IL148539A - Vehicle weapon fire control system - Google Patents
Vehicle weapon fire control systemInfo
- Publication number
- IL148539A IL148539A IL148539A IL14853902A IL148539A IL 148539 A IL148539 A IL 148539A IL 148539 A IL148539 A IL 148539A IL 14853902 A IL14853902 A IL 14853902A IL 148539 A IL148539 A IL 148539A
- Authority
- IL
- Israel
- Prior art keywords
- weapon
- camera
- aiming
- operator
- control
- Prior art date
Links
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
- F41G3/16—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
- F41G5/24—Elevating or traversing control systems for guns for vehicle-borne guns for guns on tanks
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Description
148539/2
ii-ji pvi » D *?v >i> flipa naive
Vehicle weapon fire control system
Sagem SA
C. 138114
- -
WEAPON FIRE CONTROL SYSTEM
The present invention relates to weapon fire control systems .
GENERAL TECHNICAL FIELD
Fire controls are conventionally known, comprising:
- a weapon mobile about two axes, elevation and bearing, the aiming of which is effected with regard to each of the two axes by way of a velocity servocontrol achieved on the basis of a facility for motorization of the weapon and of an angular velocity measurement sensor;
- a video camera mounted securely with the weapon and whose sighting axis is parallel to that of the weapon; this sighting axis is defined by a reticle inlaid into the video image;
The operator then uses the video image supplied by the camera to sight a target by aligning this target with the reticle inlaid into the image. To do this, he acts on an aiming stick which supplies the servocontrol of the weapon with the elevational and bearing velocity commands reguired for the tracking of the target.
In the case where the above system is used on a mobile vehicle it is necessary to ensure the stabilization of the weapon about both axes, elevation and bearing, so as to eliminate the angular disturbances of aim which are caused by the movement of the vehicle.
Stabilization of the weapon is then generally achieved by using a gyroscopic facility (rate gyro) as the weapon's angular velocity measurement sensor.
In such a system the following problems appear:
1) The camera being secured to the weapon, the aiming of the sight is obtained directly by the aiming of the weapon. However, having regard:
01381144U5-01
- to the generally considerable mass and inertia of the weapon,
to the numerous disturbing torques (unbalances, friction, etc.) which intervene in the servocontrol ,
- to the technical solutions generally employed for this type of motorization (geared reduction motor inevitably exhibiting some play and limited mechanical stiffness) , the performance of the weapon's aiming servocontrol is itself limited.
This results in mediocre quality of aiming of the weapon which is experienced directly by the operator with regard to his sight and which impedes the obtaining of fine, continuous and well-centred tracking of the sight onto the target .
2) The stabilization of the sight (decoupling from the movements of the vehicle) is obtained directly by stabilization of the weapon. However, having regard to the difficulties recalled above, the quality conventionally obtained in weapon stabilization is likewise limited and generally insufficient so as not to significantly degrade the intrinsic quality of the image supplied by the camera. Specifically, the residual movements of the weapon which are transmitted directly to the camera are generally of a much larger order of magnitude than the camera's own resolution, thereby creating blur on the image observed and resulting in a loss of observation range.
3) In the case where firing is requested, there is reason, as in any conventional fire control, to shift prior to firing the axis of the weapon with respect to the direction of the target by an angular correction in elevation and bearing (fire correction). This fire correction takes account in particular of the effects of the ballistic trajectory of the munition (lift correction) and of any relative displacement of the target with respect to the marksman during the time of
01381 144X45-01
- -
flight of the munition (kinematic correction)
The calculation of the fire correction requires in particular the knowledge of the distance of the target and of the target /marksman relative angular velocity. These parameters are generally acquired during a preliminary phase of target tracking by the use of a telemeter coupled to the video camera and the acquisition of the measurements of angular velocity of aim of the weapon during the target tracking phase.
In the type of system alluded to, the introduction of the fire correction is performed by shifting the sighting reticle in the video image by an angular deviation corresponding to the calculated fire correction.
The firing sequence is then performed thus:
- acquisition of the target by the operator in the field of the camera.
- Fine tracking of the target by the operator using his sighting reticle.
Acquisition of the parameters required for the calculation of the fire correction.
- Translation of the sighting reticle in the video image so as to allow the introduction of an angular shift equal to the fire correction between the direction of the weapon and the direction of the sighting reticle once displaced.
