WO2022083822A1 - Détermination de solution de guidage de tir d'arme d'artillerie - Google Patents

Détermination de solution de guidage de tir d'arme d'artillerie Download PDF

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Publication number
WO2022083822A1
WO2022083822A1 PCT/DE2021/100806 DE2021100806W WO2022083822A1 WO 2022083822 A1 WO2022083822 A1 WO 2022083822A1 DE 2021100806 W DE2021100806 W DE 2021100806W WO 2022083822 A1 WO2022083822 A1 WO 2022083822A1
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WO
WIPO (PCT)
Prior art keywords
weapon
target
account
fire control
artillery
Prior art date
Application number
PCT/DE2021/100806
Other languages
German (de)
English (en)
Inventor
Dr. Axel Scheibel
Matthias Czok
Original Assignee
Krauss-Maffei Wegmann Gmbh & Co. Kg
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 Krauss-Maffei Wegmann Gmbh & Co. Kg filed Critical Krauss-Maffei Wegmann Gmbh & Co. Kg
Priority to KR1020237014098A priority Critical patent/KR20230106595A/ko
Priority to AU2021366077A priority patent/AU2021366077A1/en
Priority to CA3193896A priority patent/CA3193896A1/fr
Priority to EP21799175.1A priority patent/EP4229352A1/fr
Priority to IL301614A priority patent/IL301614A/en
Priority to US18/032,275 priority patent/US20230392899A1/en
Publication of WO2022083822A1 publication Critical patent/WO2022083822A1/fr

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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
    • F41G3/20—Indirect aiming means specially adapted for mountain artillery
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/02—Aiming or laying means using an independent line of sight
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A17/00—Safety arrangements, e.g. safeties
    • F41A17/08—Safety arrangements, e.g. safeties for inhibiting firing in a specified direction, e.g. at a friendly person or at a protected area
    • 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
    • F41G3/12—Aiming or laying means with means for compensating for muzzle velocity or powder temperature with means for compensating for gun vibrations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/22—Aiming or laying means for vehicle-borne armament, e.g. on aircraft
    • 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
    • F41G5/24—Elevating or traversing control systems for guns for vehicle-borne guns for guns on tanks

