of missiles 1, 2, 3 and 4. Missiles 1, 2, 3 and 4 are for example anti-aircraft missiles.
  • the shooting platform 7 is connected by a line 9 to a control device 8.
  • the control device 8 comprises in particular a computer capable of collecting information which is transmitted to it and of sending by a line 9 control signals to firing platform control circuits 7.
  • the shooting platform 7 includes means for acquiring data for example a camera whose sensitivity is in a visible spectrum 5 as well as an infrared camera 6.
  • the control device 8 is advantageously connected to other data acquisition devices such as for example a radar 10, to an optical objective designation device 42 (helmet), a laser rangefinder 43 or a friend-enemy detection device 44 (IFF in English terminology).
  • the radar 10 is connected to the control device 8 by radio communication means 11.
  • the control device 8 is connected to human-machine interfaces.
  • the device 8 is connected to a screen 17 with cathode ray tube for viewing the images collected by the cameras 5 and / or 6, a screen 18 with jumper scanning making it possible to view the information collected by the radar 10, a keyboard 19 and a control lever 20.
  • missiles comprising an infrared seeker, a radar seeker, a visible seeker or an image processing device.
  • the seeker 12 of missile 4 is activated;
  • the firing platform 7 is pointed in the direction of the aircraft allowing the hooking of the seeker 12 on the aircraft;
  • the firing platform 7 performs a pointing allowing the missile 4 to have an advance angle facilitating the interception of the aircraft.
  • the firing platform 7 When the firing platform 7 performs a pointing allowing the missile 4 to have an angle of advance the television cameras 5 and 6 are no longer pointed in the direction of the missile. Thus, it is no longer possible to control, until the moment of firing, whether the seeker 12 of the missile 4 is still attached to the target.
  • the dropout of the seeker 12 can be caused for example by the movement of the firing platform 7, a sudden movement of avoidance of the aircraft, by the passage of the aircraft behind an obstacle such as for example a thicket of trees by the attachment of the seeker 12 to a more powerful source of radiation such as another aircraft or decoys.
  • the control device 8 By collecting and viewing information transmitted by the seeker 12 of the missile 4 before firing the control device 8 makes it possible to verify until the moment of the firing that the seeker 12 is indeed hooked on the targeted target.
  • the device according to the present invention makes it possible to operate in degraded mode.
  • the operator it is always possible for the operator to point the firing platform 7 towards an aircraft with the joystick 20 in the event of the unavailability of the television cameras 5 and 6, it suffices for example that it is superimposed on screen 17 a reticle 15 indicating the position of the target given by means of acquisition of the missile data (seeker) with the center of the screen 30 corresponding to the pointing direction of the turret.
  • control device 8 automatically points the firing platform 7 towards the aircraft according to the information transmitted by the seeker 12.
  • the seeker 12 can transmit information only if it is activated.
  • the activation of the seeker of a missile is obtained by the use of a sequencer for example included in the control device 8.
  • the automatic pointing of the firing platform is thus particularly advantageous in the case of use infrared seeker with reduced lifespan.
  • missiles 1 and 2 are shown in storage containers. It is understood that the seeker 12 of missiles 1 and 2 will only be able to collect information after the protective tubes have been dropped. Missiles 3 and 4 corresponding to an alternative embodiment without a protective tube.
  • FIG. 2 one can see a firing platform 7 comprising four missiles 1, 2, 3 and 4 and a television camera 5.
  • the television camera 5 is for example a camera sensitive to visible light.
  • the shooting platform 7 of FIG. 2 is an economical version of the shooting platform 7 of FIG. 1. These performances are lower than those of the shooting platform 7 of FIG. 1, in particular at night.
  • missiles comprising a passive infrared seeker it is possible, at night, to use said seeker to determine the position of the target, make the decision to fire, give an angle of advance to the interceptor missiles of the target.
  • FIG. 3 one can see an example of information displayed by a display screen 13.
  • the screen 13 for example with cathode ray tube, displays an aircraft 14 as well as a reticle 15.
  • the aircraft 14 is for example automatically tracked in deposit and in elevation by the firing platform 7.
  • the reticle 15 shows the pointing position of the missile seeker.
  • the superposition of the reticle 15 with the center of the screen 13 is facilitated by the presence of a reticle 30 at said center.
  • FIG. 4 one can see an example of information displayed by a display screen during the introduction of the angle of advance of the platform 7.
  • the aircraft 14 is no longer in the center of the screen 13
  • the magnification provided by the television camera, for example the camera 5 is less than the magnification in FIG. 3.
  • the aircraft is on the edge of the image.
  • the reticle 15 is superimposed on the aircraft 14. Depending on the distance and the speed of the aircraft it is possible that the latter completely disappears from the screen 13. In this case the reticle 15 is for example on the edge of the image.
  • the invention is not limited to anti-aircraft defense devices.
  • the invention also applies to terrestrial, maritime or mixed targets.
  • the invention applies to platforms 7 for launching missiles 1, 2, 3 and 4 comprising a seeker 12, means for viewing the targets 5, 6, 10, 13 and 16.
  • the device according to the present invention applies mainly to anti-aircraft defense platforms comprising missiles with passive infrared seeker 12 as well as anti-aircraft and anti-tank firing platforms.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
EP87401992A 1986-09-09 1987-09-04 Verfahren und Vorrichtung zur Darstellung von Zielen oder der Lage von Zielen mit Hilfe der Datenempfangseinrichtung des Waffensystems Expired - Lifetime EP0260191B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8612618A FR2603695B1 (fr) 1986-09-09 1986-09-09 Procede et dispositif de visualisation des cibles et/ou des positions des cibles utilisant des moyens d'acquisition des donnees d'un systeme d'armes
FR8612618 1986-09-09

