Control mechanism securable to a firing device and method

A control mechanism securable to a firing device is provided. The control mechanism includes an actuation component adapted to generate signals in response to activation of the actuation component. Further, the control mechanism includes an attachment apparatus adapted to support the actuation component adjacent to a stock of the firing device. The attachment apparatus has at least one securing member for securement of the attachment apparatus to the stock of the firing device.

CARTRIDGE BASED MODULAR TURRET CONTROL SYSTEM

Apparatus and associated methods relate to a modular cartridge turret assembly system for quickly exchanging modular cartridges to interact with a ring gear. A modular cartridge may be a brake cartridge, which when inserted into a modular cartridge turret assembly, operably engages with the ring gear to inhibit the rotation of a turret. In an illustrative example, the brake cartridge, when inserted, may prevent damages and injuries caused by the rotation of the turret during transportation. In an exemplary embodiment, the modular cartridge turret assembly system may include a locking mechanism to secure the modular cartridge within the modular cartridge turret assembly. The locking mechanism may safeguard that the brake cartridge remains within the modular cartridge turret assembly system during turbulent situations caused by environmental conditions. 120.-. (canceled)21. A toollessly interchangeable ring gear drive mount system for a rotatable turret , the toollessly interchangeable ring gear drive system comprising:a ring gear;a ring gear drive module;a mount bracket extending in a plane perpendicular to an axis of rotation of the ring gear, the mount bracket being adapted for mounting to a platform arranged in a rotatable relationship to the ring gear;a pair of receiver members extending from the mount bracket and defining a pair of slide channels, each of the slide channels being defined by a pair of opposing channel sidewalls that are connected by a channel backwall, wherein the slide channels are positioned substantially vertically and oriented substantially parallel to the axis of rotation; and,a pair of mount flanges each sized and shaped to be slidably inserted into a corresponding one of the pair of slide channels, wherein when engaged in the slide channels, the mount flanges are adapted to support the ring gear drive module,wherein the ring gear drive module is configured to permit relative rotation between the mount bracket and the ring gear about the ...

ELECTRONIC SYSTEM FOR THE IDENTIFICATION AND NEUTRALIZATION OF MENACES IN A PREDEFINED AREA

An electronic system for the identification and the neutralization of menaces in a predefined area includes radar detection including at least three discovery radars (RRR) arranged on the vertices of a triangle at a predefined distance among them within the area to be protected. A processing electronic unit (CPU) receives from each of the discovery radars information related to the ballistic menace, for recognizing the ones deriving from the same menace, for each of them, through a triangulation algorithm, for identifying three-dimensional position and speed. 1. Electronic system for identification and neutralization of ballistic menaces in a predefined area through radar detection comprising:at least three discovery radars arranged on vertices of a triangle at a predefined distance among the discovery radars, within said predefined area, each discovery radar being arranged for carrying out a bidimensional detection, producing information on each ballistic menace, said information comprising distance, azimuth and radial speed;a processing electronic unit for receiving from each of said discovery radars information related to the ballistic menace, and for recognizing ones deriving from the same menace, for each of the menaces identifying three-dimensional position and speed through a triangulation algorithm, to provide said data to a control device for a weapon through to direct firing of the weapon and neutralizing the menace.2. The system according to claim 1 , wherein each discovery radar is a pulse Doppler radar.3. The system according to claim 1 , wherein said triangle is an isosceles triangle.4. The system according to claim 1 , wherein said processing unit is associated to one of the three discovery radars that becomes the main radar whereas the other two radars become secondary radars.5. The system according to claim 1 , wherein an interface unit acts as system operative console and communicates with said central processing unit. The present invention refers ...

MOTOR-LESS CARTRIDGE RING GEAR ENGAGEMENT MODULE FOR ACTUATING ROTATION OF A TURRET

Apparatus and associated methods relate to a motor-less cartridge ring gear engagement module (CRGEM) for a turret-rotating system that includes a main drive gear configured to rotate in a rotation plane, a manual input shaft that extends substantially orthogonal relative to the rotation plane, and a drive shaft that extends substantially orthogonal relative to the rotation plane, where the drive shaft and the manual input shaft extend substantially parallel to one another. In an illustrative example, both the main drive gear and a hand crank may be located on a top surface of the CRGEM. In some embodiments, a manual drive cap may be hingedly coupled to the gearbox and configured to rotate in a vertical plane that is substantially orthogonal to the rotation plane. At least some examples may provide for a hand-operated, manual traverse unit that advantageously does not require electrical power to operate. 1. A turret-rotating system comprising:a main drive gear configured to: (1) engage a geared perimeter of a circular ring gear that defines a first plane, (2) rotate in a second plane that is substantially parallel to the first plane, and (3) move relative to the circular ring gear in response to rotation of the main drive gear;a main drive shaft that: (1) is configured to fixedly couple to the main drive gear, and (2) is configured to drive rotation of the main drive gear; and,a manual input shaft that: (1) is configured to rotate in response to a manual user input, (2) is in mechanical communication with the main drive shaft such that rotation of any one of the manual input shaft and the main drive shaft imparts rotation upon the other, and (3) extends along an axis that is substantially orthogonal to the first plane,wherein the turret rotating system comprises a motor-less turret rotating system.2. The turret-rotating system of claim 1 , further comprising a handle configured to mechanically couple to the manual input shaft claim 1 , such that when a user rotates ...