Definitions

  • the present invention relates to methods for determining a fire control solution of an artillery weapon in indirect ballistic fire to hit a target. Further objects of the invention are a fire control system for determining a fire control solution for an artillery weapon in indirect ballistic fire to hit a target and an artillery weapon system with an artillery weapon for combating a target in indirect ballistic fire.
  • a fire control equation is used which, when solved, provides a fire control solution according to which the weapon can be aimed in order to be able to engage the target.
  • a fire control system is usually used, which enables the fire control solution to be determined automatically.
  • the artillery weapon systems have one of the most important support functions in modern military conflicts. As flexible systems, they can be used both offensively and defensively. The precision of the artillery weapons of such artillery weapon systems has increased significantly in the past. Modern weapon systems, thanks to high manufacturing quality, the use of the latest ammunition and improved fire control technology, enable high hit accuracy. Above all, this makes it possible to minimize collateral damage and avoid endangering your own or allied forces.
  • artillery weapons attack a target using indirect ballistic fire.
  • the ballistic projectile is fired from the artillery weapon in the lower or upper angle group, ie with an angle increase of up to 65°, which is also referred to as vertical fire.
  • direct-firing weapons have a direct line of sight between the weapon and the target, so that the target can be seen from the weapon and directly relative to it in the coordinate system of the direct-firing weapon, such a direct line of sight does not exist with artillery weapons.
  • the target is rather obscured by visual obstacles or because of the great distance covers the curvature of the earth.
  • the term "non-line-of-sight" conditions is therefore also used.
  • the object of the present invention is therefore to increase the survivability of the artillery weapon and its operating crew, especially during a firefight in which the weapon fires on a target and is itself exposed to return fire.
  • this task is solved in that a changing weapon position of the weapon and a target position of the target are taken into account as geographic position data.
  • the fire control solution is determined taking into account the changing weapon position of the weapon and the target position of the target as geographic position data.
  • the geographic position data can be recorded in the form of geographic coordinates, for example in the form of degrees of latitude and longitude.
  • the fire control solution can be determined while the weapon is moving.
  • the preparation for indirect firing while moving can also be done in this way while moving.
  • the ability to fire indirectly while on the move can lead to a reduction in the reaction time between receiving a fire order via a guidance system and implementing the fire order as part of an adapted fire command after determining the fire control solution in combination with a minimized vulnerability of the weapon.
  • At least one absolute parameter that is independent of the relative position and/or relative location of the weapon and the target is preferably taken into account. By taking an absolute parameter into account, it is possible to take into account parameters that are independent of the relative position and/or relative orientation of the weapon and the target and that influence the fire control solution when determining the fire control solution.
  • the at least one absolute parameter can be determined in an absolute coordinate system that does not depend on the position of the weapon and/or the target, or it can be determined as a value on an absolute scale.
  • Such an absolute parameter can thus be independent of the relative position of the weapon and the target to one another and/or the relative location of the weapon and the target to one another, ie it is affected by a change in the position and/or location of the weapon in relation to the target just as irrelevant as a change in the position and/or location of the target in relation to the weapon.
  • an absolute terrain height of the weapon position, an absolute terrain height of the target position, an absolute time and/or an absolute system parameter of the weapon are taken into account as absolute parameters.
  • the absolute height of the terrain of the weapon position and/or the target position can be determined as the height difference of the weapon position or the target position compared to a zero level.
  • topographical map material and/or topographical measuring instruments can be used to determine the absolute height of the terrain.
  • the same zero level can be used.
  • parameters entering the fire control equation which are determined at different times, at different locations and/or by different system components, can be calculated in a consistent time- borrowed connection take place.
  • the absolute time can serve as a time standard to which reference is made when determining the other parameters that are included in the fire control equation.
  • the long distances involved in indirect ballistic fire of artillery weapons can result in significant transmission and acquisition times. Influences of acquisition and/or transmission times can be taken into account by means of the absolute time.
  • Parameters that exist at the same time but are present at different times due to the acquisition and/or transmission times can be synchronized with one another using the absolute time and used as synchronous parameters for determining the fire control solution.
  • the absolute time can be taken into account as a time stamp, in particular in decentrally organized system components for determining the parameters.
  • the absolute temperature of the propellant, the shape of the projectile, the weight of the projectile, the caliber of the weapon, the draft profile of the weapon and/or the rifling of the weapon can be taken into account as absolute system parameters of the weapon.
  • a movement dynamics of the weapon and a movement dynamics of the target are taken into account.
  • a fire control solution for hitting a moving target with a moving artillery weapon in indirect ballistic fire can be determined.
  • the consideration of the movement dynamics makes it possible, in addition to constant, linear movements of the weapon and/or the target, to also take into account changes in the movement speed and direction of movement of the weapon and/or the target.
  • the method can also be used to find a fire control solution for a for a stationary artillery weapon to hit a stationary target, for a stationary artillery weapon to hit a moving target, and for a stationary artillery weapon to hit a stationary target.
  • the functionality of the known determination methods of a fire control solution can be covered with this method, so that this method can not only supplement known determination methods, but can completely replace them.
  • the movement of the target can be extrapolated from the previously recorded movement dynamics of the target.
  • the movement dynamics in absolute coordinates they can be taken into account independently of the relative position and/or the relative location of the weapon and the target to one another.
  • the movement dynamics of the weapon and the movement dynamics of the target can be taken into account with the absolute coordinates without being influenced by a change in the target position or the weapon position.
  • the movement dynamics of the weapon and the movement dynamics of the target can in each case be the movement behavior, in particular the entirety of the previously recorded movements, of the weapon or of the target.
