EP1983294B1 - Method and device for combating a launching position of an attack munition - Google Patents
Method and device for combating a launching position of an attack munition Download PDFInfo
- Publication number
- EP1983294B1 EP1983294B1 EP20080007446 EP08007446A EP1983294B1 EP 1983294 B1 EP1983294 B1 EP 1983294B1 EP 20080007446 EP20080007446 EP 20080007446 EP 08007446 A EP08007446 A EP 08007446A EP 1983294 B1 EP1983294 B1 EP 1983294B1
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- weapon
- ammunition body
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- main
- assault
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- 238000000034 method Methods 0.000 title claims description 25
- 238000010304 firing Methods 0.000 claims description 14
- 230000033001 locomotion Effects 0.000 claims description 9
- 230000000295 complement effect Effects 0.000 claims description 3
- 238000012876 topography Methods 0.000 claims description 3
- 238000005259 measurement Methods 0.000 claims description 2
- 230000003028 elevating effect Effects 0.000 claims 1
- 239000004570 mortar (masonry) Substances 0.000 description 15
- 230000007123 defense Effects 0.000 description 13
- 238000004364 calculation method Methods 0.000 description 4
- 238000010276 construction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
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Classifications
-
- 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
Definitions
- a defense ammunition body from a main weapon in particular an artillery gun, or a secondary weapon, in particular a mortar launcher, is fired, in which case the defense ammunition body according to the selection and is fired in accordance with a determined by a Feuerleitrechner Feuerleitans.
- the mortar weapon system of the secondary weapon 7 can shoot 3 'in the larger upper angle group range due to the use of mortar defense ammunition and thus reach short ranges of well below 1,000 m, for example from 400 m. In particular, goals in this distance range in Schuhanghus are effectively combated.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
Die Erfindung betrifft ein Verfahren und eine Vorrichtung zur Bekämpfung einer einen fliegenden Angriffsmunitionskörper abfeuernden Abschussvorrichtung. Fliegende Angriffsmunitionskörper können insbesondere Raketen sowie Artillerie- und Mörsergeschosse (sogenannte RAM-Bedrohung) u.Ä. darstellen.The invention relates to a method and an apparatus for controlling a launching device firing a flying attack ammunition. Flying assault ammunition can be used in particular for missiles and artillery and mortar shells (so-called RAM threat) and the like. represent.
Es ist bekannt, nach der Ortung eines Angriffsmunitionskörpers Gegenmaßnahmen einzuleiten. So kann beispielsweise versucht werden, den Angriffsmunitionskörper durch Abfeuern eines Abwehrmunitionskörpers in der Luft zu bekämpfen. Ein solches Verfahren und eine solche Vorrichtung werden in der zum Zeitpunkt der vorliegenden Anmeldung noch nicht veröffentlichten deutschen Patentanmeldung
Neben der Maßnahme, den fliegenden Angriffsmunitionskörper zu bekämpfen, ist es auch sinnvoll, die gegnerische Abschussvorrichtung des Angriffsmunitionskörpers unschädlich zu machen, damit weitere Angriffe verhindert werden können. Aus diesem Grund ist es bekannt, die Flugbahn des Angriffsmunitionskörpers zu ermitteln, um daraus durch Rückrechnung den Abschussort zu bestimmen und Abwehrmunitionskörper in Richtung dieser Position abzufeuern. Diese Art der Bekämpfung sollte möglichst schnell erfolgen, da der angreifende Gegner häufig nach dem Abfeuern eines oder mehrerer Angriffsmunitionskörper seine in der Regel mobile Abschussvorrichtung an eine andere, unbekannte Position bewegt.In addition to the measure to combat the flying attack ammunition, it is also useful to make the enemy launching device of the attack ammunition harmless, so that further attacks can be prevented. For this reason, it is known to determine the trajectory of the attack ammunition body to determine from it by recalculation of the shooting site and fire defense ammunition in the direction of this position. This type of combat should be done as quickly as possible, since the attacking opponent often moves his usually mobile launcher to another, unknown position after firing one or more assault ammo.
