EP3377840A1 - Remotely controllable weapon station and method for operating a remotely controllable weapon station - Google Patents
Remotely controllable weapon station and method for operating a remotely controllable weapon stationInfo
- Publication number
- EP3377840A1 EP3377840A1 EP16778410.7A EP16778410A EP3377840A1 EP 3377840 A1 EP3377840 A1 EP 3377840A1 EP 16778410 A EP16778410 A EP 16778410A EP 3377840 A1 EP3377840 A1 EP 3377840A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- weapon
- point
- display system
- pixel
- target
- 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 description 19
- 238000003860 storage Methods 0.000 claims description 18
- 238000004590 computer program Methods 0.000 claims description 6
- 230000004044 response Effects 0.000 claims description 5
- 230000008859 change Effects 0.000 claims description 4
- 238000012423 maintenance Methods 0.000 claims description 4
- 230000007613 environmental effect Effects 0.000 claims description 3
- 238000003909 pattern recognition Methods 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 3
- 238000001931 thermography Methods 0.000 claims description 3
- 238000007598 dipping method Methods 0.000 claims description 2
- 230000003287 optical effect Effects 0.000 abstract description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- 238000010586 diagram Methods 0.000 description 6
- 238000010304 firing Methods 0.000 description 3
- VVNCNSJFMMFHPL-VKHMYHEASA-N D-penicillamine Chemical compound CC(C)(S)[C@@H](N)C(O)=O VVNCNSJFMMFHPL-VKHMYHEASA-N 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 229940075911 depen Drugs 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000008021 deposition Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 230000004807 localization Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000001454 recorded image Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/14—Indirect aiming means
- F41G3/142—Indirect aiming means based on observation of a first shoot; using a simulated shoot
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/06—Aiming or laying means with rangefinder
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/14—Indirect aiming means
- F41G3/16—Sighting devices adapted for indirect laying of fire
- F41G3/165—Sighting devices adapted for indirect laying of fire using a TV-monitor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G5/00—Elevating or traversing control systems for guns
- F41G5/14—Elevating or traversing control systems for guns for vehicle-borne guns
- F41G5/20—Elevating or traversing control systems for guns for vehicle-borne guns for guns on ships
- F41G5/22—Elevating or traversing control systems for guns for vehicle-borne guns for guns on ships to compensate for rolling or pitching
Definitions
- the present invention relates to a remotely operable weapon station having a weapon which is directionally mounted in azimuth and elevation in a carriage for controlling a target object. Furthermore, the present invention relates to a military vehicle with such a remote-controlled weapon station as ⁇ a method for operating a remote-controlled weapon station.
- Such remote-controlled weapon stations are known for example from DE 10 2011 050 277 AI and DE 10 2006 034 689 AI. It can be delivered from the remote-controlled weapon station single shots or salvos.
- a remote weapon station ⁇ which comprises a control device having a display device and a memory device.
- the display shows a stored at ⁇ view a target device and the storage device stores the infor- nen on the shelf between the firing line (Line of Fire L ⁇ F!) And the view ⁇ line (Line of Sight; LOS).
- a disadvantage of the conventional solutions is that the filing must be manually determined and corrected by the operator or user of the remote-controlled weapon station. This disadvantageously results in a certain inaccuracy in the determination of the storage. Furthermore, this is time consuming, fetr -prone and the tray can not be determined in real time and corrects the ⁇ .
- an object of the present invention is to provide an improved remote-operated weapon station.
- a remotely operable weapon station with a weapon for fighting a target object is proposed, which is directionally mounted in a mount in azimuth and elevation.
- the remote control weapon station comprises a display system for the optical display of a target region of the WAF ⁇ fe, a first unit for determining an image point of a target impact point of a projectile of the gun shown on the display system, a second A ⁇ unit for determining an image point displayed on the display system ei ⁇ nes actual impact point in dependence on down by means of a holding device taken image data of the actual impact point of the projectile, and a third a ⁇ unit for determining a storage of the gun in response to the limited hours ⁇ th pixel of the target impact point and the particular Pixel of the actual meeting point on the display system.
- the current filing of the weapon can be automatically determined and taken over by the fire control computer for controlling the weapon of fernbe ⁇ servable weapon station.
- the first unit, the second unit and the third unit can calculate the tray together in real time or ⁇ determined.
