EP1782018A1 - Verfahren und system zur aktivierung einer munitionslast, mit einer hochpräzisen aktivierungsvorrichtung versehene munition und system zur neutralisierung eines ziels - Google Patents

Verfahren und system zur aktivierung einer munitionslast, mit einer hochpräzisen aktivierungsvorrichtung versehene munition und system zur neutralisierung eines ziels

Info

Publication number
EP1782018A1
EP1782018A1 EP05774192A EP05774192A EP1782018A1 EP 1782018 A1 EP1782018 A1 EP 1782018A1 EP 05774192 A EP05774192 A EP 05774192A EP 05774192 A EP05774192 A EP 05774192A EP 1782018 A1 EP1782018 A1 EP 1782018A1
Authority
EP
European Patent Office
Prior art keywords
munition
ammunition
target
optical
detectors
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.)
Ceased
Application number
EP05774192A
Other languages
English (en)
French (fr)
Inventor
Jean-Paul Thales Intellectual Property GUYVARCH
Patrick Thales Intellectual Property Doignon
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.)
TDA Armements SAS
Original Assignee
TDA Armements SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by TDA Armements SAS filed Critical TDA Armements SAS
Publication of EP1782018A1 publication Critical patent/EP1782018A1/de
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C13/00Proximity fuzes; Fuzes for remote detonation
    • F42C13/02Proximity fuzes; Fuzes for remote detonation operated by intensity of light or similar radiation