  • the movement dynamics are recorded in indirectly referenced coordinate systems.
  • the movement dynamics recorded in indirectly referenced coordinate systems can be related to each other without the coordinate system in which the movement dynamics is recorded directly on the coordinate system in which the other movement dynamics is detected, is referenced. Since there is no line of sight between the weapon and the target in indirect ballistic fire, the coordinate systems of the weapon and the target cannot be directly referenced to each other.
  • the movement dynamics recorded in different coordinate systems can be related to one another, in particular in absolute coordinates, even without a direct line of sight.
  • two coordinate systems can be related to one another.
  • two, in particular moving, coordinate systems can be related to one another without there being a direct line of sight between them.
  • a further embodiment provides that a detection system is used to detect the target.
  • the acquisition system can also allow acquisition of the target without a direct line of sight between the weapon and the target.
  • the detection system can be an independent system that is separate from the weapon and, in particular, independent of the weapon, for example a satellite, a drone, a UAV, an unmanned land vehicle, an observation post, a vehicle-based target detection system and/or an infantry target detection system.
  • the target and in particular the target position relative to the detection system can be detected from a coordinate system linked to the detection system.
  • the detection system can use one or more detection signals to detect the target.
  • the detection signal can be, for example, radar radiation reflected by the target, infrared radiation emitted by the target or light reflected by the target, with which the detection system can detect the target.
  • the movement dynamics of the detection system are preferably taken into account when determining the fire control solution.
  • an absolute detection system position of the detection system is used when referencing the coordinate systems indirectly.
  • the target's coordinate system can be directly referenced to the acquisition system coordinate system located at the acquisition system position.
  • the coordinate system of the detection system located at the detection system position can in turn be referenced directly or indirectly via further coordinate systems to the coordinate system of the weapon.
  • the coordinate system of the target can be indirectly referenced to the coordinate system of the weapon via the coordinate system of the detection system.
  • the coordinate system of the weapon can be indirectly referenced to the coordinate system of the target or the coordinate systems of the weapon and the target can be indirectly referenced to another coordinate system.
  • referencing the coordinate systems they can be related to one another in such a way that the positions and directions recorded in a first coordinate system can be transformed into the other coordinate system without loss of information.
  • several corresponding positions in particular at least three, can be recorded from both coordinate systems.
  • the properties of the detection system are taken into account.
  • Characteristics of the detection system to be taken into account can be, for example, the processing time from receipt to the forwarding of a detection signal by the detection system to the weapon, the propagation time of the detection signal from the target to the detection system, the propagation time of a forwarded signal from the system to the weapon, the movement of the detection system and/or the movement dynamics of the detection system.
  • the accuracy in determining the fire control solution can be further improved by also taking into account properties of the detection system when determining the fire control solution.
  • At least one artillery-relevant influencing parameter in particular vibrational influences of the weapon, vibrational influences of a weapon carrier and/or a firing time development, is taken into account.
  • Artillery-relevant influencing parameters can have an impact on the internal ballistics and/or the external ballistics in indirect ballistic fire.
  • the influencing parameters relevant to artillery can be described statistically, in particular the vibration influences of the weapon and/or the vibration influences of the weapon carrier.
  • the weapon carrier can hold the weapon as such and enable it to be moved in the field, with the weapon carrier being able to be, for example, a chassis or an armored hull. Together with the weapon, the weapon carrier forms part of a weapon system.
  • vibrations of the weapon carrier relative to the surrounding terrain as well as vibrations of the weapon relative to the weapon carrier can occur. Vibrations of the weapon as well as those of the weapon carrier can affect the fire control solution, whereby both constructive and destructive interferences of the respective vibrations can occur. By taking into account the vibration effects of the weapon and the vibration effects of the weapon carrier, these interferences can also be taken into account.
  • the acceleration time of the projectile can be taken into account. In addition to pure acceleration The acceleration behavior of the projectile can also be taken into account as a further artillery-related influencing parameter.
  • the influencing parameter relevant to artillery in particular its effect on the fire control solution, is extrapolated.
  • extrapolating a statement can be made from the previous development of the at least one artillery-relevant influencing parameter about the size of this influencing parameter in the immediate and relevant future for determining the fire control solution.
  • At least one geographical interference parameter is taken into account to determine a projectile trajectory free of interference contours.
  • a projectile trajectory free of interference contours In addition to the topography of the area, i. H. the elevation of the earth's surface without vegetation and buildings, also includes other natural or artificially constructed geographical structures, such as vegetation or buildings.
  • geographical interference parameters in the area of the weapon position and in the area of the target position are taken into account, in particular exclusively, for determining the interfering contour-free projectile trajectory.
  • a trouble-free departure angle of the projectile from the weapon and a trouble-free approach angle of the projectile at the position of the target can be ensured.
  • the distance between the weapon position and the target position, the projectile flight time and/or the movement dynamics of the target can also be taken into account.
  • terrain modeling in particular continuous, takes place between the weapon position and the target position.
  • the terrain modeling which in addition to the topology can also contain the geographical disturbance parameters present in the terrain, can be used at any time and for any weapon position on a model of the terrain that reflects the real conditions.
  • the terrain modeling preferably takes place in a highly dynamic manner, so that a reliable terrain model can be provided even if there are changes in the direction of movement and movement speed of the weapon and/or the target.
  • Map material stored in a database of one or more maps can be used for terrain modeling.
  • the terrain modeling can take place between the weapon position assumed at the moment of modelling, as a quasi-static firing position during the movement of the weapon, and the current and/or extrapolated target position.