Publications (2)

Publication Number Publication Date
EP0260191A1 true EP0260191A1 (de) 1988-03-16
EP0260191B1 EP0260191B1 (de) 1992-08-05

Family

ID=9338804

Family Applications (1)

Application Number Title Priority Date Filing Date
EP87401992A Expired - Lifetime EP0260191B1 (de) 1986-09-09 1987-09-04 Verfahren und Vorrichtung zur Darstellung von Zielen oder der Lage von Zielen mit Hilfe der Datenempfangseinrichtung des Waffensystems

Country Status (9)

Country Link
US (1) US4843459A (de)
EP (1) EP0260191B1 (de)
JP (1) JPS6375492A (de)
AR (1) AR247022A1 (de)
CA (1) CA1305886C (de)
DE (1) DE3780888T2 (de)
DK (1) DK168966B1 (de)
ES (1) ES2033901T3 (de)
FR (1) FR2603695B1 (de)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0276099A2 (de) * 1987-01-16 1988-07-27 Recon/Optical, Inc. Einvisiermittel für Geschoss
EP0431892A2 (de) * 1989-12-07 1991-06-12 Hughes Aircraft Company Verteiltes Werfernetzwerk für Aktivradar-Flugkörper
EP0431804A2 (de) * 1989-12-07 1991-06-12 Hughes Aircraft Company Werfersteuersystem für bodengeworfene Aktivradar-Flugkörper
EP0471225A2 (de) * 1990-08-16 1992-02-19 Hughes Aircraft Company Werfersteuersystem
GB2265444A (en) * 1992-03-28 1993-09-29 Secr Defence Aiming guided weapons
WO1997026550A2 (de) * 1996-01-20 1997-07-24 Dornier Gmbh Vorrichtung zum suchen, entdecken und verfolgen von flugzielen
WO1999010701A1 (de) * 1997-08-21 1999-03-04 LFK Lenkflugkörpersysteme GmbH Einrichtung zur zielentdeckung für ein flugkörpersystem
GR990100359A (el) * 1998-10-19 2000-06-30 Nauchno-Issledovatelsky Elektromekhanichesky Συστημα καθοδηγησης για αντιαεροπορικη πυραυλικη μοναδα μικρου βεληνεκους