Definitions

  • the present invention relates to a method and a system for activating the charge of a munition. It also relates to a munition equipped with a high precision activation device. Finally, it concerns a system for neutralizing a target. The invention applies in particular to hit hidden targets where there is not necessarily a direct impact with these targets.
  • the guided or unguided munitions fired remotely by any device can have a direct kinetic effect on the objective. This effect may be lethal or non-lethal depending on the shooting conditions and the nature of the projectile, such as metal or rubber.
  • These ammunition can also have a reinforced or indirect effect by equipping the munition with a secondary device such as:
  • a pyrotechnic charge which is hollow, explosive or dispersed with sub-projectiles, liquid or gas, for example a tear gas;
  • indirect effects applications include, for example:
  • An object of the invention is in particular to overcome the aforementioned drawbacks, in particular by allowing a sufficiently precise trigger position without implementation complexity.
  • the subject of the invention is a method of activating a munition near a target using a laser beam that illuminates an object located near the target, firing the charge of the ammunition being activated from the detection by the munition of the laser spot backscattered by the object.
  • the firing is activated a time ⁇ t1 after the detection time t 0 of the laser spot, possibly the time ⁇ t1 is substantially zero.
  • the aiming direction of the munition preferably passes close to the object.
  • the object can be an obstacle behind which hides the target.
  • the head of the ammunition is equipped with at least one optical detector.
  • the invention also relates to a system for activating a munition near a target, the system comprising at least: a laser source creating a beam that illuminates an object located near the target;
  • an optical device equipping the munition to detect the laser spot backscattered by the object; a control block equipping the munition creating the activation signal from a detection signal received by the optical device.
  • the laser source being coupled to the gun firing the ammunition, the aiming direction of the barrel passes close to the object.
  • the control block transmits the firing signal a time ⁇ t1, possibly zero, after the instant t 0 for receiving the detection signal.
  • the optical device comprises, for example optical detectors placed at the periphery of the head of the munition.
  • the invention also relates to a munition comprising an activation device composed of at least one optical detector and a control block, the optical detector being intended to detect a signal produced by an object located near a target.
  • the detectors are disposed at the periphery of the head of the munition.
  • the optical detectors are for example located on the periphery of the same cross section.
  • the optical opening of the detectors is elliptical, the major axis of the opening being oriented perpendicular to the axis of symmetry of the munition.
  • the optical axis of a detector forms for example with the axis of the munition an angle ⁇ substantially equal to 60 °.
  • the optical detector 43 and the control block are made for example in the form of a kit adaptable to ammunition existing instead of a control device originally equipping the munition.
  • the invention finally relates to a system for neutralizing a target comprising at least one munition as defined above and a laser source for illuminating an object located near the target, the firing of the charge of the munition being activated by the control block from the detection of the laser spot backscattered by the object.
  • FIG. 1 an exemplary implementation of the activation of the charge of a munition according to the prior art
  • FIG. 2 an illustration of the method and of a system according to the invention for activating an ammunition
  • FIG. 3 an illustration of the trajectory of a munition in the vicinity of an object located near a target
  • FIG. 4 an illustration of the head of a munition equipped with an activation device according to the invention.
  • FIG. 1 illustrates an exemplary implementation of a system for activating the charge of a munition according to the prior art.
  • a munition 1 is fired at a distance by a gun 2.
  • the purpose of the mission is to neutralize a target X hidden behind an obstacle 3, for example a wall.
  • the gun 2 is located about one kilometer from the wall 3. Knowing the speed of the ammunition 1, it is theoretically possible to deduce at a time ⁇ t after firing the distance traveled by the ammunition. On the other hand, knowing the distance D to which the charge of the munition must explode, one deduces the corresponding delay ⁇ t 0 to apply to the firing.
  • the speed of the ammunition can not, for example, be better than 1%.
  • FIG. 2 illustrates a method and also a system for activating the charge of a munition 23 according to the invention.
  • a laser beam 21 is used. This laser beam 21 illuminates not the target X, because it is hidden, but an object located in its vicinity and chosen by the shooter.
  • the object may be the obstacle that hides the target, for example a wall or wall 3 behind which is hidden the target X.
  • the chosen object could also be for example the frame of a window or a window. opening of a building.
  • the aiming direction 22 of the ammunition 23 is chosen by the shooter. It passes close to the object 3. It aims for example the center of a window or a place located about a meter above a wall.
  • the laser beam 21 is created by a laser source, for example coupled to the barrel 2.
  • the munition 23 is equipped with a directional optical detector intended to detect the laser spot 24 backscattered by the neighboring object of the target X, in this case the wall 3 in the example of Figure 2, according to a predefined geometric configuration.
  • a firing delay ⁇ t1 is engaged. At the end of this time ⁇ t1 the munition is fired and explodes 25.
  • the time ⁇ t1 is very short but sufficient for the ammunition 23 to exceed the obstacle 3 and explode opposite the target X, close to the latter.
  • the uncertainty of the distance traveled since the detection of the laser spot on the obstacle is extremely small because the distance in play predefined is no longer of the order of a kilometer but of the order of ten meters, even a few meters.
  • an inaccuracy of 1% leads to an inaccuracy of distance traveled only 0.1 meters.