Re-aiming by the operator at the target with the sighting reticle, the latter occupying its new position.
In such a sequence, the operator must track the target a first time and then re-aim at it accurately a second time after introduction of the fire correction by shift of the reticle.
This two-stage method ' is prejudicial to the total reaction time of the system before firing having regard in particular to the need for the operator to accurately
01381144X45-01
- -
re-aim at the target a second time with his reticle.
In order to eliminate the various drawbacks stated above a conventional solution is to introduce an aiming and stabilization device specific to the video channel (in addition to the weapon's aiming and stabilization device) based either on the interposition of a two-axis stabilized mirror downstream of the camera, or on the mounting of the camera directly on a two-gimbal stabilized platform.
For an example of an automatic target tracking device, reference may advantageously be made to Patent Application FR 2 484 626.
In this document, the television camera which constitutes the observation and sighting means is mobile with respect to the turret of the tank.
According to two degrees of freedom there are provided processing means allowing it to undertake target tracking to which the aimin of the weapon is servocontrolled.
By virtue of these means which are specific thereto, the aiming and stabilization of the sight become independent of that of the weapon, the latter generally being feedback controlled by duplication of the position of the sight.
The aiming and stabilization performances obtained with regard to sighting are generally very good.
The introduction of the fire correction is achieved by
01381 144X45-01
148539/2 shifting the weapon with respect to the sight, this shift possibly being effected automatically by introducing the shift directly into the feedback control of the weapon with regard to the sight. The sight which is stabilized independently is not disturbed by this introduction of the fire correction and the operator has no operation of re-aiming at the target to be performed. The ergonomics of the system are improved and the total reaction time of the system before firing is minimal.
This solution offers numerous technical advantages but it results unfortunately in a very considerable increase in the complexity and cost of the system, thereby greatly limiting its use.
PRESENTATION OF THE INVENTION AND STATE OF THE ART
The objectives of the present invention are to afford the same improvements as the previous solutio in terms of performance, ergonomics and reaction time but by proposing a much more economical and physically much
i
less complex and bulky solution.
It is already known practice to restore video images degraded by angular deflection movements undergone by a camera by applying to these N images a translation inverse to the translation undergone by the image, together with, as appropriate, a blur restoration processing.
Reference may for example be made in this regard to French Patent No. 2 689 354, which describes only image restoration in the case of a camera mounted on a mobile craft undergoing angular destabilizations .
For its part, the invention proposes a fire control system for the aiming of a weapon by an operator, comprising:
means of motorization able to drive the weapon, means able to control the means of motorization so as to displace the weapon as a function of a control command
- aiming means allowing the operator to generate this control command,
observation and sighting means which comprise a camera whose observation axis is parallel to the weapon,' an image captured by this camera being transmitted to the operator on a sighting channel,
means able to stabilize the image supplied to the operator on the sighting channel,
characterized in that the observation axis of the observation and sighting means is fixed with respect to the weapon and in that the stabilization means comprise means which determine an error representative of the deviation between the position corresponding to the control command and the actual position of the weapon and which apply to the image captured by the camera a translation inverse to that corresponding to this position deviation.
Advantageously, the means of control of the motorization means comprise means for summing with a control command generated by the aiming means a correction dependent on the position deviation for which a translation is applied to the image captured by the camera, the sum of the control command generated by the aiming means and of this correction being used as control command to control the displacement of the weapon .
In particular, the correction summed with the control command generated by the aiming means is furthermore dependent on a fire correction to be applied to the weapon .
Especially, in an especially preferred manner, the correction summed with the control command generated by
7 148539/2
the aiming means is dependent on the sum between the fire correction and a displacement corresponding to the inverse of the translation applied to the image captured by the camera.
Other characteristics and advantages of the invention will emerge further from the description which follows and which is purely illustrative and nonlimiting.
DESCRIPTION OF A POSSIBLE EMBODIMENT OF THE INVENTION
Architecture
The architecture of a system in accordance with a possible embodiment of the invention is represented in sole
Figure 1, which diagrammatically illustrates the servocontrols which are applied individually to each of the two elevation and bearing axes of the weapon system.
The system represented in this figure comprises an aiming stick 1 allowing the operator to generate velocity, elevation, or bearing aiming commands.
It also comprises a device 5 for motorization of the weapon in terms of elevation or bearing. This device 5 has as input a velocity error arising from a summator S3 and as output the velocity communicated to the weapon .