Es ist die Aufgabe der Erfindung, ein Verfahren und eine Vorrichtung bereitzustellen, die es ermöglichen, mittels eines Waffensystems eine gegnerische Abschussvorrichtung für einen großen Bereich an Entfernungen zwischen dem Waffensystem und der gegnerischen Abschussvorrichtung möglichst schnell zu bekämpfen.It is the object of the invention to provide a method and a device which make it possible, by means of a weapon system, to combat as fast as possible an enemy launcher for a wide range of distances between the weapon system and the enemy launcher.
Die Erfindung löst die Aufgabe verfahrensmäßig mit den Merkmalen aus dem Patentanspruch 1 und vorrichtungsmäßig mit den Merkmalen aus dem Patentanspruch 9. Vorteilhafte Weiterbildungen sind Bestandteil der abhängigen Ansprüche.The invention solves the problem procedurally with the features of
Das Verfahren zur Bekämpfung einer einen fliegenden Angriffsmunitionskörper abfeuernden Angriffsmunitionskörper-Abschussvorrichtung, sieht unter anderem vor, dass der Abschussort der gegnerischen Abschussvorrichtung ermittelt wird. Hierfür muss zunächst mittels einer Rechnereinheit die Flugbahn des zuvor mittels mindestens einer Ortungseinrichtung georteten Angriffsmunitionskörpers bekannt sein, so dass anschließend durch Rückrechnung der Abschussort bestimmt werden kann.The method for controlling an assault ammunition launcher firing a flying assault ammunition device provides inter alia that the launch site of the enemy launcher is determined. For this purpose, first by means of a computer unit the trajectory of the previously by means of at least one locating device be known attacked ammunition so that subsequently determined by recalculation of the shooting site.
Die bereits eingeführte Patentanmeldung
Ferner wird erfindungsgemäß nach der Ermittlung des Abschussortes mittels einer Auswahl-Rechnereinheit ausgewählt, ob ein Abwehrmunitionskörper aus einer Hauptwaffe, insbesondere ein Artilleriegeschütz, oder einer insbesondere an der Hauptwaffe angeordneten Nebenwaffe, insbesondere eine Mörserabschussvorrichtung, abgefeuert wird, wobei anschließend der Abwehrmunitionskörper gemäß der Auswahl und gemäß einer durch einen Feuerleitrechner ermittelten Feuerleitlösung abgefeuert wird.Furthermore, according to the invention, after the determination of the launching location by means of a selection computer unit, it is selected whether a defense ammunition body from a main weapon, in particular an artillery gun, or a secondary weapon, in particular a mortar launcher, is fired, in which case the defense ammunition body according to the selection and is fired in accordance with a determined by a Feuerleitrechner Feuerleitlösung.