Method for focusing a high-energy beam on a reference point on the surface of a flying object in flight

A method for focusing a beam of a high energy radiation source on a reference point on the surface of a flying object, comprising: recording a number of consecutive two-dimensional images of the flying object determining the trajectory of the flight path simultaneously determining the line of sight angle between the image acquisition device and the position of the flying object calculating a three-dimensional model of the flying object displaying the currently acquired two-dimensional image marking the reference point on the displayed two-dimensional image of the flying object; calculating the three-dimensional reference point on the surface of the flying object focusing the beam of the high energy radiation source on the three-dimensional reference point.

MISSION CONFIGURABLE MOUNTING SYSTEM

A mounting system alternatively configurable as either a mount for a remotely operated weapon, or as a defensive fighting position, including a container portion and a platform assembly portion disposed within the container portion. The platform assembly portion includes a vertically moveable platform selectively attachable to which is a remotely operated weapon mount or a plurality of ballistic wall and roof panels, and frame members for supporting the panels. A lift mechanism is operably connected to the platform, and the platform is moveable by the lift mechanism from a first vertical position to a second vertical position located above the first vertical position. The mounting system has a fully deployed state in the second vertical position in which either the weapon mount or the defensive fighting position structure is supported by the platform and is disposed above the container portion. 1a container portion; and a vertically moveable platform selectively attachable to which is a mount for a remotely operated weapon or a defensive fighting position structure including a plurality of ballistic wall and roof panels, and frame members for supporting the panels, and', 'a lift mechanism operably connected to the platform, the platform moveable by the lift mechanism from a first vertical position to a second vertical position located above the first vertical position;, 'a platform assembly portion disposed within the container portion, the platform assembly portion comprisingwherein the mounting system has a fully deployed state in the second vertical position in which either a remotely operable weapon mount or an occupiable defensive fighting position is supported by the platform and is disposed above the container portion.. A mission configurable mounting system alternatively configurable as either a mount for a remotely operated weapon, or as a defensive fighting position comprising ballistic panels, the mission configurable mounting system comprising: This ...

Automated Human Transported Weapon with Additional Linked Weapons

An automated weapon system [preferably a human transported weapon] is comprised of a barrel, a targeting subsystem, a computational subsystem, a positioning subsystem, and, a firing subsystem. The barrel is utilized for propelling a fired munitions as aimed towards an area of sighting. The targeting subsystem identifies a chosen target in the area of sighting. The computational subsystem, responsive to the targeting subsystem, determines where the chosen target is and where the barrel needs to be aimed so that the munitions will strike the chosen target. The positioning subsystem adjusts the aim of the munitions responsive to the computational subsystem. The firing subsystem, fires the munitions at the chosen target responsive to the positioning subsystem. In one embodiment, the system is further comprised of an additional linked automated weapon having a separate barrel, separate munitions, a separate positioning subsystem, and a separate firing subsystem. The computational subsystem determines the positioning of the separate barrel to shoot the separate munitions to strike the chosen target. The additional linked automated weapon can be mounted on a stationary mount or mounted on a movable mount.

Trainable launcher

A launcher comprising multiple barrels arranged on a rotatable plinth, each barrel configured such that its longitudinal axis can be moved through an arc from a first position where the axis is moveable through a plane substantially orthogonal to the plane in which the plinth and barrel assembly rotates to a second position and wherein one or more of the barrels can be moved independently of others carried on the plinth.

System and method for radar based threat determination and classification

A method for classifying an airborne object detected by a radar system is disclosed. The method includes the steps of identifying quefrency peaks in a quefrency cepstrum generated from a received radar return signal, the quefrency peaks indicative of a rotating physical feature of the airborne object. A rotational velocity of the physical feature is determined based on the quefrency peaks. The method further includes determining at least one parameter or characteristic of a physical feature of the airborne object. The at least one characteristic is compared to a known physical feature stored in a classifier database, wherein a classification decision is made upon identifying a match between the at least one characteristic and a known physical feature stored in the database.