  • the extrapolated target position in the terrain model By including the extrapolated target position in the terrain model, it is easy to determine whether the bullet trajectory is free of interference contours, since the end point of the bullet trajectory is the extrapolated target position at which the target is likely to be when the bullet hits.
  • the calculated projectile trajectory By overlaying the calculated projectile trajectory with the terrain model, it can easily be determined whether geographical interference parameters are in the projectile trajectory. For this purpose it can be checked whether the calculated projectile trajectory and the surface of the terrain model intersect at one or more points between the weapon position and the target position.
  • at least one blocking parameter in particular a definable blocking area, is taken into account. By taking into account at least one blocking parameter, it is possible to prevent the weapon from being fired, as a result of which the projectile would pose an impermissible safety-related threat.
  • a restricted area, into which a projectile must not enter and/or in which a projectile must not impact, can be defined as a restricted parameter in a particularly simple manner.
  • a restricted area can be defined, for example, as an area around a civil defense facility, a hospital, your own field camp or your own units. If the consideration of at least one blocking parameter shows that firing would result in the blocking parameter being violated, a fire signal from the weapon can be interrupted, for example.
  • a definable restricted area can be designed to change over time and, for example, move along with moving own units.
  • no fire control solution is output, in particular as a result of the situation and/or time. Without the output of a fire control solution, the weapon cannot be fired, which is inadmissible due to the consideration of at least one blocking parameter.
  • the output of a fire control solution can be prevented depending on the blocking parameter depending on the situation and/or time, so that, for example, a blocking parameter is only valid with regard to a type of ammunition used, in a defined time window, from a defined point in time or up to a defined point in time.
  • the artillery weapon system has a damped weapon carrier for reducing vibrations during movement dynamics, in particular for filtering high-frequency vibrations. Vibration influences on the fire control solution can be reduced by the dampened weapon carrier, whereby the accuracy of the artillery weapon system can be increased in indirect ballistic fire while driving.
  • the weapon system has a hydraulic and/or electrical compensation system for compensating for vibrations of the weapon while driving.
  • the weapon is mounted with an unbalance-compensated weapon mount relative to the weapon carrier. Due to the unbalance-compensated weapon storage, the dynamics of the aiming movement of the weapon can be increased and the target can be attacked more quickly.
  • the weapon is preferably mounted at 360° relative to the weapon carrier, in particular in a turret system.
  • the weapon carrier can advantageously offer a large contact area in order to reduce tilting movements resulting from unevenness in the terrain and/or to allow the weapon to be fired in different directions relative to the weapon carrier without a support system, in particular in a horizontal angular range of 360° around the weapon carrier.
  • Fig. 1 shows a schematic view of a direct-firing weapon
  • Fig. 3 schematically the consideration of interference parameters when determining a fire control solution
  • FIG. 4 shows schematically the taking into account a blocking parameter when determining a fire control solution.
  • FIG. 1 there is a direct line of sight 7 between a direct-firing weapon 2 and the target 5 to be hit.
  • the movement of the target 5 in the target's own coordinate system K5 can be recorded in a simple manner from the weapon 2 with a direct line of sight 7 to the target 5 directly in the coordinate system K2 of the weapon 2 and used to determine the fire control solution.
  • the position and the movement of the target 5 are determined directly relative to the weapon 2 and, as such, relative positions and movements are also taken into account when determining the fire control solution.
  • the distance between the artillery weapon 2 and the target 5 to be hit is significantly greater than in the case of a direct-firing weapon, so that there is no direct line of sight between the weapon 2 and the target 5 .
  • the line of sight 7 of the artillery weapon 2 is rather interrupted by an interference parameter 12 .
  • This interference parameter 12 is indicated in FIG. 2 as a terrain elevation, but due to the very large distances it can also be caused by the curvature of the earth as such. Due to the lack of a direct line of sight between the weapon 2 and the target 5, the coordinate systems K2, K5 can no longer be related to one another, so that there are virtually two independent coordinate systems for the weapon 2 and for the target 5.
  • the changing weapon position P2 of the weapon 2 and the target position P5 of the target 5 are taken into account as geographic position data in the method according to the invention.
  • This information can be given, for example, according to the respective degrees of longitude and latitude, so that these are taken into account for a weapon position P2 and the target position P5 as geographic position data in an absolute coordinate system KA, which is not affected by the respective relative position of the weapon 2 and the target 5 to one another being affected.
  • the respective movement dynamics of the weapon 2 and the target 5 can also be taken into account when determining the fire control solution.
  • These movement dynamics can also be taken into account when determining the fire control solution in an absolute coordinate system KA, which can be, for example, the same coordinate system as was already used to determine the geographic position data.
  • the coordinate systems K2 and K5 must be referenced to one another, i.e. related to one another will. This can be done via a detection system 6 that is independent of the weapon 2 and with which the target 5 can be detected.
  • This detection system 6 can then be used to refer the coordinate systems K2, K5 to one another indirectly, even if there is no direct line of sight between the weapon 2 and the target 5.
  • This indirect referencing means that the two moving coordinate systems K2, K5 are related to one another.
  • This movement dynamics of the target 5 transformed into the absolute coordinate system KA can then be taken into account when determining the fire control solution.
  • the influences of these vibrations can be used as artillery-relevant influencing parameters in addition to the classic parameters for shooting from the move, such as the target distance, the wind and the air pressure, when determining the fire control solution of the weapon 2, are taken into account as additional statistical parameters.
  • these vibration influences of the weapon 2 and/or the weapon carrier 3 as well as other artillery-relevant influencing parameters, such as a firing time development can be precalculated by extrapolation.
  • a terrain model for example, can also be included in the prediction of these artillery-relevant influencing parameters and in particular the vibration influences, from which unevenness in the terrain and the resulting vibration influences can also be predicted.
  • Fig. 3 the indirect ballistic firing of an artillery weapon 2 of a weapon system 1 is shown schematically from a side view. This shows how the topography of the terrain as an interference parameter 12 prevents a direct line of sight between the weapon system 1 and the target 5 .
  • the terrain at the weapon position P2 has a different terrain height than at the target position P5.