Es ergänzen sich die Reichweitenbereiche der Haupt- und Nebenwaffe. So kann die minimale Reichweite der Nebenwaffe bei vorgegebenen Umgebungsbedingungen kleiner als die minimale Reichweite der Hauptwaffe sein. Ferner kann die maximale Reichweite der Hauptwaffe größer als die maximale Reichweite der Nebenwaffe sein. Somit wird ein möglichst großer Entfernungsbereich abgedeckt, in dem sich die gegnerische Abschussvorrichtung erfolgreich bekämpfen lässt. Als besonders vorteilhaft hat es sich erwiesen, dass als Hauptwaffe ein Artilleriegeschütz und als Nebenwaffe eine Mörserabschussvorrichtung verwendet wird, da somit der Nahbereich durch die Mörserabschussvorrichtung und der Fernbereich durch das Artilleriegeschütz abgedeckt ist, wobei auch ein Überlappungsbereich vorgesehen sein kann. Die Verwendung dieser Komponenten hat den weiteren Vorteil, dass das Artilleriegeschütz auch zur Bekämpfung der fliegenden Angriffsmunitionskörper nach der bereits eingeführten Anmeldung
Der Abwehrmunitionskörper kann nach der Auswahl der entsprechenden Waffe automatisch abgefeuert werden, wobei das Ergebnis der Auswahl auch auf einer an die Auswahl-Rechnereinheit angeschlossenen Anzeigevorrichtung, wie ein Computer-Monitor, angezeigt werden kann, so dass die Auswahl aus Gründen der Sicherheit von einer das Waffensystem bedienenden Person überprüft und vor dem Abfeuern bestätigt werden kann. Durch eine entscheidungsunterstützende Software kann dem Bediener auch eine Entscheidungshilfe zum Einsatz entweder des Hauptwaffensystems oder des Nebenwaffensystems gegeben werden.The defense ammunition body can be fired automatically after the selection of the corresponding weapon, wherein the result of the selection can also be displayed on a connected to the selection computer unit display device, such as a computer monitor, so that the selection for reasons of safety of a the Checked weapon operating system and confirmed before firing. Decision support software may also provide the operator with decision support for use of either the main weapon system or the secondary weapon system.
Bei der Auswahl der geeigneten Waffe können der Standort der Haupt- und Nebenwaffe und der Zielstandort sowie die Geländetopographie berücksichtigt werden.When selecting the appropriate weapon, the location of the main and auxiliary weapon and the target location, as well as the terrain topography, can be taken into account.
Es kann im Rahmen der Auswahlermittlung versucht werden, jeweils eine Feuerleitlösung für die Hauptwaffe und Nebenwaffe zu ermitteln. Falls keine zulässige Feuerleitlösung für eine der Waffen gefunden werden kann, kann somit erkannt werden, ob die jeweilige Waffe für die Bekämpfung der gegnerischen Abschussvorrichtung geeignet ist. Die Ermittlung der entsprechenden Feuerleitlösung kann im Übrigen auch erst nach der Auswahl durchgeführt werden.It can be attempted within the framework of the selection determination to determine a Feuerleitlösung for each of the main weapon and secondary weapon. If no admissible Feuerleitlösung for one of the weapons can be found, it can thus be recognized whether the respective weapon is suitable for the fight against the enemy launcher. Incidentally, the determination of the corresponding fire-control solution can also be carried out only after the selection.
Die Feuerleitlösung für die Nebenwaffe kann bevorzugt mittels des gleichen Feuerleitrechners ermittelt werden, der auch die Feuerleitlösung der Hauptwaffe ermittelt.The Feuerleitlösung for the secondary weapon can preferably be determined by means of the same fire control computer, which also determines the Feuerleitlösung the main weapon.
Bevorzugt ist die Hauptwaffe Teil eines stationären oder selbstfahrenden Artilleriewaffensystems mit einem Geschützturm, wie z. B. eine Panzerhaubitze. Zu dieser bekannten Vorrichtung kann die Nebenwaffe, insbesondere eine Mörserabschussvorrichtung, nachgerüstet werden, die auf Grund der Mörsermunitionskörper, vorzugsweise mit einem Kaliber von 60 mm bis 120 mm, im größeren oberen Winkelgruppenbereich schießen kann. Vorteilhaft ist es, wenn die Nebenwaffe an dem Geschützturm, insbesondere auf dem Geschützturm, angeordnet ist.Preferably, the main weapon is part of a stationary or self-propelled artillery weapon system with a turret, such. B. a tank howitzer. For this known device, the secondary weapon, in particular a mortar launcher, be retrofitted, which can shoot on the basis of the mortar ammunition, preferably with a caliber of 60 mm to 120 mm, in the larger upper angle group range. It is advantageous if the auxiliary weapon is arranged on the turret, in particular on the turret.