OPTICAL SYSTEM AND METHOD FOR POINTING A LASER THROUGH THE ATMOSPHERE

An optical system for laser-pointing a target through the atmosphere, with four optical channels: a passive imaging channel with an auxiliary camera linked to a coarse pointing control device; an illumination channel with a pulsed illumination source and temporal synchronization means, these channels including a first common optical coarse pointing device; an effector channel with a high-power laser source; an active imaging channel with: a high-speed camera synchronized with the illumination source by the synchronization means, and linked to a fine pointing control device; means for harmonizing the high-speed camera with the high-power laser source; the active imaging and effector channels form a pair and include a second common optical coarse pointing device, the coarse pointing devices controlled by the coarse pointing control device; a common optical fine pointing device, controlled by the fine pointing control device; and the coarse pointing control device is linked to the fine pointing control device. 1. An optical system for laser-pointing a target through the atmosphere , comprising four optical channels:a passive imaging channel with an auxiliary camera capable of obtaining images of the target, and a coarse pointing control device linked to this camera;an illumination channel with a pulsed illumination source and temporal synchronization means;the passive imaging and illumination channels including a first common optical coarse pointing device linked to the coarse pointing control device;an effector channel with a high-power laser source; a high-speed camera synchronized with the illumination source by the temporal synchronization means;', 'means for harmonizing the high-speed camera with the high-power laser source; and', 'a fine pointing control device linked to this high-speed camera, and wherein the active imaging and effector channels form a pair and include, 'an active imaging channel witha second common optical coarse pointing device, the first ...

METHOD OF FIRE CONTROL FOR GUN-BASED ANTI-AIRCRAFT DEFENCE

A method of fire control against aerial targets traveling towards an object of protection. A position of the object of protection is known. A position of the aerial target is measured. The position of the aerial target is estimated. A velocity of the aerial target is estimated. A model of a guidance law of the aerial target is applied. An acceleration of the aerial target sufficient to hit the object of protection is calculated. A future trajectory of the aerial target is predicted based on the position of the object of protection, the estimated position of the aerial target, the estimated velocity of the aerial target, and the calculated acceleration of the aerial target. Points of aim along the predicted future trajectory are calculated. A fire control system includes at least one sensor for measuring the position of the aerial target as a function of time. 1. A method of fire control against aerial targets on their way towards an object of protection , wherein a position of the object of protection is known , the method comprising:measuring a position of the aerial target,estimating the position of the aerial target,estimating a velocity of the aerial target,applying a model of a guidance law of the aerial target,calculating an acceleration of the aerial target sufficient to hit the object of protection,predicting a future trajectory of the aerial target based on the position of the object of protection, the estimated position of the aerial target, the estimated velocity of the aerial target, and the calculated acceleration of the aerial target, andcalculating points of aim along the predicted future trajectory.2. The method of fire control against aerial targets according to claim 1 , wherein the guidance law of the aerial target comprises navigation constants calculated by multiplying an observed acceleration by a predicted time to impact into the object of protection squared claim 1 , divided by a distance from the aerial target to the object of protection.3. ...

Systems and Methods for Obtaining Wind Information

A system and method for determining the wind force along the planned trajectory of a projectile are disclosed herein. A drone is flown along the expected path of the trajectory along a set heading. The drone is programmed to maintain the heading. As wind forces act upon the drone during its flight, the drone's electronic stability system provides automatic power and directional control to one or more motors that control the rotors and propellers that keep the drone aloft. By monitoring the changes in motor or drone state information over time in response to wind forces, the wind can be determined at various locations along the flight path. This information can be provided to a ballistics calculator to determine the launch heading of the projectile.

Semi-autonomous motorized weapon systems

Various techniques are described herein for controlling autonomous and semi-autonomous motorized weapons systems. In various embodiments, semi-autonomous motorized weapons systems may perform automated target identification, selection and prioritization techniques. Dynamic target tracking may be performed, for both primary and secondary targets, in cases of stationary and moving targets and weapon systems. A motorized weapon system then may be actuated automatically toward a firing solution target point, during which the operator-controlled firing mechanism may be enabled or disabled based on the projected point of impact of the weapon in comparison to a determined boundary area associated with the target.