  • these different absolute terrain heights of the weapon position P2 and the target position P5 are taken into account as absolute parameters.
  • the absolute heights of the terrain at the weapon position P2 and the target position P5 can be specified in relation to an absolutely defined zero level, such as sea level, and as such, for example, from map information that is stored in a memory of the weapon system 1, using the geographic position data of the weapon position P2 and the Target position P5 can be removed.
  • a detection system 6 in the form of a satellite is shown above the weapon system 1 and the target 5 in FIG. From the detection system position P6, this detection system 6 can directly detect both the target 5 at the target position P5 and the weapon system 1 at the weapon position P2, ie there is a direct line of sight between the detection system 6 and the target 5 or the weapon system 1.
  • the detection system 6 can detect the target 5 and its movement dynamics in the coordinate system K5 from the detection system position P6. This detection can take place, for example, based on radar radiation reflected by the target 5, emitted infrared radiation or optically based on the light reflected from the target 5. In this way, the reflected radar radiation, the emitted infrared radiation or the reflected light forms a detection signal which, despite propagating at the speed of light, requires a time t1 to cover the distance between the target 5 and the detection system 6 and to be detected at the detection system position P6 .
  • This detection signal is processed in the detection system 6 before the processed signal is forwarded from the detection system 6 to the weapon system 1 a time t2 after the detection.
  • the detection system 6 Since both the weapon 2 with the coordinate system K2 located at the weapon position P2 and the target 5 with the coordinate system K5 located at the target position P5 can be detected by the detection system 6, the detection system 6 is suitable with its determinable in the absolute coordinate system KA Detection system position P6 and the local coordinate system K6 of the detection system 6 for indirect ten referencing of the coordinate systems K2 and K5.
  • the coordinate system K5 having its origin in the target position P5 can first be referenced from the detection system position P6 with the original coordinate system K6 there. This detection system position P6 can then be referenced in the coordinate system K2 from the weapon position P2.
  • the coordinate system K2 and the coordinate system K5 at the vehicle position P2 or the target position P5 can be referenced to one another via the coordinate system K6 located at the detection system position P6, even without a direct line between the target position P5 and the weapon position P2 Line of sight must exist.
  • properties of the detection system 6 are also taken into account when determining the fire control solution. These properties can in particular be the time t1 for the detection system 6 to detect the detection signals of the target 5, the time t3 for the transmission of the detection signals or the time t2 for the detection system 6 to process the detection signal.
  • the detection system 6 is shown as a satellite in FIG. 3, the detection system 6 can also be other movable detection systems 6, such as a drone, a UAV or a reconnaissance aircraft. Such movable detection systems 6 can have a changing detection system position P6.
  • the properties of the detection system 6 to be taken into account when determining the fire control solution can also include the movement dynamics of the detection system 6 itself.
  • a special challenge for land-based weapon systems 1 in the context of indirect fire from the movement consists in solving geographic challenges, which are reflected in particular in the form of geographic interference parameters 12-14.
  • These geographical interference parameters 12-14 can be, for example, the topography 12 of the terrain or geographical structures, for example bridges or buildings as structures or the trees 13, 14 shown in FIG.
  • a projectile trajectory 11 must be selected which is free from interference contours of these geographical interference parameters 12-14.
  • the firing weapon system 1 has to calculate the freedom from interference contours of the projectile trajectory 11 to the target 5 on the basis of geographical map material. This requires continuous, highly dynamic terrain modeling between the weapon system 1 at the weapon position P2 and the target 5 at the target position P5, which is extrapolated into the future, particularly taking into account the projectile flight duration.
  • the projectile trajectory 11 is free of interfering contours.
  • the projectile trajectory 8 having a smaller departure angle A would already intersect in the area of the weapon 2 with the interfering contour 13 shown as a tree, so that a projectile on this projectile trajectory 8 would be disturbed by the interfering contour 13 .
  • the projectile trajectory 9 intersects with the course of the terrain as a disturbance parameter 12, so that the projectile on this projectile trajectory 9 does not reach the target 5, but previously in the elevation of the terrain would hit.
  • the projectile trajectory 10 also intersects an interference parameter 14 in the form of a tree, as a result of which the approach angle B of the projectile would be disturbed.
  • the projectile trajectory 11 would be free of interference contours and would therefore be suitable for hitting the target 5 in indirect ballistic fire.
  • a further detection system 6 is provided at the detection position P6, which can be, for example, a stationary observation post from which the target 5 at the target position P5 can be detected . From this terrestrial observation post as a detection system 6, the movement dynamics of the target 5, which is moving along a road 17, can be detected.
  • the movement dynamics of the target 5 recorded relative to the detection system position P6 can be transmitted to a fire control system 4 of the weapon system 1 together with the absolute position of the detection system 6, for example in the form of GPS positions in the absolute coordinate system KA.
  • the movement dynamics of the target 5 in the absolute coordinate system KA can be determined from the relative movement dynamics of the target 5 together with the absolute detection system position P6 for consideration when determining the fire control solution.
  • the absolute movement dynamics of the weapon system 1 which may have been recorded and transformed in the coordinate system K2, then also flow into the absolute coordinate system KA.
  • the detection signals processed by the detection system 6 designed as a satellite can also be forwarded to the fire control system 4 of the weapon system 1 to determine the fire control solution.
  • a defined restricted area 15 extends as a restricted parameter around an object 16 to be protected, which is a hospital, for example for the object 16 would represent. In order to comply with this restricted area 15, this is taken into account as a restricted parameter when determining the fire control solution. Should the target 5 move further along the road 17 in the direction of the object 16 to be protected, so that it enters the restricted area 15, no fire control solution would be issued when the fire control solution was determined as long as the target 5 was in the restricted area 15 stops, even if it would be possible to hit target 5 without observing the blocking parameter.
  • the fire control system 4 and the artillery weapon system 1 it is possible to increase the survivability of the artillery weapon 2 and its operating crew, especially during a firefight in which the weapon 2 shoots at a target 5 and is itself exposed to return fire , to increase.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