The summator S3 receives as input a velocity command.
It subtracts the velocity of the weapon therefrom, which is measured by a sensor 6 which measures the angular velocity of the weapon in terms of elevation or bearing. This sensor 6 is for example a rate gyro in the case of a stabilized system.
The motorization device 5, the sensor 6 and the
8 148539/2 summator S3 constitute the weapon's velocity servocontrol loop.
The velocity command received as input by the summator
S3 is the sum of the velocity commanded by the operator on the basis of the aiming stick 1 and of a velocity correction determined by the assembly which will now be described.
This assembly comprises a summator SI which subtracts from the velocity commanded by the operator with the aid of the aiming stick 1 and the velocity of the weapon as measured by the sensor 6.
The output signal from this summator SI is transmitted to integrator 2 which carry out the time integration of the velocity error corresponding to the signal output by the summator SI.
The velocity error thus integrated is transmitted to means 3 which carry out a restoration of the degraded image by implementing a processing of the type of that described in Patent FR 2 689 354, consisting in applying to the current image a translation inverse to the value supplied by the integrator 2 (the sampling of the output of the integrator 2 being done in a manner synchronized with the acquisition of the video images) .
The integrated velocity error arising from the integrator 2 is furthermore transmitted as input to a summator S2.
The summator S2 forms the sum between this integrated velocity error arising from the integrator 2 and a value of the fire correction, which is calculated elsewhere independently, and which has to be introduced into the system. The fire correction processing may be very diverse (ballistic lift corrections, anticipations of target movement, weather, etc.) and is in itself
conventionally known to the person skilled in the art.
The output signal from the summator S2 is transmitted to gain means 4 which generate on this signal a velocity control gain making . it possible to transform a position deviation arising from the summatory S2 into a velocity command for the servocontrol of the weapon.
Manner of operation ;
The various functionalities offered by the architecture just described are presented in a progressive manner independently of one another hereinbelow:
Stabilization of the image in the absence of commanded aiming velocity and of fire correction to be introduced:
The sensor 6 measures the residual velocity of the weapon (which is not completely zero having regard to the imperfect stabilization of the weapon).
The output of the integrator 2 reconstructs the positional movement of the weapon and hence of the camera (successive positions of the camera at each image) .
The means 3 carry out on each image a translation inverse to the camera's residual movement supplied by the integrator 2, thereby allowing compensation of this movement. The image presented to the operator is therefore thus stabilized.
Independent control of the velocity sighting in the absence of stabilization (vehicle stationary) and of fire correction to be introduced:
The aiming stick 1 supplies the instructed velocity aiming command on sighting. This command is sent to the
weapon's velocity servocontrol (anticipation control). The weapon duplicates this velocity command only imperfectly. The summator SI takes the difference between the velocity instructed on sighting and the velocity achieved by the weapon as measured by the sensor 6. The output of the integrator 2 represents the deviation in position between the position instructed on sighting and the measured position of the weapon and hence of the camera. The means 3 perform on each image a translation inverse to that corresponding to the position deviation supplied by the integrator 2. The image presented to the operator is then decoupled from the weapon's own movement. As far as the operator is concerned, this amounts to having direct control of sighting independent of the weapon which nevertheless carries the camera.
Introduction of the fire correction in the absence of stabilization (vehicle stationary) and of instructed aiming velocity:
The fire correction (elevational or bearing angular shift command) is introduced by way of the summator S2.
This command is transformed into a velocity control for the servocontrol of the weapon by the gain means 4.
The servocontrol of the weapon reacts and the weapon is driven. The sensor 6 measures the velocity achieved by the weapon and feeds the integrator S2 which brings about the progressive translation of the image.
When the translation effected on the image is equal to the fire correction to be introduced the velocity command arising from the summator S2 is cancelled out and the weapon comes to a standstill.
The weapon is then shifted with respect to the sighting by the value of the fire correction, the image
presented to the operator having remained still.
In practice the various modes of operation analysed independently above are overlaid.
A system is thus obtained which simultaneously has:
• Stabilization of the image presented to the operator (image decoupled from the movements of the vehicle and the weapon) .
· Independent control of velocity sighting (not constrained by the quality of the servocontrol of the weapon) .
• Automatic introduction of the fire correction without disturbance with regard to sighting (thus allowing a minimal reaction time before firing) .