Um den Aufbau der Haupt- und Nebenwaffe möglichst klein zu halten, kann für die Haupt- und Nebenwaffe ein gemeinsamer Antrieb für die Bewegung in Azimut vorgesehen sein. Hierbei kann die Bewegung der Nebenwaffe in Azimut mit der Bewegung der Hauptwaffe in Azimut mechanisch gekoppelt sein. Um die notwendigen Berechnungen hinsichtlich der Ausrichtung der Nebenwaffe gering zu halten, ist es vorteilhaft, wenn die Nebenwaffe parallel zur Hauptwaffe ausgerichtet ist. Sie kann jedoch auch mit einem vorgegebenen Versatz zur Hauptwaffe ausgerichtet sein.In order to keep the construction of the main and secondary weapon as small as possible, a common drive for the movement in azimuth can be provided for the main and secondary weapon. In this case, the movement of the secondary weapon in azimuth can be mechanically coupled to the movement of the main weapon in azimuth. To make the necessary calculations regarding To keep the alignment of the secondary weapon low, it is advantageous if the secondary weapon is aligned parallel to the main weapon. However, it can also be aligned with a predetermined offset to the main weapon.
Für die Elevation der Haupt- und Nebenwaffe kann jeweils ein eigener Antrieb vorgesehen sein, wobei der Antrieb der Nebenwaffe als winkelgebergesteuerter Höhenrichtantrieb ausgestaltet sein kann.
Des Weiteren kann der Richtbereich in Elevation der Nebenwaffe 0° bis <90°, insbesondere 0° bis 85°, betragen.For the elevation of the main and secondary weapon each have its own drive can be provided, the drive of the secondary weapon can be configured as angle encoder controlled elevation drive.
Furthermore, the directional range in elevation of the secondary weapon can be 0 ° to <90 °, in particular 0 ° to 85 °.
Bei der Ausgestaltung der Hauptwaffe als Artilleriegeschütz mit Geschützturm kann der Geschützturm eine verschließbare Luke aufweisen und die Nebenwaffe derart auf dem Geschützturm im Bereich der Luke angeordnet sein, dass ein manuelles Nachladen der Nebenwaffe, die zu diesem Zweck insbesondere in eine Indexposition bringbar ist, bequem von einer sich in der Luke befindlichen Person durchgeführt werden kann.In the design of the main weapon as an artillery gun with turret gun turret may have a closable hatch and the side weapon so arranged on the turret in the hatch that a manual reloading of the secondary weapon, which can be brought for this purpose, in particular in an index position, conveniently from a person in the hatch can be carried out.
Um eine besonders genaue Ausrichtung der beiden Waffen zu erhalten, kann das Waffensystem ein inertiales Navigationsgerät umfassen, welches die Position und/oder Richtung der Haupt- und Nebenwaffe ermittelt.In order to obtain a particularly accurate alignment of the two weapons, the weapon system may comprise an inertial navigation device, which determines the position and / or direction of the main and secondary weapon.
Um eine besonders genaue Flugbahnermittlung durchführen zu können, können nach der ersten Ortung des Angriffsmunitionskörpers durch die Ortungseinrichtung, insbesondere ein Rundsuchradargerät, die Ortungsdaten an eine zweite Ortungseinrichtung, insbesondere ein Zielfolgeradargerät, übergeben werden, welche die Messung der für die Bestimmung der Flugbahn notwendigen Größen durchführt.In order to be able to carry out a particularly accurate trajectory determination, after the first location of the assault ammunition by the locating device, in particular a Rundsuchradargerät, the location data to a second locating device, in particular a Zielfolderadargerät be passed, which performs the measurement necessary for the determination of the trajectory sizes ,
Ein mögliches Ausführungsbeispiel der Erfindung wird anhand der
- Fig. 1
- eine schematische Darstellung einer Vorrichtung zur Bekämpfung einer Angriffsmunitionskörper-Abschuss-vorrichtung;
- Fig. 2
- ein erstes Artilleriewaffensystem mit einer nachgerüsteten Nebenwaffe;
- Fig. 3
- das Artilleriewaffensystem nach
Fig. 2 in einer anderen Stellung; - Fig. 4
- ein zweites Artilleriewaffensystem mit einer nachgerüsteten Nebenwaffe;
- Fig. 5
- das Artilleriewaffensystem nach
Fig. 4 in einer anderen Stellung; - Fig. 6
- eine Detailansicht des Geschützturm des Artilleriewaffensystems nach
Fig. 2 während des Nachladens der Nebenwaffe; und - Fig. 7
- die Detailansicht nach
Fig. 6 in einer anderen Perspektive.