L'invention concerne un procédé de détermination d'une solution de guidage de tir d'une arme d'artillerie (2) dans un tir balistique indirect pour atteindre une cible (5), une position d'arme changeante (P2) de l'arme (2) et une position cible (P5) de la cible (5) étant prises en compte comme données de position géographique.
PCT/DE2021/100806 2020-10-19 2021-10-06 Détermination de solution de guidage de tir d'arme d'artillerie WO2022083822A1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
KR1020237014098A KR20230106595A (ko) 2020-10-19 2021-10-06 포병 무기의 사격 통제 솔루션의 결정
AU2021366077A AU2021366077A1 (en) 2020-10-19 2021-10-06 Determination of a fire guidance solution of an artillery weapon
CA3193896A CA3193896A1 (fr) 2020-10-19 2021-10-06 Determination de solution de guidage de tir d'arme d'artillerie
EP21799175.1A EP4229352A1 (fr) 2020-10-19 2021-10-06 Détermination de solution de guidage de tir d'arme d'artillerie
IL301614A IL301614A (en) 2020-10-19 2021-10-06 Determining the fire aiming solution for artillery weapons
US18/032,275 US20230392899A1 (en) 2020-10-19 2021-10-06 Determination of a fire guidance solution of an artillery weapon

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DE102020127430.0A DE102020127430A1 (de) 2020-10-19 2020-10-19 Ermittlung einer Feuerleitlösung einer artilleristischen Waffe