Variant embodiments other than that just described are of course possible. In particular
• the video camera may be a television camera or a thermal camera.
• The invention applies as a priority to systems using cameras equipped with matrix detectors which are therefore not furnished with an internal device for line or column scanning. However the invention may be applied to cameras equipped with a linear-array detector which require an internal device for line scanning. In this case the stabilization of the image will be satisfactorily obtainable only with regard to a limited zone of the image for which the image-by- image acquisition of the movement of the camera is perfectly synchronized with the acquisition of this zone of the image.
• The camera might not be mounted directly on the weapon but integrated into a viewfinder which has an aiming mirror linked mechanically to the weapon allowing the camera sight to be secured to (fixed) and coaxial with this weapon (case of a turret roof viewfinder with mechanical feedback duplication of the weapon) .
The stabilization of the weapon can be achieved by-means of loopings different from that described in the invention (for example: open-loop stabilization of the weapon on the basis of a chassis rate gyro for bearing and of a turret rate gyro for elevation) . The proper operation of the invention requires only the ability on the one hand to control the weapon in terms of displacement and on the other hand to have available the measurement either of the velocity or of the position achieved by the weapon (in the latter case, the summator SI is placed downstream of the integrator 2 in diagram 1) .
If the case of a stationary vehicle is considered, the servocontrol of stabilization of the weapon can be replaced by a simple servocontrol of velocity based on the use of tachometers allowing measurement of the relative velocity of the weapon with respect to its support. The functions of independent control of the line of sight and of automatic introduction of the fire correction are still available in such a configuration .
Claims (7)
13 148539/2 CLAIMS J —"Fire control system for the aiming of a vehicle weapon by an operator, comprising: means of motorization able to drive the weapon, means able to control the means of motorization so as to displace the weapon as a function of a control command, aiming means allowing the operator to generate this control command, observation and sighting means which comprise a camera whose observation axis is parallel to the weapon, an image captured by this camera being transmitted to the operator on a sighting channel, means able to stabilize the image supplied to the operator on the sighting channel, characterized in that the observation axis of the observation and sighting means is fixed with respect to the weapon and in that the stabilization means comprise means which determine an error representative of the deviation between the position corresponding to the control command and the actual position of the weapon and which apply to the image captured by the camera a translation inverse to that corresponding to this position deviation.
2. System according to Claim 1, characterized in that the means of control of the motorization means comprise means for summing with a control command generated by the aiming means a correction signal dependent on the position deviation for which a translation is applied to the image captured by the camera, the sum of the control command generated by the aiming means and of this correction being used as control command to control the displacement of the weapon.
3. System according to Claim 2, characterized in that the correction signal summed with the control command generated by the aiming means is furthermore dependent 14 148539/2 on a fire correction signal to be applied to the weapon.
4. System according to Claim 3 , characterized in that the correction signal summed with the control command generated by the aiming means is dependent on the sum between the fire correction signal and. a displacement corresponding to the inverse of the translation applied to the image captured by the camera.
5. System according to one of the preceding claims, characterized in that it comprises an angular velocity or position sensor which supplies measurements of angular velocity or of position of the weapon on the one hand to the means to stabilize the image supplied to the operator on the sighting channel and on the other hand to the means which control the motorization means.
6. System according to one of the preceding claims, characterized in that the means to stabilize the image supplied to the operator on the sighting channel receive as input on the one hand a command representative of an angular velocity of command and on the other hand an angular velocity measurement and in that the stabilization means comprise means for integrating over time the deviation between this command this measurement.