REMOTE CONTROL GUN

The present application provides a remote-controlled gun, comprising a gun base, a gun body, an angle adjustment device, a camera, and a remote controller, wherein the angle adjustment device is connected with the gun body and the gun base, and configured for adjusting a pitch shooting angle of the gun body with respect to the gun base in a vertical plane and a left and right swing angle of the gun body with respect to the gun base in a horizontal plane; the camera is configured for monitoring a shooting target and a front sight of the gun body; the remote controller is connected with the camera and configured for displaying a monitoring image of the camera; and the remote controller is also connected with the angle adjustment device and configured for controlling the gun body to rotate with respect to the gun base until the front sight is aligned with the shooting target within a monitoring area; and the remote controller is also connected with the gun body, and configured for controlling the shooting of the gun body. Compared with the prior arts, this remote-controlled gun makes the user's shooting behavior be changed from operation at site to remote operation, which greatly increases the safety of use; the flexibility of operation be greatly increased, the user can concentrate on a screen of the remote controller to find a target; the aiming be improved, without the need to aim by a naked eye and manual firing, reducing effects due to human factors. 1. A remote-controlled gun , comprising a gun base , a gun body , an angle adjustment device , a camera , and a remote controller ,the angle adjustment device is connected with the gun body and the gun base, and configured for adjusting a pitch shooting angle of the gun body with respect to the gun base in a vertical plane and a left-right shooting angle of the gun body with respect to the gun base in a horizontal plane;the camera is configured for monitoring a shooting target and a front sight of the gun body;the ...

PRACTICAL APPROACH FOR MULTI-OBJECT DETECTION, DATA ASSOCIATION, AND TRACKING

A multiple target tracking, data association, and track file management system (MTT, DA, and TFM) specifically developed for a ground based EO/IR camera proposed in this present disclosure is intended for three main purposes: (1) providing a ground-based combat vehicle with multiple mission capability by adding a new low cost EO/IR sensor with MTT, DA, and TFM functionalities built-in to interact with the ground-based fire control and command guidance for both surface-to-surface and surface-to-air defense missions; (2) serving as a plug-and-play integrated sensor with built-in MTT functionalities easily adaptable to be used for other missions; (3) part of the weapon GN&C subsystem to function in a smart fashion allowing projectiles to work in a collaborative engagement fashion. 1. An improved tracking , targeting , and guidance system , comprising:at least one sensor installed on a vehicle, wherein the sensor is part of a fire control subsystem (FCS);the sensor having an on-board multiple target detection and tracking (MTT), data association (DA), and track file management (TFM) system installed thereon, wherein the multiple target detection and tracking (MTT), data association (DA), and track file management (TFM) system are configured to direct the following operations to deliver one or more correct track files to a guidance system to complete an engagement:process images from the at least one sensor in real-time;detect one or more target location measurements for one or more targets using the images from the at least one sensor to produce potential target tracks;process the one or more target location measurements to determine if the one or more target location measurements from the at least one sensor are correlated with predicted target tracks via the fire control system, if not, then uncorrelated target tracks are placed in a separate file for possible new target track initiation/creation;associate the potential target tracks via a gating system, wherein ...

System integration

A method and apparatus for generating, in an aircraft in flight, a feasibility display indicative of the feasibility of a weapon, the method comprising: providing a performance envelope for the weapon; determining, using the performance envelope, configuration data for configuring a generic algorithm; uploading the configuration data to the aircraft; generating feasibility data N indicative of the feasibility of a weapon carried on the aircraft successfully engaging a target and/or the feasibility of a weapon carried on the target successfully engaging the aircraft; determining, on board the aircraft, using the same generic algorithm and the uploaded configuration data, one or more test criteria; performing, on board the aircraft, an assessment process including determining whether or not the feasibility data satisfies the one or more test criteria; and, based the assessment, using the feasibility data, generating the feasibility display.

CARTRIDGE BASED MODULAR TURRET CONTROL SYSTEM

Apparatus and associated methods relate to a modular cartridge turret assembly system for quickly exchanging modular cartridges to interact with a ring gear. A modular cartridge may be a brake cartridge, which when inserted into a modular cartridge turret assembly, operably engages with the ring gear to inhibit the rotation of a turret. In an illustrative example, the brake cartridge, when inserted, may prevent damages and injuries caused by the rotation of the turret during transportation. In an exemplary embodiment, the modular cartridge turret assembly system may include a locking mechanism to secure the modular cartridge within the modular cartridge turret assembly. The locking mechanism may safeguard that the brake cartridge remains within the modular cartridge turret assembly system during turbulent situations caused by environmental conditions. 1. A modular cartridge apparatus for controlling the operation of a ring gear of a turret , the modular cartridge apparatus comprising:a brake base having a top surface and a bottom surface connected by opposing side walls;a slide flange extending from one of the side walls to define an engagement surface that decreases along a line of travel in the direction of a gravity vector when a ring gear is oriented in a plane orthogonal to the gravity vector, wherein the slide flange is adapted to releasably engage with a slide channel of a cartridge mounting assembly (CMA), wherein the CMA and the ring gear are both supported by a carrier structure; and,a ring gear engagement module extending from the brake base;wherein, when the slide flange is received by the slide channel, the ring gear engagement module engages the ring gear so as to prevent relative movement between the slide flange and the ring gear.2. The apparatus of claim 1 , further comprising a locking mechanism to secure the slide flange when received by the slide channel.3. The apparatus of claim 2 , further comprising a slide flange aperture in the slide flange ...

