EP1920209A1 - Procede d'optimisation du declenchement du tir d'une arme ou d'une piece d'artillerie - Google Patents
Procede d'optimisation du declenchement du tir d'une arme ou d'une piece d'artillerieInfo
- Publication number
- EP1920209A1 EP1920209A1 EP06762720A EP06762720A EP1920209A1 EP 1920209 A1 EP1920209 A1 EP 1920209A1 EP 06762720 A EP06762720 A EP 06762720A EP 06762720 A EP06762720 A EP 06762720A EP 1920209 A1 EP1920209 A1 EP 1920209A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- target
- fire
- data
- calculated
- time
- 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 abstract description 24
- 238000010304 firing Methods 0.000 title abstract description 7
- 238000004422 calculation algorithm Methods 0.000 claims abstract description 10
- 230000002349 favourable effect Effects 0.000 claims abstract description 6
- 238000005259 measurement Methods 0.000 claims description 10
- 230000001133 acceleration Effects 0.000 claims description 6
- 238000011161 development Methods 0.000 claims description 3
- 238000010586 diagram Methods 0.000 claims description 3
- 230000000977 initiatory effect Effects 0.000 claims 1
- 230000008569 process Effects 0.000 abstract description 4
- 230000008859 change Effects 0.000 description 2
- 238000012937 correction Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000013213 extrapolation Methods 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 230000001360 synchronised effect Effects 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
Definitions
- a device for measuring the projectile velocity at the mouth of a gun barrel is known. This comprises two spaced apart from each other on a support tube, responsive to change in a magnetic flux sensors that are in communication with an evaluation.
- Additional sources of error are in particular the unknown target movements between the time of firing the projectile and its arrival at the target.
- the probable position can be especially for longer flight distances of the projectile. difficult to predetermine the goal at the meeting point.
- models of the target movement are formulated and controlled with measurement data of the target in order to identify the kinematics of the target. These data are then used in the fire control to predict the target position after the expected flight time, usually extrapolated.
- the measurements are purely positional determinations.
- the target speed and possibly the target acceleration are derived from these and used for extrapolation.
- the accuracy of the extrapolated data is particularly dependent on the quality of the acceleration estimate.
- the Fire Department will refuse to fire.
- the known residuals of the Filters ie, the difference between the estimate and the measurement, are therefore less suitable for this purpose because they only include the position errors to the target. In a target maneuver, it always takes some time before the filter transforms the generated residuals into acceleration. This is spoken by the settling of the filter.
- the total time delay between the target maneuver and the time of the arrival of the projectile, whose fire elements take into account these maneuvers, at the target is composed
- Time delay settling of the filter + flight time of the projectile + remaining dead times.
- test projectiles which can be referred to as "closed loop.”
- closed loop To statistically improve the measurement results of the test projectiles, they are fired in a limited number in succession, a burst of fire whose first shots are measured in the target It must be longer than the projectile flying time if its last shots are to benefit from the corresponding corrections Depending on the application, such measuring systems are complicated and also expensive.
- the invention takes on the task of specifying a method which assists a surgeon in the choice of the best burst of fire, especially in target maneuvers.
- the invention is based on the idea to use a known calculation algorithm of a real shooting to determine the best moment of the fire triggering on moving targets, but not really trigger the fire command. This is purely hypothetical. Data is thereby determined and used by continuously calculating and collecting the fire commands and the associated prospective meeting points.
- the method is based on calculating the fire commands and the expected meeting point without actually triggering the fire.
- the goal is sought, the algo- rithm is switched on and this calculates everything else hypothetically.
- In the algorithm can be contained thereby also the controlling of the guns as basis for the fire order.
- the actual target position is determined and the error distance between the target and the predicted meeting point is calculated. This gives a statement about how exactly would have been shot. Although this information is obsolete by the flight time, but can be generated continuously and provide important information about the course of the expected hit probability.
- the error in the target may be a minimum distance between the trajectories of the projectile and the target. If the time at the finish also plays a role, as in the case of disintegrating projectiles or grenades with a time fuse, the distance between the two at the time of disassembly is decisive. Alternatively, angle errors may be considered. Also, a suitable combination of different error definitions is conceivable, but the result is described advantageously with a scalable size.
- current or quasi-current additional data are preferably made available to the operator via the display.
- a software consideration in the algorithm is provided, wherein the graphical representation can be maintained.
- a suitable measure of the hit error thus results as soon as the target approaches the meeting point calculated in advance.
- the calculated measure of the hit errors is graphically displayed, continuously updated and additionally made available to the surgeon or algorithm. There is no correction of the fire commands instead, rather than a costly measurement in the target area, the operator a method / presentation made available, which support him in the choice of the most favorable moment of the fire triggering.
- FIG. 4 shows the representation from FIG. 3 with a first additional information
- FIG. 5 shows the representation of FIG. 3 with a further additional information.