7. System according to one of the preceding claims, characterized in that the camera is one which employs matrix detectors. For the Applicants,
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0103233A FR2821928B1 (en) | 2001-03-09 | 2001-03-09 | SHOOTING CONDUCT SYSTEM |
Publications (2)
Publication Number | Publication Date |
---|---|
IL148539A0 IL148539A0 (en) | 2002-09-12 |
IL148539A true IL148539A (en) | 2007-07-04 |
Family
ID=8860930
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL148539A IL148539A (en) | 2001-03-09 | 2002-03-06 | Vehicle weapon fire control system |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE10208102B4 (en) |
FR (1) | FR2821928B1 (en) |
GB (1) | GB2375385B (en) |
IL (1) | IL148539A (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE1016871A3 (en) * | 2005-12-05 | 2007-08-07 | Fn Herstal Sa | IMPROVED DEVICE FOR REMOTE CONTROL OF A WEAPON. |
WO2007119951A1 (en) * | 2006-04-17 | 2007-10-25 | Moon Key Lee | Sighting device using virtual camera |
GB2439744A (en) * | 2006-07-04 | 2008-01-09 | Christopher Bee | Shot pattern and target display |
US20140267778A1 (en) * | 2013-03-15 | 2014-09-18 | Freefly Systems, Inc. | Apparatuses and methods for controlling a gimbal and other displacement systems |
DE102014114036A1 (en) * | 2014-09-26 | 2016-03-24 | Cassidian Optronics Gmbh | Straightening and guiding device and method for supporting a gunner of a weapon system |
US9900511B2 (en) | 2015-04-10 | 2018-02-20 | Freefly Systems, Inc. | Method, system, and device for controlling a stabilized camera remotely |
FR3038377B1 (en) | 2015-07-03 | 2018-06-15 | Safran Electronics & Defense | MOTORIZED METHOD AND DEVICE FOR SCORING |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2625667B2 (en) * | 1976-06-08 | 1980-01-10 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Method for calculating the reserve for fire control systems for firearms installed on a vehicle with a stabilized aiming device |
FR2480424B1 (en) * | 1980-04-11 | 1987-07-10 | Sfim | AUTOMATIC AIR-TO-AIR OR AIR-TO-GROUND CONDUCTOR |
FR2484626A1 (en) * | 1980-06-11 | 1981-12-18 | Applic Mach Motrices | Anti-aircraft target tracking system for tank - employs TV cameras and servo loops with weapon firing correction for weapon turret positioning |
DE3125678C2 (en) * | 1981-06-30 | 1983-10-06 | Bodenseewerk Geraetetechnik Gmbh, 7770 Ueberlingen | Straightening device |
US4698489A (en) * | 1982-09-30 | 1987-10-06 | General Electric Company | Aircraft automatic boresight correction |
NL8204706A (en) * | 1982-12-06 | 1984-07-02 | Hollandse Signaalapparaten Bv | INTEGRATED WEAPON FIRE CONTROL SYSTEM. |
DE3404202A1 (en) * | 1984-02-07 | 1987-05-14 | Wegmann & Co | Device for the remotely controlled guidance of armoured combat vehicles |
DE3409538C1 (en) * | 1984-03-15 | 1985-08-22 | Eltro GmbH, Gesellschaft für Strahlungstechnik, 6900 Heidelberg | Method and device for aligning two rotation planes |
DE3725760A1 (en) * | 1987-08-04 | 1989-02-16 | Honeywell Regelsysteme Gmbh | Regulator circuit system for weapon servo installation - has cascaded regulator sections with digital position regulator coupled by A=D and D=A converter interfaces |
JPH04263796A (en) * | 1991-01-10 | 1992-09-18 | Mitsubishi Electric Corp | Automatic aiming error correcting method and device therefor |
US5171933A (en) * | 1991-12-20 | 1992-12-15 | Imo Industries, Inc. | Disturbed-gun aiming system |
FR2689354B1 (en) * | 1992-03-31 | 1994-07-01 | Sfim | RECURRING PROCESS FOR RESTORING A DEGRADED VIDEO IMAGE. |
US5456157A (en) * | 1992-12-02 | 1995-10-10 | Computing Devices Canada Ltd. | Weapon aiming system |
US5949015A (en) * | 1997-05-14 | 1999-09-07 | Kollmorgen Corporation | Weapon control system having weapon stabilization |
-
2001
- 2001-03-09 FR FR0103233A patent/FR2821928B1/en not_active Expired - Fee Related
-
2002
- 2002-02-26 DE DE10208102A patent/DE10208102B4/en not_active Expired - Fee Related
- 2002-03-01 GB GB0204894A patent/GB2375385B/en not_active Expired - Fee Related
- 2002-03-06 IL IL148539A patent/IL148539A/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
DE10208102A1 (en) | 2002-09-19 |
GB2375385B (en) | 2004-08-25 |
IL148539A0 (en) | 2002-09-12 |
GB2375385A (en) | 2002-11-13 |
DE10208102B4 (en) | 2012-01-12 |
FR2821928B1 (en) | 2003-08-29 |
GB0204894D0 (en) | 2002-04-17 |
FR2821928A1 (en) | 2002-09-13 |
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