Unmanned range-programmable airburst weapon system for automated tracking and prosecution of close-in targets

An unmanned range-programmable airburst weapon system provides automated tracking and prosecution of soft targets such as UAVs at close ranges. A range-programmable gun that fires airburst rounds and a seeker that images the target within a FOV are mounted on a gimbaled turret. A tracking controller is responsive to a target cue to point the seeker to acquire the target and to subsequent tracking commands from the seeker to maintain the target in the seeker's FOV. A fire controller is responsive to tracking commands and range-to-target measurements to compute a ballistic firing solution to range program an airburst round and to point and fire the gun so that the round explodes in mid-air at a predicted target position.

MOTOR-DRIVEN AIMING DEVICE AND METHOD

A method of controlling a motor-driven aiming device, the method including the steps of servo-controlling the motor as a function of a difference between a nominal speed setpoint and a measurement of the angular speed sensor, and in the event of saturation, determining a correction value for correcting the nominal speed setpoint as a function of a difference between a reference inertial position prior to the saturation and a current inertial position, and applying the correction value to the nominal speed setpoint. An aiming device for implementing the method. 1. A method of controlling an aiming device comprising a stationary structure having mounted thereon a support so as to be steerable about at least one axis of rotation by means of at least one motor , the support being provided with at least one inertial sensor of angular speed about that axis , the method comprising the steps of:servo-controlling the motor as a function of a difference between a nominal speed setpoint and a measurement of the angular speed sensor, and monitoring for the motor becoming saturated; andin the event of saturation being detected, determining a correction value for correcting the nominal speed setpoint as a function of a difference between a reference inertial position prior to the saturation and a current inertial position, and applying the correction value to the nominal speed setpoint.2. The method according to claim 1 , wherein the correction value is obtained by a correction of the proportional integral correction type.3. An aiming device comprising a stationary structure having mounted thereon a support to be steerable about at least one axis of rotation by means of at least one motor connected to a control unit claim 1 , the device being characterized in that the support is provided with at least one inertial sensor of angular speed about that axis claim 1 , and in that the control unit is arranged:to servo-control the motor as a function of a difference between a nominal ...

Method of Use to Improve Aiming Accuracy for a Firearm

A method of using an apparatus that improves aiming accuracy with manually operated firearm provides a means to support the front part of the firearm's barrel and moving the barrel in parallel with the movements of the firearm's butt. Small rotations of the firearm's muzzle are measured by high resolution angular position sensors and rectified by moving the muzzle mount of the apparatus in horizontal and vertical directions which result in rotation opposite to the measured deviation from correct aiming direction, thus preserving the orientation of the manually operated rifle parallel to desired aiming direction. 1. A method of implementing an apparatus to improve aiming accuracy for a firearm , the method comprises the steps of:providing an apparatus with a muzzle mount for a firearm, wherein said apparatus orients said muzzle mount with a yaw axle and positions said muzzle mount with a horizontal translation mechanism;supporting and aligning said firearm with said muzzle mount along an initial aiming direction;repositioning said firearm with said horizontal translation mechanism in order to reorient said firearm parallel to said initial aiming direction,if said apparatus detects an unintentional rotation in said yaw axle,wherein said unintentional rotation in said yaw axle indicates a horizontal displacement in a butt of said firearm; andrepositioning said firearm with said horizontal translation mechanism,if said apparatus receives a user input through a horizontal control,wherein said horizontal control allows for fine manual adjustments to said horizontal translation mechanism.2. The method of implementing an apparatus to improve aiming accuracy for a firearm claim 1 , the method as claimed in comprises the steps of:measuring said unintentional rotation in said yaw axle with a yaw angular position sensor;proportionately incrementing or decrementing a yaw counter based on a magnitude and a direction for said unintentional rotation in said yaw axle;proportionately ...