- a further advantage is that no additional aids, such as a target, are needed to Be ⁇ humor of the tray.
- MLG-27 system Marine light-gun
- the adjusted firing the shot Pa ⁇ parameters uses the ship via data interface for firing transmitted ⁇ th data in order to calculate at what point on the adosys ⁇ system or screen the projectile on the water surface should occur (target meeting point of the projectile).
- This theoretical meeting point or desired meeting for example determined by the pixel coordinates on the image ⁇ screen of the display system is compared with the actual meeting point of the Geschos ⁇ ses (actual meeting point) corresponding to the pixel coordinates on the screen of the Ad ⁇ weighing system.
- the determination of the tray may now take place preferably by means of a delta calculation of the pixel coordinates and their conver ⁇ voltage in milliradians. The resulting result indicates, in particular, what specific storage is present at the present weapon station.
- the remote-controlled weapon station is arranged in particular on a military vehicle.
- the military vehicle is, for example, a warship.
- Conswei ⁇ se the command center of the warship comprising a fire control computer by means of which the weapon station can be operated remotely.
- the target object is, for example, an enemy military vehicle, for example an enemy warship.
- the weapon is protected, for example a marine ⁇ .
- the respective unit for example the first unit, can be implemented in hardware and / or software technology.
- the respective technical unit can be configured as a device or as part of a device, such as a computer or a microprocessor, or as a fire control computer ⁇ .
- the respective unit may be embodied as a computer program product, as a function, as a routine, as part of a program code, or as an executable object.
- the display system comprises a screen, for example a touch screen, and a user interface with input means for inputting commands for the display system.
- the display system is connected to a number of cameras which record the surroundings of the weapon.
- the third unit is adapted to determine the Abla ⁇ ge of the weapon based on a difference between the pixel of the target meeting point and the pixel of the actual meeting point on the display system.
- the weapon station is mounted on a clothes and eq ⁇ step vehicle
- the first unit is adapted to control the image point of the target impact point on the display system in dependence of weapons fenspezifischen parameters of vehicle-specific parameters and / or ambient parameters to determine.
- the arms specific Para ⁇ meter comprise a target distance of the target object, a target physical expansion of the target object, a type and / or a dispersion of an ammunition used in the weapon, a variance in a mechanism of the weapon and / or at least a maintenance parameters of the weapon ,
- the environmental parameters and the above-mentioned ship parameters are used.
- the surcharge removal of the missiles theoretically determined is preferably used as ei ⁇ ne base size.
- ⁇ is preferably not greater than 2, because otherwise the error-free automated localization of the impact position of Kalibrierschüssen, i.e. the entste characterized ⁇ Henden water fountains, is not optimal.
- templates or reference templates of typical water fountains can be deposited and used in impacts of projectiles in the water in a database.
- the gun is warmed up with a number of shots before the deposit is determined. This number is for example 5.
- the system is preferential ⁇ , in a manual mode is set and the gun in a given ele- vation / set azimuth position.
- no stabilization is selected and no target is tracked. Consequently, preferably no dynamic derivative is calculated.
- a swirl file is preferably taken into account.
- the system is placed in the HP (High Precision) Fire mode.
- the weapon station further comprises a laser rangefinder for determining the distance of the target Zielob ⁇ jekts.
- the vehicle-specific parameters comprise a course of the vehicle, a speed of the vehicle, a respective waves a parameter, a parameter concerning a Schwoien, a respective a dive parameter, a rolling concerned Para ⁇ meter, a respective pitching Parameters and / or a yaw-related parameter.
- the receiving device comprises a camera, a thermal imaging camera, a radar device and / or a sonar device.
- the pixel of the target impact point comprises on the display system, a pixel or a surface of a multi ⁇ number of pixels and / or pixel of the actual impact point on the adosys ⁇ system includes one pixel or a surface of a plurality of pixels.
- the second unit is set up to determine the image point of the actual meeting point on the display system based on pattern recognition using the image data recorded by the recording device and reference templates for projectile impacts stored in a database.
- the costs associated with the impact of the bullets on the water fountain water ⁇ have a typical character and can be saved as templates or refer- ence templates in the database for automatic recognition and position ⁇ determination.