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE58902538D1 (de) * 1988-05-19 1992-12-03 Siemens Ag Verfahren zur beobachtung einer szene und einrichtung zur durchfuehrung des verfahrens.
US5585813A (en) * 1992-10-05 1996-12-17 Rockwell International Corporation All aspect head aiming display
US5456157A (en) * 1992-12-02 1995-10-10 Computing Devices Canada Ltd. Weapon aiming system
DE4413916A1 (de) * 1994-04-21 1995-11-02 Bodenseewerk Geraetetech Einrichtung zur passiven Freund/Feind-Unterscheidung
US7856750B2 (en) 1997-12-08 2010-12-28 Horus Vision Llc Apparatus and method for calculating aiming point information
FR2793885A1 (fr) 1999-05-17 2000-11-24 Thomson Csf Procede et dispositif de guidage electromagnetique, appliques notamment a la poursuite de cibles
US6625454B1 (en) 2000-08-04 2003-09-23 Wireless Valley Communications, Inc. Method and system for designing or deploying a communications network which considers frequency dependent effects
US6973622B1 (en) 2000-09-25 2005-12-06 Wireless Valley Communications, Inc. System and method for design, tracking, measurement, prediction and optimization of data communication networks
US7773995B2 (en) * 2005-04-18 2010-08-10 Motorola, Inc. Method and apparatus for utilizing RF signals to create a site specific representation of an environment
US8063347B1 (en) * 2009-01-19 2011-11-22 Lockheed Martin Corporation Sensor independent engagement decision processing
CN102213566A (zh) * 2010-04-02 2011-10-12 倪明旺 对称调制弹道制导装置
JP5818479B2 (ja) 2011-03-29 2015-11-18 三菱重工業株式会社 管制装置、表示装置、協調運用システム、及び管制方法
US8902085B1 (en) * 2011-05-17 2014-12-02 Raytheon Company Integrated 3D audiovisual threat cueing system
IL228789A (en) 2013-10-08 2016-03-31 Israel Aerospace Ind Ltd A rocket system that includes a b-ads receiver
WO2020112197A2 (en) 2018-09-04 2020-06-04 Hvrt Corp. Reticles, methods of use and manufacture
CN114184091A (zh) * 2021-04-08 2022-03-15 西安龙飞电气技术有限公司 空空导弹导引头的红外雷达双模数字处理方法

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3742812A (en) * 1969-03-28 1973-07-03 Us Navy Method of aiming a television guided missile
US3912198A (en) * 1964-11-04 1975-10-14 Ltv Aerospace Corp Tracking system
GB2004038A (en) * 1977-09-09 1979-03-21 Messerschmitt Boelkow Blohm Missile seeker head vectoring system
US4324491A (en) * 1973-02-12 1982-04-13 The United States Of America As Represented By The Secretary Of The Navy Dual mode guidance system
GB2103341A (en) * 1981-08-03 1983-02-16 Ferranti Ltd Aiming rocket launchers
GB2143931A (en) * 1983-07-29 1985-02-20 Messerschmitt Boelkow Blohm A sighting system for a guided missile
DE3334729A1 (de) * 1983-09-26 1985-04-11 Siemens AG, 1000 Berlin und 8000 München Verfahren zur ausrichtung eines zielsuchkopfes eines selbstgesteuerten flugkoerpers

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3598344A (en) * 1964-06-01 1971-08-10 Philco Ford Corp Missile command system
US3567163A (en) * 1964-10-08 1971-03-02 Martin Marietta Corp Guidance system
US3440651A (en) * 1966-09-01 1969-04-22 Us Navy Iff active readout control and display system
DE2411790C3 (de) * 1974-03-12 1978-06-29 Precitronic Gesellschaft Fuer Feinmechanik Und Electronic Mbh, 2000 Hamburg Verfahren und Waffensystem zur Bekämpfung von Oberflächenzielen
DE2533697A1 (de) * 1975-07-28 1977-02-03 Precitronic Einrichtung zur signaluebertragung zwischen einer abschussbasis und einem flugkoerper mittels einer lichtuebertragungsstrecke
US4146196A (en) * 1976-07-20 1979-03-27 The United States Of America As Represented By The Secretary Of The Air Force Simplified high accuracy guidance system
US4630049A (en) * 1982-06-28 1986-12-16 The United States Of America As Represented By The Secretary Of The Navy Digital-to-composite IFF video converter
FR2531231A1 (fr) * 1982-07-28 1984-02-03 Telecommunications Sa Procede de guidage passif pour engin
FR2559252B2 (fr) * 1984-02-07 1986-12-05 Cilas Alcatel Dispositif laser pour guider un missile sur une cible
CA1225451A (en) * 1984-02-27 1987-08-11 Alan Sewards Remote identification device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3912198A (en) * 1964-11-04 1975-10-14 Ltv Aerospace Corp Tracking system
US3742812A (en) * 1969-03-28 1973-07-03 Us Navy Method of aiming a television guided missile
US4324491A (en) * 1973-02-12 1982-04-13 The United States Of America As Represented By The Secretary Of The Navy Dual mode guidance system
GB2004038A (en) * 1977-09-09 1979-03-21 Messerschmitt Boelkow Blohm Missile seeker head vectoring system
GB2103341A (en) * 1981-08-03 1983-02-16 Ferranti Ltd Aiming rocket launchers
GB2143931A (en) * 1983-07-29 1985-02-20 Messerschmitt Boelkow Blohm A sighting system for a guided missile
DE3334729A1 (de) * 1983-09-26 1985-04-11 Siemens AG, 1000 Berlin und 8000 München Verfahren zur ausrichtung eines zielsuchkopfes eines selbstgesteuerten flugkoerpers