MOTORIZED WEAPON GYROSCOPIC STABILIZER

A motorized weapon gyroscopic stabilizer which creates a stabilizing effect for single shot, semi-automatic, and fully automatic weapons. The rotating mass that generates the gyroscopic stabilizing effect is the rotor of the motor. The motor is designed to allow the mass to rotate around the open core of the motorized weapon gyroscopic stabilizer. Because of its open core design the motorized weapon gyroscopic stabilizer allows the fired projectile to pass through it, or be mounted in line with the sighting mechanism allowing the target alignment—line of sight to pass through the motorized weapon gyroscopic stabilizer, or both. 1. A gyroscopic stabilizer system for weaponry , the system comprising:a hollow core mass element having a bore extending therethrough mounted by at least one bearing for rotation around an axis of rotation extending through the bore; anda mounting structure configured to mount the mass element and bearings to an associated weapon such that the axis of rotation is parallel to an axis of a trajectory of a fired projectile;wherein the mounting structure includes a tubular inner housing about which the at least one bearing is supported, the tubular inner housing member extending at least partially into the bore of the hollow core mass element.2. The system according to claim 1 , wherein the mass element is cylindrical and the mounting structure is configured to mount the mass element and at least one bearing for rotation around the trajectory of the fired projectile and/or a line of sight.3. The system according to claim 1 , wherein the mounting structure is configured to mount the mass element and at least one bearing to an accessory which is either permanently affixed or temporarily affixed to the weapon claim 1 , the accessory including at least one of a flash suppressor claim 1 , a sighting mechanism claim 1 , a laser claim 1 , a muzzle brake claim 1 , a sound suppressor claim 1 , a gas tube claim 1 , or a compensator.4. The system according ...

REMOTELY OPERATED TARGET-PROCESSING SYSTEM

A remotely operated target-processing system includes a shooting robot having a stand supporting a firing part having an optoelectronic aiming device providing an image of the target, sensors detecting the relative position of the firing part, and actuators positioning the firing-part. A central unit receives the instructions and the signals from the sensors and generates control signals for the actuators and the firing-part. A control screen displays the image and embeds aiming data, and a control member directs the trajectory line. 16-. (canceled)7. A remotely operated target-processing system , comprising: an optoelectronic aiming device providing an image of a target;', 'sensors that detect the relative position of the firing part; and', 'actuators that position the firing part;, 'a shooting robot having a stand supporting a firing part, the shooting robot further comprisinga central unit that receives instructions and signals from the sensors and that generates command signals for the actuators and the firing part;a control screen that displays the image of the target provided by the optoelectronic device and embeds aiming data in the image; anda control member to direct the trajectory line of the firing part and to control settings of the firing part and shooting of the firing part.8. The system of claim 7 , wherein the central unit executes a gap correction function comprising the steps of:capturing, as the optoelectronic aiming is operating, the image of a target surface and digitising the image and an aiming point;instructing the shooting robot to shoot at the target and to capture the image of the same target surface and to digitise the image with the new position of the aiming point;comparing the images to determine a gap between the aiming point after firing and the aiming point before firing; andgenerating correcting signals to order the movement of the firing part to make the new aiming point coincide with the initial aiming point before firing.9. The ...

AUTONOMOUS UNMANNED TOWER MILITARY MOBILE INTERMODAL CONTAINER AND METHOD OF USING THE SAME

A method for operating a weapon system including the steps of transporting said weapon system to a desired location, wherein said weapon system comprises an intermodal shipping container, providing power to said weapon system, activating a computer processing unit of said weapon system by a remote operator, assembling said weapon system by means of said computer processing unit, raising an unmanned weapons unit by means of a lifting system, wherein a top flap of said intermodal shipping container is opened and wherein said lifting system is capable of raising and lowering said unmanned weapons unit, and transmitting images from a camera system, wherein said camera system coordinates with said unmanned weapons unit. 1. A method for operating a weapon system comprising the steps of: an intermodal shipping container;', 'an unmanned weapons unit configured to fit within the intermodal shipping container;', 'a modular energy source capable of providing power to said weapon system;', 'a modular computing processing unit disposed within said intermodal shipping container;', 'a lifting system, wherein said lifting system is capable of raising said unmanned weapons unit from said intermodal shipping container;', 'a camera system, wherein said camera system is capable of capturing images and communicating said images to said modular computing processing unit; and', 'a recharging station coupled to said modular energy source and disposed on an exterior wall of said intermodal shipping container to provide power;, 'transporting said weapon system to a desired location, wherein said weapon system comprisesproviding power to said weapon system using said modular energy source;activating the modular computer processing unit of said weapon system by a remote operator;activating said weapon system by using said modular computer processing unit;raising said unmanned weapons unit by using said lifting system, wherein a top flap of said intermodal shipping container is opened; ...