  • the optical detector of the munition detects the laser spot 24 and with the preset delay ⁇ t1, the charge of the ammunition is fired. If necessary ⁇ t1 can be taken equal to 0. In this case the delay created is the natural firing delay which is sufficient for the charge to explode a few meters after time t 0 .
  • the ammunition has an optical device. It also comprises a control block for processing the detection signals received by the optical device, creating the possible delay ⁇ t1 and creating the activation signal for firing the charge of the munition from a received detection signal .
  • the obstacle 3 is rough, that is to say that it comprises, in particular, surface irregularities of dimensions greater than the wavelength of the laser, and that it is not totally absorbent; which causes a backscattering laser signal 24 little directive and sufficient intensity to allow detection a few meters. These conditions are often encountered in reality and are therefore not very restrictive.
  • FIG. 3 illustrates the trajectory of the munition 23, assumed to be coincidental with the firing axis 22, and the optical axis 26 of a detector equipping the munition near the obstacle 3, for example a wall.
  • the two axes 22, 26 form a substantially constant angle ⁇ .
  • M 0 represents the first point of the trajectory 22 where the detector detects the laser spot 24 on the obstacle, corresponding to the instant t 0 above.
  • the spot is located at a point I on the surface of the obstacle.
  • the point H represents the projection of the point I on the trajectory 22 of the munition and the point M F the desired point of ignition on this same trajectory.
  • the distance M 0 H depends on the height of overflight of the munition with respect to the obstacle, the point illuminated on the obstacle and the angle ⁇ of orientation of the detector, assumed to be perfectly known. It follows that:
  • the uncertainty ⁇ (IH) is notably a function of the pointing errors of the laser sighting axis and the firing axis, the characteristics of the laser spot on the obstacle 3 and the characteristics of the detector embedded in the munition 23
  • the error ⁇ (IH) may be of the order of 2 meters.
  • angle ⁇ is important. This angle ⁇ depends in fact on the arrangement of the detector in the munition 23 and more particularly on the inclination of its optical axis with respect to the axis of the munition. If ⁇ is weak, the term 1 / tg ⁇ becomes very large and tends to infinity when ⁇ tends to 0.
  • the backscattered laser signal is weaker and more dependent on the surface state of the obstacle
  • FIG. 4 illustrates the head of a munition according to the invention, equipped with a high precision activation device.
  • a munition detonates at a location that can be precisely defined, including a precision as previously expressed.
  • the activation device comprises in particular optical detectors and an associated electronic processing and control unit.
  • the munition is composed of a body, not shown, for example comprising the pyrotechnic charge and the head 41.
  • the head has a substantially conical appearance around the axis of symmetry 42 of the munition which merges with the axis of its axis. trajectory during the shooting phase.
  • the head 41 of the munition comprises an optical device intended in particular to detect the laser spot reflected by an obstacle 3.
  • This optical device comprises optical detectors 43 placed at the periphery of the head 41 of the ammunition.
  • the optical detectors are for example infrared detectors.
  • the optical axis 26 of a detector 43 forms the angle ⁇ with the axis 42 of the munition. According to what has been specified above, the angle ⁇ is for example of the order of 60 °.
  • the field of optics is a parameter to adjust according to the characteristics of the mission.
  • the optical detectors are for example disposed on the same cross section of the head and distributed around the perimeter of this section.
  • detectors can be distributed regularly and in sufficient number to cover the entire space, and more particularly to take into account the roll of the ammunition. Indeed, the rolling position of the ammunition is generally not known. It is then necessary to use several detectors distributed around the perimeter of the head, preferably on the same cross section. These detectors may be distributed regularly and symmetrically with respect to the axis 42 of the munition. In order to limit the number of detectors, especially for cost reasons, it is advantageous to use optics with asymmetrical aperture, for example having a large field in the plane perpendicular to FIG. 4 passing through the optical axis 26. The opening of a detector is then elliptical, the major axis being oriented perpendicular to the axis of symmetry 42 of the munition.
  • the device with several detectors is also useful to reduce uncertainty in the instant of detection.
  • this rotation speed usually reaches values greater than 1000 revolutions per second. Under these conditions, two detectors can suffice.
  • the head furthermore comprises an electronic block intended in particular to process the optical signals supplied by the detectors and then to create the activation signal for firing the charge of the munition, possibly with the delay ⁇ t1.
  • the electronic block is connected to the optical detectors.
  • An ammunition whose head is illustrated in FIG. 3 can be used in a system substantially different from that of FIG. 2 provided that it can detect a signal, for example a laser spot, located near a target. Such an ammunition associated with a laser source composes an effective neutralization system of a target.
  • the optical detector 43 and the control block are for example made for example in the form of a kit adaptable to existing ammunition instead of a control device originally equipping the ammunition, for example to the place of a chronometric rocket or an impact detector.
  • the old control device is then removed, unscrewed for example, and replaced by the adaptable kit.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP05774192A 2004-07-23 2005-07-22 Verfahren und system zur aktivierung einer munitionslast, mit einer hochpräzisen aktivierungsvorrichtung versehene munition und system zur neutralisierung eines ziels Ceased EP1782018A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0408188A FR2873438B1 (fr) 2004-07-23 2004-07-23 Procede et systeme d'activation de la charge d'une munition, munition equipee d'un dispositif d'activation a grande precision et systeme de neutralisation d'une cible
PCT/EP2005/053582 WO2006010741A1 (fr) 2004-07-23 2005-07-22 Procede et systeme d'activation de la charge d'une munition, munition equipee d'un dispositif d'activation a grande precision et systeme de neutralisation d'une cible