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
REVUE INTERNATIONALE DE DEFENSE, vol. 14, no. 11, 1981, pages 1463-1468, Cointrin-Genève, CH; J.PH. GEDDES: "Un nouveau départ pour le missile Maverick" *

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0276099A3 (de) * 1987-01-16 1991-07-03 Recon/Optical, Inc. Einvisiermittel für Geschoss
EP0276099A2 (de) * 1987-01-16 1988-07-27 Recon/Optical, Inc. Einvisiermittel für Geschoss
EP0431892A2 (de) * 1989-12-07 1991-06-12 Hughes Aircraft Company Verteiltes Werfernetzwerk für Aktivradar-Flugkörper
EP0431804A2 (de) * 1989-12-07 1991-06-12 Hughes Aircraft Company Werfersteuersystem für bodengeworfene Aktivradar-Flugkörper
EP0431804A3 (en) * 1989-12-07 1992-09-23 Hughes Aircraft Company Launcher control system for surface launched active radar missiles
EP0431892A3 (en) * 1989-12-07 1992-09-23 Hughes Aircraft Company Distributed launcher network for active radar missiles
TR26547A (tr) * 1990-08-16 1995-03-15 Hughes Aircraft Co FüZE FIRLATICILAR VE DAHA BELIRLI OLARAK BIR HAVA TASITININ FIRLATILMASINI VE UCUSUNU KONTROL ETMEK ICIN BIR FIRLATICI KONTROL SISTEMI.
EP0471225A2 (de) * 1990-08-16 1992-02-19 Hughes Aircraft Company Werfersteuersystem
EP0471225A3 (en) * 1990-08-16 1992-09-30 Hughes Aircraft Company Launcher control system
GB2265444A (en) * 1992-03-28 1993-09-29 Secr Defence Aiming guided weapons
GB2265444B (en) * 1992-03-28 1996-11-27 Secr Defence Aiming systems
WO1997026550A2 (de) * 1996-01-20 1997-07-24 Dornier Gmbh Vorrichtung zum suchen, entdecken und verfolgen von flugzielen
WO1997026550A3 (de) * 1996-01-20 1997-10-16 Dornier Gmbh Vorrichtung zum suchen, entdecken und verfolgen von flugzielen
US5964432A (en) * 1996-01-20 1999-10-12 Dornier Gmbh Lhg System for searching for, detecting and tracking flying targets
WO1999010701A1 (de) * 1997-08-21 1999-03-04 LFK Lenkflugkörpersysteme GmbH Einrichtung zur zielentdeckung für ein flugkörpersystem
US6484966B1 (en) 1997-08-21 2002-11-26 Lfk-Lenkflugkorpesysteme Gmbh Target-detection device for a missile system
GR990100359A (el) * 1998-10-19 2000-06-30 Nauchno-Issledovatelsky Elektromekhanichesky Συστημα καθοδηγησης για αντιαεροπορικη πυραυλικη μοναδα μικρου βεληνεκους

Also Published As

Publication number Publication date
FR2603695A1 (fr) 1988-03-11
JPS6375492A (ja) 1988-04-05
DK168966B1 (da) 1994-07-18
DE3780888D1 (de) 1992-09-10
CA1305886C (en) 1992-08-04
EP0260191B1 (de) 1992-08-05
ES2033901T3 (es) 1993-04-01
FR2603695B1 (fr) 1990-10-19
DK464187A (da) 1988-03-10
US4843459A (en) 1989-06-27
DK464187D0 (da) 1987-09-07
AR247022A1 (es) 1994-10-31
DE3780888T2 (de) 1992-12-24

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