- Fig. 1
- a schematic representation of an apparatus for controlling an assault ammunition launcher;
- Fig. 2
- a first artillery weapons system with a retrofitted secondary weapon;
- Fig. 3
- the artillery weapon system
Fig. 2 in a different position; - Fig. 4
- a second artillery weapon system with a retrofitted secondary weapon;
- Fig. 5
- the artillery weapon system
Fig. 4 in a different position; - Fig. 6
- a detailed view of the turret of the artillery weapons system after
Fig. 2 while reloading the secondary weapon; and - Fig. 7
- the detail view after
Fig. 6 in a different perspective.
Die
Die Auswahl-Rechnereinheit 6, mittels der ausgewählt wird, ob ein Abwehrmunitionskörper 3 aus der Hauptwaffe 2 oder ein Abwehrmunitionskörper 3' aus der Nebenwaffe 7 abgefeuert wird, ist zusammen mit dem Feuerleitrechner 6 zusammengeführt.The
Die
Der als winkelgebergesteuerter Höhenrichtantrieb ausgeführte Antrieb 13 für die Bewegung in Elevation der Nebenwaffe ist in den
Die Mörser-Abwehrmunitionskörper 3' können mit allen zur Verfügung stehenden und geeigneten Zündern verschossen werden. Die Programmierung der Zünder erfolgt mit den für Mörser-Abwehrmunitionskörper 3' typischen Zündereinstellern.The mortar defense ammunition 3 'can be fired with all available and suitable detonators. The programming the detonator is made with the typical for mortar defense ammunition 3 'fuseholders.
Die Berechnung von Aufsatz und Vorhalt der Nebenwaffe 7 erfolgt im Waffensystemrechner 6 des Artilleriewaffensystems. Die Feuerleitverfahren zum Abfeuern der Mörser-Abwehrmunitionskörper 3' sind analog zu den Verfahren der Hauptwaffe 2 in Bezug auf Bekämpfung von bodennahen Zielen, vorwiegend in Hinterhangstellungen.The calculation of essay and Vorhalt the
Die beschriebene Hauptwaffe 2 ist aufgrund der verwendeten Munition (Geschoss- und Treibladungssystem) sowie der verwendeten Ballistikalgorithmen nach dem modifizierten Punkt-Masse-Modell gemäß STA-NAG 4355 in der Erreichung kurzer Reichweiten im indirekten Schießen (obere Winkelgruppe) auf untere Entfernungen bis > ca. 3,5 km begrenzt.The
Das Mörserwaffensystem der Nebenwaffe 7 kann aufgrund der Verwendung von Mörser-Abwehrmunitionskörper 3' im größeren oberen Winkelgruppenbereich schießen und somit kurze Reichweiten von weit unter 1.000 m, beispielsweise ab 400 m, erreichen. Damit sind insbesondere Ziele in diesem Entfernungsbereich in Hinterhangstellung wirkungsvoll bekämpfbar.The mortar weapon system of the
Der Bekämpfungsablauf ist wie folgt:
- I.