- FIG. 1 shows a directional gun labeled 1, which fights a target 2 from a computer 3 with data.
- the computer 3 is electrically connected to the gun 1 as well as to a display device 4 for an operator 5.
- the target measurements are usually synchronized with the base clock of the fire control, so they do not coincide with the predictable hit points P1 - P3.
- Fig. 2 a part of a burst of fire is shown.
- the flight time to the target 2 in the example shown is two to three fire cycles.
- the data is unified in time by a suitable interpolation.
- the gun data will be kept for at least the duration of the projectile flight. As a result of the target movement, a certain amount of time expands so that no or more target measurements occur between two shots, which is taken into account in the data processing.
- T W time window
- the data is graphically represented as a left-moving curve 6.
- the age of the most recent data equals the time of flight and is plotted on the right side of the window (T).
- T F In order to improve the obsolete data T F , additional information is preferably integrated into the method, which gives the surgeon 5 other relevant information Of origin so that the operator 5 can determine if the time had been properly selected also from the point of view of T F.
- the surgeon 5 additionally has data provided with T F / 2 as part curve (g) graphically (FIG. 4).
- the partial curve (g) indicates in the example shown that the current moment is not favorable, as was assumed on the basis of FIG. 3, since the hit errors increase again.
- Another source of additional data may be the estimated accelerations from the filter. These are updated continuously with the help of the latest target measurement.
- the direct observation of the goal 2 offers. Before an aircraft 2 exercises a maneuver, it must change its position relative to the direction of flight. In this case, as shown in Fig. 5, a video image of the target 2 can be displayed in the display diagram of the display 4. This also provides up-to-date data or additional information that the operator 5 takes into account in assisting him in choosing the most favorable moment of the fire triggering.
- the graphical representations according to FIGS. 3 to 5 therefore support the surgeon 5, who interprets these displayed data in such a way that he can conclude from the trend of the processes on the future development of the hit errors.
- An alternative implementation of the invention is to automate the process by a suitable algorithm to simplify the presentation of the result, for example with a lamp or to fire the fire by a fire command.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Gas Separation By Absorption (AREA)
- Luminescent Compositions (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102005041704A DE102005041704A1 (de) | 2005-09-02 | 2005-09-02 | Verfahren zur Optimierung eines Feuerauslösens einer Waffe oder eine Geschützes |
| PCT/EP2006/007128 WO2007028455A1 (fr) | 2005-09-02 | 2006-07-20 | Procede d'optimisation du declenchement du tir d'une arme ou d'une piece d'artillerie |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1920209A1 true EP1920209A1 (fr) | 2008-05-14 |
| EP1920209B1 EP1920209B1 (fr) | 2011-03-30 |
Family
ID=37232475
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP06762720A Not-in-force EP1920209B1 (fr) | 2005-09-02 | 2006-07-20 | Procede d'optimisation du declenchement du tir d'une arme ou d'une piece d'artillerie |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US8579194B2 (fr) |
| EP (1) | EP1920209B1 (fr) |
| CN (1) | CN101300458B (fr) |
| AT (1) | ATE503980T1 (fr) |
| CA (1) | CA2620435A1 (fr) |
| DE (2) | DE102005041704A1 (fr) |
| DK (1) | DK1920209T3 (fr) |
| ES (1) | ES2364187T3 (fr) |
| WO (1) | WO2007028455A1 (fr) |
| ZA (1) | ZA200800614B (fr) |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102009010362A1 (de) | 2009-02-25 | 2011-01-13 | Rheinmetall Waffe Munition Gmbh | Feuerleitung einer richtbaren Waffenanlage |
| US8336776B2 (en) | 2010-06-30 | 2012-12-25 | Trijicon, Inc. | Aiming system for weapon |
| US8172139B1 (en) | 2010-11-22 | 2012-05-08 | Bitterroot Advance Ballistics Research, LLC | Ballistic ranging methods and systems for inclined shooting |
| TWI485630B (zh) | 2012-12-14 | 2015-05-21 | Sintai Optical Shenzhen Co Ltd | 瞄準器，其操作方法，及其電腦程式產品 |
| DE102013007229A1 (de) | 2013-04-26 | 2014-10-30 | Rheinmetall Waffe Munition Gmbh | Verfahren zum Betrieb eines Waffensystems |
| US11016302B2 (en) | 2015-03-17 | 2021-05-25 | Raytrx, Llc | Wearable image manipulation and control system with high resolution micro-displays and dynamic opacity augmentation in augmented reality glasses |