Publications (1)

Publication Number Publication Date
EP1782018A1 true EP1782018A1 (de) 2007-05-09

Family

ID=34950063

Family Applications (1)

Application Number Title Priority Date Filing Date
EP05774192A Ceased EP1782018A1 (de) 2004-07-23 2005-07-22 Verfahren und system zur aktivierung einer munitionslast, mit einer hochpräzisen aktivierungsvorrichtung versehene munition und system zur neutralisierung eines ziels

Country Status (5)

Country Link
US (1) US8146499B2 (de)
EP (1) EP1782018A1 (de)
FR (1) FR2873438B1 (de)
IL (1) IL180868A0 (de)
WO (1) WO2006010741A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8378277B2 (en) 2009-11-30 2013-02-19 Physical Optics Corporation Optical impact control system

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4269121A (en) * 1974-08-12 1981-05-26 The United States Of America As Represented By The Secretary Of The Navy Semi-active optical fuzing
US4199686A (en) * 1978-07-31 1980-04-22 Coulter Electronics, Inc. Dark field illuminator and collector apparatus and method
GB2132740B (en) * 1982-07-21 1986-03-12 James Bertram King Weapons system
SE460439C (sv) * 1986-12-11 1999-05-11 Bofors Ab Zonrör för robot, projektil eller liknande
FR2747185B1 (fr) * 1996-04-05 1998-05-22 Luchaire Defense Sa Projectile generateur d'eclats dont la charge explosive est declenchee au moyen d'un designateur de cible
IL150295A0 (en) * 2002-06-18 2003-05-29 Rafael Armament Dev Authority Bullet
US7143539B2 (en) * 2004-07-15 2006-12-05 Taser International, Inc. Electric discharge weapon

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2006010741A1 *

Also Published As

Publication number Publication date
FR2873438B1 (fr) 2006-11-17
IL180868A0 (en) 2007-07-04
US20070193466A1 (en) 2007-08-23
WO2006010741A1 (fr) 2006-02-02
FR2873438A1 (fr) 2006-01-27
US8146499B2 (en) 2012-04-03

Similar Documents

Publication Publication Date Title
JPH0215122Y2 (de)
EP0887613B1 (de) Im-Flug-Programmierverfahren für Auslösungsmoment eines Geschosselements, Feuerleitung und Zünder zur Durchführung dieses Verfahrens
EP1719969B1 (de) Verfahren zum Steuern einer Munition oder einer Submunition, Angreifsystem, Munition und Zielanzeiger für eine Durchführung eines solchen Verfahrens
EP0273787B1 (de) Geschoss zum indirekten Angriff auf Panzerfahrzeuge
EP0800054B1 (de) Geschoss dessen Sprengladung durch einen Zielanzeiger ausgelöst wird
FR2739921A1 (fr) Dispositif de protection pour vehicule blinde
FR2742540A1 (fr) Projectile avec un dispositif de correction de la trajectoire
FR2761463A1 (fr) Dispositif de conduite de tir pour systeme de defense antiaerienne, notamment mobile
FR2514884A1 (fr) Procede et dispositif pour corriger globalement, d'un tir au suivant, le tir d'une arme a tir tendu
EP2570761A1 (de) Method for detecting an impact point on an actual mobile target
EP2600097B1 (de) Kontrollverfahren zur Auslösung eines Gefechtskopfes, Kontrollvorrichtung und Zünder eines Geschosses, in dem ein solches Verfahren zur Anwendung kommt
EP1782018A1 (de) Verfahren und system zur aktivierung einer munitionslast, mit einer hochpräzisen aktivierungsvorrichtung versehene munition und system zur neutralisierung eines ziels
EP1536246B1 (de) Verfahren zur Detektion des Eintritts eines Zieles in einer Zone, Detektionsgerät und Schutzgerät zur Durchführung des Verfahrens
EP0918205B1 (de) Projektil mit radialer Wirkrichtung
EP0913662B1 (de) Hohlladungsprojektil und dazugehöriges Waffensystem
EP1293751B1 (de) Verfahren zum Einstellen eines Geschosszünders, Programmiereinrichtung und Zeitzünder die in einen solchem Verfahren verwendet werden
WO1988004400A1 (fr) Guidage par infra-rouge simplifie pour tout projectile
FR2577036A1 (fr) Systeme d'arme a projectiles contenant une charge vulnerante
EP0809084B1 (de) Vorrichtung zur Rollwinkelbestimmung eines Flugkörpers, insbesondere einer Munition
FR2929700A1 (fr) Dispositif decentralise d'autodefense comprenant un pointeur portable et mobile apte a assurer en urgence la defense rapprochee d'un navire ou d'une plate-forme en mer contre une menace de surface.
FR2860065A1 (fr) Systeme de protection d'une cible
FR2716966A1 (fr) Système de défense anti-aérienne à très courte portée, de type missile sol-air.
FR2634012A1 (fr) Projectile antibut mobile, a echelon unique de correction, a pilotage par reference pendulaire et a trois modes de detection selectionnables
FR2863055A1 (fr) Procede de detection de l'approche d'une cible, dispositif de detection et dispositif de protection mettant en oeuvre ce procede
FR2747185A1 (fr) Projectile generateur d'eclats dont la charge explosive est declenchee au moyen d'un designateur de cible

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20070205

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB IT

17Q First examination report despatched

Effective date: 20070920

DAX Request for extension of the european patent (deleted)
RBV Designated contracting states (corrected)

Designated state(s): DE FR GB IT

18D Application deemed to be withdrawn

Effective date: 20150209

D18D Application deemed to be withdrawn (deleted)
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION HAS BEEN REFUSED

18R Application refused

Effective date: 20160314