- the third unit is configured to determine an azimuth bin and elevation bin based on the determined pixel of the target hitting point and the particular pixel of the actual hitting spot on the display system.
- the third unit is adapted for determining the azimuth storage to the elevation angle in each case by a predetermined at a plurality M of successive shots by the weapon folic constricting respectively to 0 ° devisstel ⁇ len and the azimuth angle each to determine number of degrees to changed ⁇ countries a value for the azimuth storage to each of the successive shots based on the determined image point of the target meeting place and on the particular pixel of the actual impact point on the display system, and the azimuth storage using a applied to the M values for the azimuth storage probabilistic method to determ ⁇ men.
- the third unit is adapted for determining the elevation shelf to the azimuth angleiser respectively to 270 ° represent at a plurality M of successive shots by the weapon ⁇ and the elevation angle in each case by a predetermined number of degrees to change to respectively determine a value for the elevation tray to each of the on ⁇ successive shots based on the determined image point of the desired impact point, and on the determined image point of the actual impact point on the To ⁇ pointing system, and the elevation shelf to determine using the M values applied for the elevation shelf probabilistic Ver ⁇ driving.
- a military vehicle which has a number N of remote-controlled weapon stations according to the first aspect, with N> 1.
- the military vehicle is, for example, a warship.
- the military vehicle may also be a land vehicle, such as a tank, in particular a remote-controlled tank.
- a method for operating a remote sign ⁇ dienbaren weapon station with a weapon for fighting a target object, wel ⁇ che is mounted directable in a mount in azimuth and elevation, and proposed a display system for visual representation of a target area of the weapon , The method comprises the following steps
- a computer program product which initiates the execution of the method according to the third aspect as explained above on a program-controlled device.
- a computer program product such as a computer program means, for example, as a storage medium, such as memory card, USB stick, CD-ROM, DVD, or in the form of a downloadable file provided by a server in ei ⁇ nem network or delivered. This can be done, for example, in a wireless communication network by the transmission of a corresponding file with the computer program product or program Computerpro ⁇ agent.
- Fig. 1 shows a schematic block diagram of a first embodiment ⁇ example of a remote-controlled weapon station
- Fig. 2 shows a schematic block diagram of a second embodiment of an execution ⁇ remotely controllable weapon station
- Fig. 3 to 7 show schematic views of a display system at a succession of shots to determine the azimuth storage!
- FIGS. 8 to 12 are schematic views of a display system in a sequence of shots for determining the elevation tray!
- Fig. 13 shows a schematic flow diagram of an exemplary embodiment of a method for operating a remote-controllable Waf ⁇ fenstation.
- Fig. 1 is a schematic block diagram of a first embodiment of a remote-controlled weapon station 1 is shown.
- the remote control weapon ⁇ station 1 comprises a gun 2 for controlling a target object, which is mounted orientable in elevation and azimuth in a carriage.
- the remote-controlled Waf ⁇ fenstation 1 is installed in particular on a military vehicle.
- the military vehicle may include a plurality of remotely operable weapon stations 1.
- the military vehicle is, for example, a warship.
- the remotely operable weapon station 1 comprises a display system 4 for visualizing a target area of the weapon 2.
- the display system 4 is exemplified as a screen on which the horizon, a target Z and a bullet impact G are shown.
- the projectile impact G is exemplified as a water fountain.
- Tl denotes a pixel of a target impact point of a Ge ⁇ lap of the weapon 2 and T2 an image point of an actual impact point of the Geschos- ses of the gun 2.
- the remote weapon station 1 includes a first unit 5, a second unit 6 which is coupled to a receiving device 7, and a third unit 8.
- the first unit 5, the second unit 6 and the third A ⁇ unit 8 are in particular in a Fire control computer 9 of the weapon station 1 integrated.
- the first unit 5 is adapted to Darge on the display system 4 ⁇ presented pixel Tl of the target impact point of the bullet of the gun 2 to be agree ⁇ .
- the second unit 6 can be coupled to the recording device 7 and is further configured to receive image data BD of the actual meeting point of the projectile picked up by the recording device 7.
- the actual meeting point of the projectile and in particular corresponds to the projectile impact G of Fig. 1.
- the second unit 6 is adapted to the image point T2 of the shown on the display system 4 actual impact point in depen ⁇ dependence of the recorded by the recording means 7 To determine image data BD.