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US20230204326A1 (en) * 2021-12-23 2023-06-29 Raytheon Company Generation and application of autonomously-created three-dimensional safety offset bounding surfaces from three-dimensional virtual maps around points of interest

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1304539A1 (fr) * 2001-10-12 2003-04-23 Oerlikon Contraves Ag Procédé et dispositif pour pointer un tube de cannon et utilisation du dispositif
US20070103673A1 (en) * 2005-11-08 2007-05-10 Honeywell International Inc. Passive-optical locator
US20140251123A1 (en) * 2012-01-22 2014-09-11 Raytheon Company Unmanned range-programmable airburst weapon system for automated tracking and prosecution of close-in targets
US9886040B1 (en) * 2014-09-24 2018-02-06 Rockwell Collins, Inc. System and method for platform alignment, navigation or targeting
US20180094902A1 (en) * 2013-10-31 2018-04-05 Aerovironment, Inc. Interactive Weapon Targeting System Displaying Remote Sensed Image of Target Area

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4949089A (en) 1989-08-24 1990-08-14 General Dynamics Corporation Portable target locator system
US7440610B1 (en) 2004-01-28 2008-10-21 The United States Of America As Represented By The Secretary Of The Navy Apparatus and method for image based coordinate determination
FR2989775B1 (fr) 2012-04-20 2014-06-06 Thales Sa Procede de determination des corrections de tir d'artillerie
US10345078B2 (en) 2016-05-11 2019-07-09 Rivada Research, Llc Method and system for using enhanced location-based information to guide munitions
EP3704437A4 (fr) * 2017-11-03 2021-07-28 Aimlock Inc. Systèmes d'armes motorisés semi-autonomes
WO2022016260A1 (fr) * 2020-07-21 2022-01-27 Kwesst, Inc. Procédés et systèmes de visée de cible indirecte référencée par image numérique
US11460270B1 (en) * 2021-11-23 2022-10-04 George Carter System and method utilizing a smart camera to locate enemy and friendly forces

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1304539A1 (fr) * 2001-10-12 2003-04-23 Oerlikon Contraves Ag Procédé et dispositif pour pointer un tube de cannon et utilisation du dispositif
US20070103673A1 (en) * 2005-11-08 2007-05-10 Honeywell International Inc. Passive-optical locator
US20140251123A1 (en) * 2012-01-22 2014-09-11 Raytheon Company Unmanned range-programmable airburst weapon system for automated tracking and prosecution of close-in targets
US20180094902A1 (en) * 2013-10-31 2018-04-05 Aerovironment, Inc. Interactive Weapon Targeting System Displaying Remote Sensed Image of Target Area
US9886040B1 (en) * 2014-09-24 2018-02-06 Rockwell Collins, Inc. System and method for platform alignment, navigation or targeting

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CA3193896A1 (fr) 2022-04-28
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AU2021366077A1 (en) 2023-04-06
DE102020127430A1 (de) 2022-04-21
EP4229352A1 (fr) 2023-08-23

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