Advance security gun with advance coding system

A high-tech security gun that works with Wi-Fi or any other special network, and will not work when it is removed from the address installed by its provider. The gun does not point forward at anyone except it is operated to point at any direction, when controlled wirelessly with a special module. 1. A gun that works with wireless networks with an embodiment that comprises a movable metal hand , a metal part that the said gun is completely installed on , the said gun has a safety compartment , a compartment that is specially designed on its embodiment to conceal the said gun , the said gun can be wirelessly placed in its safety compartment by the user operating the metal hand or part and can be operated out wirelessly by the user operating the metal hand or part , to be drawn out of the safety compartment to point the said gun to any segment or direction aiming or firing at a target , the said gun also called security gun is operated by the user wirelessly on a real time monitoring network with the use of a special internet connectable module also called coding system , the said gun further comprises;a housing with a movable metal hand a part that the said gun is completely installed on;a housing with a safety compartment specially designed to conceal the said gun;a movable metal hand that can be operated to point to any segment upward or downward;a movable metal hand on the embodiment of the said gun that is connected to an internal area built with cranks, bearings, a brake system, an electric motors, and many special moving parts, and special parts and joints;a movable metal hand that can be made hydraulic powered hand with moving parts and joints;an inbuilt cameras on the embodiment of the said gun for aiming shots and monitoring the location of the said gun;an electronics circuits that include a Wi-Fi transceiver, a GPS transceiver, and a GSM transceiver and many special circuits built on a circuit board;an inbuilt laser pointer mounted on the embodiment of the ...

Stabilized integrated commander's weapon station for combat armored vehicle

A weapon station includes a low profile adapter and rotating platform. The low profile adapter is mountable on numerous vehicles or structures, including armored combat vehicles, and mounted concentrically with an operator ingress and egress. The low profile adapter may be mountable on optical sights, such as periscopes. The rotating platform is mounted on the low profile adapter and concentric with the operator ingress and egress and is rotatable about an azimuth axis. The weapon station includes a weapon that can be fired in stabilized, power, and manual modes. The weapon can be fired from within the vehicle in stabilized and power modes, and an operator can fire the weapon manually without leaving the protection of the operator ingress and egress. The weapon station does not obstruct a line-of-sight through optical sights and affords an operator enhanced protection during combat engagements due to its ingress/egress-centric configuration.

Automatic Weapon Subsystem Comprising a Plurality of Automated Weapons Subsystems

An automated weapon system is comprised of a plurality of weapon subsystems; a targeting subsystem; a sensing subsystem; a decision subsystem; a device selection subsystem; and, trigger activation logic. The plurality of weapon subsystems each capable of firing a munition therefrom towards a respective selected target at a respective firing time. The targeting subsystem has a field of view in a target area and provides for identifying at least one said target in the field of view as a selected target. The sensing subsystem provides sensing of the selected target and tracking of location of the selected target through environment in the target area. The decision subsystem, determines where the selected target is located at a firing time responsive to the sensing subsystem. The device selection subsystem determines which of the plurality of weapon subsystems is the selected weapon subsystem in a best position for having munitions fired therefrom to strike the selected target. The trigger activation logic initiates firing of the munitions from the selected weapon subsystem at the firing time, so that the munition will hit the selected target.

Adjustable Sighting and Shooting Firearm Mounting Vise

An adjustable sighting and shooting firearm mounting vise receives a firearm to assist shooters with sighting and discharging the firearm. The firearm mounting vise includes a first base support, a second base support, a pair of positional-adjustment tracks, a forend support, a stock support, a trigger actuator, a trigger switch, a controller housing, a wireless receiver, and a microcontroller. The first base support and the second base support the pair of positional-adjustment tracks. The pair of positional-adjustment tracks allows the forend support, the stock support, and the trigger actuator to translate along each positional-adjustment track to accommodate a plurality of firearms to be secured by the firearm mounting vise. The controller housing protects electrical components including the microcontroller and the wireless receiver. The microcontroller receives control signals through the wireless receiver or directly from the trigger switch to activate the trigger actuator and discharging the firearm. 1. An adjustable sighting and shooting firearm mounting vise comprises:a pair of positional-adjustment tracks being adjacently connected to a forward base support;each positional-adjustment track being adjacently connected to a rear base support;the forward base support being oppositely positioned to the rear base support along each positional-adjustment track;a forend support and a trigger actuator slideably engaging one of the positional-adjustment tracks;a stock support being slideably mounted between each positional-adjustment track;the trigger actuator being positioned between the stock support and the forend support;an at least one linear actuator being adjacently connected between the stock support and the forend support;a controller housing being slideably mounted to one of the positional-adjustment tracks;a trigger switch being adjacently connected to the controller housing;a wireless receiver and a microcontroller being internally mounted to the ...