Ortung des Angriffsmunitionskörpers 4 mit der ersten Ortungseinrichtung 12; - II. Übergabe der Zieldaten an
die zweite Ortungseinrichtung 5 und Zielverfolgung; - III. Ermittlung der Flugbahn durch Anwendung des in
der Patentanmeldung DE beschriebenen Verfahrens und Ermittlung des Abschussortes durch Rückrechnug mittels der Bewegungsdifferentialgleichungen;10 2007 007 403.6 - IV. Bestimmung der Position und der Richtung der Hauptwaffe 2 und Nebenwaffe 7 mittels eines inertialen Navigationssystems (Kurs-Lage-Gerät);
- V. Auswahl des abzufeuernden Abwehrmunitionskörpers 3 oder 3' durch die Auswahl-
Rechnereinheit 6 unter Berücksichtigung der Standorte der Hauptwaffe 2 und Nebenwaffe 7 und des Zielstandorts und der Geländetopographie; - VI. Anzeige der Auswahl auf der
Anzeigevorrichtung 9; - VII. Manuelle Freigabe des Abfeuerns durch einen Bediener;
- VIII. Berechnung der entsprechenden Feuerleitlösung durch
den Feuerleitrechner 6; - IX.
Abfeuern des Abwehrmunitionskörpers 3 oder 3' in Richtung des Abschussortes.
- I. Locating the
assault ammunition 4 with thefirst locating device 12; - II. Transfer of the target data to the
second location device 5 and tracking; - III. Determination of the trajectory by applying the in the
patent application DE described method and determination of the shooting site by back-calculation by means of the motion differential equations;10 2007 007 403.6 - IV. Determining the position and direction of the
main weapon 2 andsecondary weapon 7 by means of an inertial navigation system (course-position device); - V. Selection of the
defensive ammunition body 3 or 3 'to be fired by theselection computer unit 6, taking into account the locations of themain weapon 2 andsub-weapon 7 and the target location and the terrain topography; - VI. Display of the selection on the
display device 9; - VII. Manual release of firing by an operator;
- VIII. Calculation of the appropriate Feuerleitlösung by the
fire control computer 6; - IX. Firing the
defensive ammunition 3 or 3 'in the direction of the shooting site.
Claims (19)
- A method for combating a launching device firing an air-borne assault ammunition body, whereini. the air-borne assault ammunition body (4) is located by means of at least one locating device (5, 12),ii. the trajectory of the assault ammunition body (4) is determined,iii. the launch point of the assault ammunition body (4) is determined,iv. a selection computer unit (6) is used to select whether a defence ammunition body (3, 3') is fired from a main weapon (2) or an auxiliary weapon (7) of the same weapon system, whereof the firing ranges complement one another, andv. the defence ammunition body (3, 3') is fired according to the selection.
- A method according to Claim 1, characterised in that the defence ammunition body (3, 3') is fired automatically according to the selection.
- A method according to Claim 1 or 2, characterised in that the result of the selection is displayed on a display device (9) connected to the selection computer unit (6).
- A method according to one of the preceding claims, characterised in that the position of the main weapon (2) and auxiliary weapon (7) and the target position and preferably the topography of the terrain are taken into account in the selection.
- A method according to one of the preceding claims, characterised in that a fire control solution for the main weapon (2) and auxiliary weapon (7) is determined in each case in the course of determining the selection.
- A method according to Claim 5, characterised in that the fire control solution for the auxiliary weapon (7) is determined by means of the same fire control computer (6) as that which also determines the fire control solution of the main weapon (2).
- A method according to one of the preceding claims, characterised in that the ballistic coefficient c of the assault ammunition body (4) is determined for the purpose of calculating the trajectory of the assault ammunition body (4).
- A method according to Claim 7, characterised in that the ballistic coefficient c is determined by identifying the air resistance of the assault ammunition body (4).
- A method according to Claim 8, characterised in that the difference between two kinetic energies of the assault ammunition body (4) at two points and the distance between these points is used to determine the air resistance in relation to mass, wherein, in particular for determining a kinetic energy, two measuring points are recorded by the locating device (5, 12) which are used to determine the velocity of the assault ammunition body (4).