- the third unit 8 is adapted to a tray, in particular an azimuth tray and an elevation tray, the weapon 2 as a function of the ⁇ voted pixel Tl of the target meeting point on the display system 4 and of the specific pixel T2 of the actual Meeting point on the display system 4 to determine.
- the third unit 8 is particularly adapted to the exhaust of the weapon 2 would be based on a difference between the image point Tl of the target impact point and the image point T2 of the actual impact point to be determined on the adosys ⁇ tem. 4
- the difference can be, for example, a difference vector, in particular a two-dimensional or a three-dimensional difference vector.
- the first unit 5 is a directed to determine the pixel Tl of the desired impact point on the display system 4 in response to force-specific parameters, vehicle-specific Pa ⁇ rametern and / or ambient parameters.
- the environmental parameters are meteorological data such as ambient temperature, wind direction and wind force.
- weapon-specific parameters are the target distance of the target Z or the target object, a physical target extent of the target object, a type and / or a scatter of ammunition used in the weapon 2, a variance in a mechanics of the weapon 2 and / or maintenance parameters of the weapon , as in ⁇ example maintenance intervals.
- Examples of the vehicle-specific parameters comprise a course of driving ⁇ zeugs, for example, a ship course, a speed of the vehicle, a a surge parameter concerned, a a Schwoien concerned Pa ⁇ parameters, concerning a dipping parameter, a rolling relate ⁇ parameter, a pound-related parameter and / or a yaw-related parameter.
- the recording device 7, which is coupled to the second unit 6, comprises, for example, a camera, a thermal imaging camera, a radar device and / or a sonar device.
- the pixel T1 of the target meeting point on the display device 4 is, for example, a pixel or an area of a plurality of pixels. Accordingly, the pixel T2 of the actual meeting point on the display system 4 is also a pixel or an area of a plurality of pixels.
- FIG. 2 shows a schematic block diagram of a second embodiment of a remote-controlled weapon station 1.
- the second embodiment of Fig. 2 of the remote-controlled weapon station 1 includes all of the features of the first embodiment of Fig. 1.
- ⁇ from the weapon station 1 of FIG. 2 includes a database 10 for storing reference template RT for projectile impacts G.
- the second unit 6 of Fig. 2 is adapted to the image point T2 of the actual impact point on the display system 4 based on a pattern recognition un ⁇ ter using the captured by the pickup means 7 Jardinda ⁇ th BD and stored in the database 10 reference Templates RT for the projectile impacts G to determine.
- the third unit 8 is set up to determine an azimuth bin ⁇ and an elevation bin ⁇ based on the determined pixel Tl of the target hitting point and on the specific pixel T2 of the actual hitting spot on the display system 4.
- the third unit 8 for determining the azimuth offset ⁇ is set up to set the elevation angle in each case to 0 ° and to change the azimuth angle in each case to a predetermined number of degrees in the case of a plurality M of successive shots by the weapon 2, respectively determine a value for the azimuth map ⁇ for each of the successive shots based on the determined pixel Tl of the target hitting point and on the designated pixel T2 of the actual hitting point on the display system 4 and the azimuth map ⁇ using a agree applied to the M values for the azimuth storage probabilistic method to be ⁇ .
- the elevation angle is set to 0 ° and the azimuth angle is set to five different angles. In the example shown in FIGS. 3 to 7, these are the azimuth angles 285 °, 275 °, 270 °, 265 ° and 255 °.
- a shot is fired and the actual meeting point according to the pixel T2 of the actual meeting point is compared with the theoretical meeting point according to the pixel Tl of the target meeting point on the basis of the pixel positions present in the display system 4.
- the statistically most likely azimuth storage ⁇ is taken from the five, in particular ⁇ special converted into millirad present values as offset value from the fire control computer 9.
- the sequence of the five shots of the ship's course for the example of a ship as a military vehicle is to be selected preferably so that the meteorological ⁇ specific wind either in the weft direction or the weft direction (no cross wind).
- the ship's speed and heading should preferably be kept constant throughout the determination of the five values for the azimuth track ⁇ .
- a ship speed speed Zvi ⁇ rule nodes 10 and 20 is preferably selected.