| US12235445B2 (en) | 2015-03-17 | 2025-02-25 | Raytrx, Llc | Wearable image manipulation and control system with high resolution micro-displays and dynamic opacity augmentation in augmented reality glasses |
| US12094595B2 (en) * | 2015-03-17 | 2024-09-17 | Raytrx, Llc | AR/XR headset for military medical telemedicine and target acquisition |
| US11956414B2 (en) | 2015-03-17 | 2024-04-09 | Raytrx, Llc | Wearable image manipulation and control system with correction for vision defects and augmentation of vision and sensing |
| US12237074B2 (en) | 2015-03-17 | 2025-02-25 | Raytrx, Llc | System, method, and non-transitory computer-readable storage media related to correction of vision defects using a visual display |
| US12137974B1 (en) | 2015-03-17 | 2024-11-12 | Raytrx, Llc | System, method, and non-transitory computer-readable storage media related to correction of vision defects using a visual display |
| US12062430B2 (en) | 2015-03-17 | 2024-08-13 | Raytrx, Llc | Surgery visualization theatre |
| AU2018410908B2 (en) * | 2018-03-01 | 2021-11-11 | Axon Enterprise, Inc. | Systems and methods for detecting a distance between a conducted electrical weapon and a target |
| US12142367B2 (en) | 2020-02-21 | 2024-11-12 | Raytrx, Llc | Surgery visualization theatre |
| WO2021262324A2 (fr) * | 2020-05-04 | 2021-12-30 | Raytrx, Llc | Casque de réalité augmentée/étendue (ar/xr) pour télémédecine militaire et acquisition de cible |
| US12537092B2 (en) * | 2020-05-04 | 2026-01-27 | Raytrx, Llc | AR/XR headset for military target acquisition |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1165459B (de) | 1959-07-04 | 1964-03-12 | Boelkow Entwicklungen Kg | Einrichtung zur Vorausbestimmung des oder der Winkel, unter dem oder denen zu einem bestimmten Zeitpunkt ein Flugkoerper seinen Startort verlassen muss, um mit einem vorausbestimmten Ziel zu kollidieren |
| CH474738A (de) | 1968-05-07 | 1969-06-30 | Baumann Martin | Vorrichtung zur Anzeige von Richtfehlern |
| CH650857A5 (en) | 1979-07-11 | 1985-08-15 | Hans Baasch Dr Ing | Monitoring apparatus for determining and displaying the aiming error when aiming and firing at moving targets |
| US4308015A (en) * | 1979-12-20 | 1981-12-29 | General Electric Company | System and method for aircraft gunnery training and accuracy evaluation |
| FR2477695A1 (fr) * | 1980-03-07 | 1981-09-11 | Giravions Dorand | Procede et appareillage de commande de tir sur cible reelle |
| DE3381149D1 (de) | 1982-09-30 | 1990-03-01 | Gen Electric | Automatische schussverbesserung fuer flugzeuge. |
| US4794235A (en) * | 1986-05-19 | 1988-12-27 | The United States Of America As Represented By The Secretary Of The Army | Non-linear prediction for gun fire control systems |
| CH691143A5 (de) | 1995-03-17 | 2001-04-30 | Contraves Ag | Vorrichtung zur Messung der Geschossgeschwindigkeit an der Mündung eines Waffenrohres eines Geschützes hoher Kadenz. |
| GB0005594D0 (en) * | 2000-03-09 | 2000-12-20 | British Aerospace | A ballistics fire control solution process and apparatus for a spin or fin stabilised projectile |
-
2005
- 2005-09-02 DE DE102005041704A patent/DE102005041704A1/de not_active Withdrawn
-
2006
- 2006-07-20 CN CN2006800409248A patent/CN101300458B/zh not_active Expired - Fee Related
- 2006-07-20 WO PCT/EP2006/007128 patent/WO2007028455A1/fr not_active Ceased
- 2006-07-20 DE DE502006009219T patent/DE502006009219D1/de active Active
- 2006-07-20 AT AT06762720T patent/ATE503980T1/de active
- 2006-07-20 CA CA002620435A patent/CA2620435A1/fr not_active Abandoned
- 2006-07-20 US US11/991,229 patent/US8579194B2/en not_active Expired - Fee Related
- 2006-07-20 DK DK06762720.8T patent/DK1920209T3/da active
- 2006-07-20 ES ES06762720T patent/ES2364187T3/es active Active
- 2006-07-20 EP EP06762720A patent/EP1920209B1/fr not_active Not-in-force
-
2008
- 2008-01-21 ZA ZA200800614A patent/ZA200800614B/xx unknown
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2007028455A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| US8579194B2 (en) | 2013-11-12 |
| ZA200800614B (en) | 2008-12-31 |
| DE102005041704A1 (de) | 2007-03-15 |
| DK1920209T3 (da) | 2011-07-11 |
| US20090218400A1 (en) | 2009-09-03 |
| ES2364187T3 (es) | 2011-08-26 |
| DE502006009219D1 (de) | 2011-05-12 |
| CA2620435A1 (fr) | 2007-03-15 |
| EP1920209B1 (fr) | 2011-03-30 |
| WO2007028455A1 (fr) | 2007-03-15 |
| CN101300458B (zh) | 2012-09-26 |
| ATE503980T1 (de) | 2011-04-15 |
| CN101300458A (zh) | 2008-11-05 |
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