- A method according to one of the preceding claims, characterised in that, after the first determination of the position of the assault ammunition body (4) by the locating device (12), the location data are transmitted to a second locating device (5), in particular a target-tracking radar device, which measures the necessary variables for determining the trajectory.
- A device for implementing the method according to one of the preceding claims, havingi. a locating device (5, 12), in particular a radar device, for locating an air-borne assault ammunition body (4),ii. at least one computer unit, in particular a fire control computer (6), for determining the trajectory and the firing point of the assault projectile (4),iii. a main weapon (2) and an auxiliary weapon (7) of the same weapon system, whereof the firing ranges complement one another,iv. a selection computer unit (6) for determining the selection as to whether a defence ammunition body (3, 3') is fired from the main weapon (2) or the auxiliary weapon (7),v. at least one fire control computer (6) for determining fire control solutions for the main weapon (2) and auxiliary weapon (7).
- A device according to Claim 11, characterised in that the main weapon (2) is part of a stationary or automotive artillery weapon system (1) with a turret (8) and in that the auxiliary weapon (7) is arranged on the turret (8).
- A device according to Claim 11 or 12, characterised in that it has a common drive for the azimuth movement of the main weapon (2) and auxiliary weapon (7).
- A device according to one of Claims 11 to 13, characterised in that it is designed such that the azimuth movement of the auxiliary weapon (7) is mechanically linked to the azimuth movement of the main weapon (2).
- A device according to Claim 13 or 14, characterised in that the auxiliary weapon (7) is aligned parallel to the main weapon (2) or with a predetermined offset therefrom.
- A device according to one of Claims 11 to 15, characterised in that it has a separate drive for the elevation of the main weapon (2) and auxiliary weapon (7) in each case, wherein the drive of the auxiliary weapon (7) is designed in particular as an elevating drive (13) controlled by an angle transmitter.
- A device according to one of Claims 12 to 16, characterised in that the turret (8) has a closable hatch (10) and in that the auxiliary weapon (7) is arranged on the turret (8) in the region of the hatch (10) such that it is possible for a person (14) located in the hatch (10) to carry out manual reloading of the auxiliary weapon (7) which, for this purpose, can be brought in particular into an index position.
- A device according to one of Claims 11 to 17, characterised in that it comprises an inertial navigation device which determines the position and/or direction of the main weapon (2) and auxiliary weapon (7).
- A device according to one of Claims 11 to 18, characterised in that it comprises a second locating device (5), in particular a target-tracking device, which, after the first position of the assault ammunition body (4) is determined by the first locating device (12), receives the transmitted location data and carries out the measurement required to determine the trajectory of the assault ammunition body (4).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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DE200710018507 DE102007018507B4 (en) | 2007-04-19 | 2007-04-19 | Method and apparatus for controlling an assault ammunition launcher |
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EP1983294A2 EP1983294A2 (en) | 2008-10-22 |
EP1983294A3 EP1983294A3 (en) | 2011-10-05 |
EP1983294B1 true EP1983294B1 (en) | 2013-02-13 |
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EP20080007446 Active EP1983294B1 (en) | 2007-04-19 | 2008-04-16 | Method and device for combating a launching position of an attack munition |
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WO2009023322A1 (en) | 2007-05-14 | 2009-02-19 | Raytheon Company | Methods and apparatus for selecting a target from radar tracking data |