- the elevation angle for five consecutive shots is set to the following shot angle: -1 °; -0.5 °; 0 °; + 0.5 °; and + 1 °.
- Determining the elevation tray is, as stated above, the azimuth angle, for example, set to 270 °. Under any angle setting for the Elevation angle is given a shot and the actual meeting point according to the pixel Tl is compared with the theoretical meeting point according to the pixel T2 on the display system 4 on the basis of the present pixel positions. An example of this is shown in the schematic views of the display system 4 according to FIGS. 8 to 12.
- Fig. 13 shows a schematic flow diagram of an embodiment ei ⁇ nes method of operating a remotely controllable weapon station 1. Examples of the remote weapon station 1 are shown in Figs. 1 and 2.
- the embodiment of the method according to FIG. 13 comprises the following steps 1301, 1302 and 1303:
- a pixel Tl of a target hit point of a projectile of the weapon 2 shown on the display system 4 is determined.
- a pixel T2, represented on the display system 4, of an actual meeting point of the projectile is determined by means of a recording system. Means 7 recorded image data BD of the actual meeting point of Geschos ⁇ ses determined.
- a tray in particular comprising an azimuth storage ⁇ and an elevation tray ⁇ , the gun 2 in response to the be ⁇ voted pixel Tl of the desired impact point on the display system 4 and of the determined image point T2 of the actual Meeting point on the display system 4 be ⁇ true.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102015120036.8A DE102015120036A1 (en) | 2015-11-19 | 2015-11-19 | Remote weapon station and method of operating a remote weapon station |
PCT/EP2016/074169 WO2017084806A1 (en) | 2015-11-19 | 2016-10-10 | Remotely controllable weapon station and method for operating a remotely controllable weapon station |
Publications (3)
Publication Number | Publication Date |
---|---|
EP3377840A1 true EP3377840A1 (en) | 2018-09-26 |
EP3377840B1 EP3377840B1 (en) | 2022-01-26 |
EP3377840B9 EP3377840B9 (en) | 2022-04-20 |
Family
ID=57113366
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16778410.7A Active EP3377840B9 (en) | 2015-11-19 | 2016-10-10 | Remotely controllable weapon station and method for operating a remotely controllable weapon station |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP3377840B9 (en) |
DE (1) | DE102015120036A1 (en) |
HU (1) | HUE059023T2 (en) |
WO (1) | WO2017084806A1 (en) |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19716199A1 (en) * | 1997-04-18 | 1998-10-22 | Rheinmetall Ind Ag | Procedure for aiming the weapon of a weapon system and weapon system for implementing the method |
US6125308A (en) * | 1997-06-11 | 2000-09-26 | The United States Of America As Represented By The Secretary Of The Army | Method of passive determination of projectile miss distance |
US20080022575A1 (en) * | 2006-05-08 | 2008-01-31 | Honeywell International Inc. | Spotter scope |
DE102006034689A1 (en) | 2006-07-24 | 2008-01-31 | Rheinmetall Landsysteme Gmbh | Protective device for a military vehicle, which acts as a support vehicle and can carry out all pioneering and mining work |
US8074555B1 (en) * | 2008-09-24 | 2011-12-13 | Kevin Michael Sullivan | Methodology for bore sight alignment and correcting ballistic aiming points using an optical (strobe) tracer |
KR101472445B1 (en) | 2010-12-09 | 2014-12-12 | 삼성테크윈 주식회사 | Firearm system and method for contolling a firearm unit |
DE102011050277B4 (en) | 2011-05-11 | 2012-11-29 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Adapter for attaching a carriage to an object, mount and military vehicle |
FR2989456B1 (en) * | 2012-04-12 | 2018-05-04 | Philippe Levilly | TELEOPERATED TARGET PROCESSING SYSTEM |
DE102014019200A1 (en) * | 2014-12-19 | 2016-06-23 | Diehl Bgt Defence Gmbh & Co. Kg | automatic weapon |
-
2015
- 2015-11-19 DE DE102015120036.8A patent/DE102015120036A1/en not_active Ceased
-
2016
- 2016-10-10 HU HUE16778410A patent/HUE059023T2/en unknown
- 2016-10-10 WO PCT/EP2016/074169 patent/WO2017084806A1/en unknown
- 2016-10-10 EP EP16778410.7A patent/EP3377840B9/en active Active
Also Published As
Publication number | Publication date |
---|---|
DE102015120036A1 (en) | 2017-05-24 |
HUE059023T2 (en) | 2022-10-28 |
WO2017084806A1 (en) | 2017-05-26 |
EP3377840B9 (en) | 2022-04-20 |
EP3377840B1 (en) | 2022-01-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE3790614C2 (en) | ||
DE2411790B2 (en) | PROCEDURE AND WEAPON SYSTEM FOR COMBATING SURFACE TARGETS | |
DE102005007910A1 (en) | Firearm for long flight duration projectiles has fire guidance system with target data acquisition and adjusters for sight tube on weapon | |
EP1304539A1 (en) | Method and device for aiming a gun barrel and use of the device | |