DE102011109658A1 (en) | 2011-08-08 | 2013-02-14 | Rheinmetall Air Defence Ag | Device and method for protecting objects |
FR3002030B1 (en) | 2013-02-12 | 2017-08-11 | Nexter Systems | LIGHT ARMY SYSTEM |
FR3099823B1 (en) * | 2019-08-05 | 2021-12-03 | Gautier Investissements Prives | AUTONOMOUS AND INTELLIGENT DEFENSE SYSTEM |
DE102020007996A1 (en) | 2020-12-17 | 2022-06-23 | Atlas Elektronik Gmbh | Guidance system for aligning a barrel weapon |
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DE6609990U (en) * | 1964-07-16 | 1974-09-12 | Rheinstahl Ag | ARMORED VEHICLE EQUIPPED WITH A ROTATING TOWER. |
DE3733962A1 (en) * | 1987-10-08 | 1989-04-27 | Wegmann & Co | METHOD FOR AUTOMATIC TARGET CLASSIFICATION BY AGRICULTURAL AND WATER COMBATING VEHICLES AND DEVICE FOR CARRYING OUT SAID METHOD |
DE4204217C2 (en) * | 1992-02-13 | 2000-05-25 | Krauss Maffei Wegmann Gmbh & C | Combat vehicle with turret and missile launchers |
DE19610770A1 (en) * | 1996-03-19 | 1997-09-25 | Juergen Dipl Ing Fryen | Automatic, unmanned system-object person monitoring analysis and defence system |
DE19626645A1 (en) * | 1996-03-19 | 1997-12-04 | Juergen Fryen | Automatic system for continuous discovery, measurement and following of movable object tracks |
DE19638968A1 (en) * | 1996-09-23 | 1998-03-26 | Reinhold Ficht | Fighting method for approaching flying object |
DE19753752C1 (en) * | 1997-12-04 | 1999-07-29 | Eurocopter Deutschland | Device and method for determining the point of impact of a ballistic missile |
US6584881B1 (en) * | 2001-03-26 | 2003-07-01 | United Defense Lp | Multi-purpose missile launcher system for a military land vehicle |
GB2380244B (en) * | 2001-08-13 | 2006-02-15 | Joseph Zabrana Michael | Automated Sound Missile and Associated Defence System |
SE520373C2 (en) * | 2001-09-18 | 2003-07-01 | Alvis Haegglunds Ab | For a military vehicle, the weapon tower is equipped with a medium-caliber automatic weapon and a relatively coarse-caliber weapon. |
DE10247350A1 (en) * | 2002-10-10 | 2004-04-22 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Device for protection against munitions designed as guided missiles e.g. for protection of military vehicles and buildings, has all warning sensors for detection and acquisition and active defence devices arranged on common carrier |
DE10331523A1 (en) * | 2003-07-11 | 2005-02-10 | Küsters, Manfred | Hazard detection and defense system |
DE10337642B4 (en) * | 2003-08-16 | 2007-08-02 | Kraus-Maffei Wegmann Gmbh & Co. Kg | Modular weapon station, in particular for placement on a combat vehicle |
IL161487A (en) * | 2003-10-09 | 2008-11-26 | Elbit Systems Ltd | Multiple weapon system for an armored vehicle |
US20060283317A1 (en) * | 2004-07-16 | 2006-12-21 | Trex Enterprises Corp | Missile protection system for vehicles |
DE102004038264A1 (en) * | 2004-08-06 | 2006-03-16 | Diehl Bgt Defence Gmbh & Co. Kg | Self protection method, involves aligning main armaments, connected with defense grenade, to firing point of attacking projectile after interception of instantaneous threat, where point is determined by tracing dynamic data of projectile |
US7151478B1 (en) * | 2005-02-07 | 2006-12-19 | Raytheon Company | Pseudo-orthogonal waveforms radar system, quadratic polyphase waveforms radar, and methods for locating targets |
DE102005023739A1 (en) * | 2005-05-17 | 2006-12-07 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method for determining a Feuerleitlösung |
DE102007007403A1 (en) | 2007-02-12 | 2008-08-21 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Method and device for protection against flying attack ammunition |
-
2007
- 2007-04-19 DE DE200710018507 patent/DE102007018507B4/en not_active Expired - Fee Related
-
2008
- 2008-04-16 EP EP20080007446 patent/EP1983294B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
DE102007018507A1 (en) | 2008-10-23 |
DE102007018507B4 (en) | 2012-05-03 |
EP1983294A3 (en) | 2011-10-05 |
EP1983294A2 (en) | 2008-10-22 |
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