EP0977003A1 (en) | Method for combating at least one aerial target by means of a fire group, fire group comprising at least two fire units and use of the fire group | |
DE2805903A1 (en) | FIRE CONTROL DEVICE FOR AN AIRPLANE DEFENSE WEAPON SYSTEM | |
DE102015007028A1 (en) | Method for focusing a high-energy beam on a breakpoint on the surface of a flying flying object | |
EP1314949A1 (en) | Method and device for assessing the aiming errors of a weapon system and use of the device | |
DE2936643A1 (en) | METHOD AND ARRANGEMENT FOR ESTIMATING THE ACCURACY OF A WEAPON | |
DE2658501A1 (en) | Anti-aircraft target training appts. - has disc computer for storing aircraft silhouettes projected onto rotating panoramic dome | |
DE1951622C3 (en) | Arrangement for the simulated display of firing trajectories | |
EP2803938A2 (en) | Method for designating the target for a missile launching installation | |
EP3350536B1 (en) | Remotely controllable weapon station and method for operating a controllable weapon station | |
EP3377840A1 (en) | Remotely controllable weapon station and method for operating a remotely controllable weapon station | |
EP3034983B2 (en) | Automatic gun | |
EP0154809A1 (en) | Method for simulating combat | |
EP4229352A1 (en) | Determination of a fire guidance solution of an artillery weapon | |
EP1159578B1 (en) | Shooting simulation method | |
DE102013111644A1 (en) | Method for controlling a directable weapon of a vehicle during firing exercises | |
EP3350534B1 (en) | Remotely controllable weapon station and method for operating a controllable weapon station | |
WO1992018824A1 (en) | Method and device for displaying shot deviations in a gunner's sight | |
EP3367045A1 (en) | Method and device for improving the precision of fire guidance solutions | |
EP3593081A1 (en) | Simulator and method for simulating a deployment of a missile | |
EP3350535B9 (en) | Weapon station that can be operated remotely and method for operating a remotely operatable weapon station | |
DE102018128517A1 (en) | Remote-controlled weapon station and method for operating a remote-controlled weapon station |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
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 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20180313 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20200130 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F41G 3/14 20060101AFI20210720BHEP Ipc: F41G 3/06 20060101ALI20210720BHEP Ipc: F41G 3/16 20060101ALN20210720BHEP Ipc: F41G 5/22 20060101ALN20210720BHEP |
|
INTG | Intention to grant announced |
Effective date: 20210810 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1465591 Country of ref document: AT Kind code of ref document: T Effective date: 20220215 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502016014465 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PK Free format text: BERICHTIGUNG B9 |
|
REG | Reference to a national code |
Ref country code: RO Ref legal event code: EPE |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: FP |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG9D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220526 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220426 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220427 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220526 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502016014465 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: HU Ref legal event code: AG4A Ref document number: E059023 Country of ref document: HU |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed |
Effective date: 20221027 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20221031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221010 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221031 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221031 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221010 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20231019 Year of fee payment: 8 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 1465591 Country of ref document: AT Kind code of ref document: T Effective date: 20221010 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20231020 Year of fee payment: 8 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221010 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: RO Payment date: 20231003 Year of fee payment: 8 Ref country code: HU Payment date: 20231024 Year of fee payment: 8 Ref country code: DE Payment date: 20231020 Year of fee payment: 8 Ref country code: CZ Payment date: 20231004 Year of fee payment: 8 Ref country code: BG Payment date: 20231020 Year of fee payment: 8 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220126 |