WEAPON SYSTEM CONTROL HANDLE

An apparatus. The apparatus includes electrical circuitry for selectably controlling a first and a second weapon system different from the first weapon system. The electrical circuitry includes a first switch including a first pole and a pole. The apparatus also includes a first connector having a first terminal coupled to a common terminal of the first pole. A second connector has a first terminal coupled to a common terminal of the second pole. The first connector is configured to couple to a first weapon system mounted on a mobile platform; and the second connector is configured to couple to a second weapon system mounted on the mobile platform. The first weapons system is configured to operate when the first switch is in a first positon and the second weapon system is configured to operate when the first switch is in a second position. 1. An apparatus comprising:a trigger switch;a first relay having a double throw contact, the common terminal of the double throw contact of the first relay coupled to a first terminal of the trigger switch; and when the first relay is in the un-energized state, the common terminal of the double throw contact of the first relay is further connected to a first terminal of the double throw contact of the first relay, the first terminal of the double throw contact of the first relay coupled to a first terminal of a connector coupled to a first weapons system; and', 'when the first relay is in the energized state, the common terminal of the double throw contact of the first relay is further connected to a second terminal of the double throw contact of the first relay, the second terminal of the double throw contact of the first relay coupled to a first terminal of a connector coupled to a second weapons system; and', 'when the second relay is in the energized state, the common terminal of the double throw contact of the second relay is further connected to a first terminal of the double throw contact of the second relay, the first ...

AIMING DEVICE AND METHOD

The present invention relates to a firearm aiming system comprising: an inclinometer measuring at least the angle of elevation of the weapon; a computer comprising a memory of an initial angle of elevation; a ballistics chart included in the computer, which matches a shooting distance with an angle of elevation (a) relative to the initial angle of elevation; a first display device which, when in use, displays for the user the shooting distance as a function of the initial angle of elevation and the instantaneous angle of elevation. 1. An aiming system for a firearm comprising:a clinometer measuring at least an angle of elevation of the firearm;a computer comprising a memory storing an initial angle of elevation;a ballistics chart included in the memory of the computer, wherein the ballistics chart matches a firing distance to a target with an angle of elevation (α) relative to the initial angle of elevation;a first display device which, when in use, displays for a user the firing distance based on the initial angle of elevation and an instantaneous angle of elevation; anda semitransparent surface superposing over the target an image at infinity of a screen displaying the firing distance.2. The aiming system as claimed in claim 1 , comprising a second display device indicating a vertical bore axis.3. The aiming system as claimed in claim 1 , further comprising movable designation means claim 1 , the computer being arranged to move claim 1 , when in use claim 1 , said movable designation means along a vertical axis so as to keep said movable designation means at the initial angle of elevation.4. The aiming system as claimed in claim 3 , wherein said movable designation means are selected from the group consisting of a red dot claim 3 , a reticle and a pointer.5. The aiming system as claimed in claim 1 , further comprising a low-pass frequency filter between the clinometer and the computer claim 1 , operable to stabilize an inclination measurement.6. The aiming system ...

Servo compensation for inertia change

An improvement in the servo drive system as used in a missile director during the elevation function to compensate for changes in inertia. The secant potentiomenter and its associated circuitry is amended to compensate for inertia change as well as changes in elevation angle.

Apparatus and method for analyzing weapon delivery of aircraft

본 발명은 항공기의 무장 투하 해석 장치 및 방법을 개시한다. 본 발명에 따른 항공기의 무장 투하 해석 장치는, 타겟을 조준할 수 있도록 항공기의 조종사에게 가시 거리를 제공하는 조준부, 조준부에 의해서 조준된 타겟에 대한 시야 각도(sighting angle) 및 직거리(slant range)에 대한 정보를 획득하는 조준 센서부, 및 무장의 발사 초기 조건에 따라 무장의 탄착점을 예측하고, 시야 각도 및 직거리에 기초하여 예측된 탄착점으로 투하되는 무장의 비행 궤적을 예측하는 해석부를 포함하고, 해석부는 예측된 비행 궤적을 구성하는 복수의 지점에 대해서 무장의 비행 시간 순서에 따라 무장의 속도 및 위치 값을 순차적으로 보정하고, 보정된 속도 값 및 위치 값에 기초하여 탄착점을 수정할 수 있다. The present invention discloses an apparatus and method for analyzing an armed release of an aircraft. The apparatus for analyzing a weapon of an aircraft according to the present invention includes a sighting part for providing a visual distance to a pilot of an aircraft so as to aim the target, a sighting angle and a slant distance for a target aimed by the sighting part, and an analysis unit for predicting the impact point of the weapon in accordance with the initial conditions of the launch of the weapon and predicting the flight path of the weapon dropped to the predicted impact point based on the view angle and the direct distance, And the analyzing unit sequentially corrects the speed and position value of the weapon according to the order of flight time of the weapon against a plurality of points constituting the predicted flight trajectory and corrects the impact point based on the corrected speed value and the position value have.

Light small arms with automated electro-optical sighting system and aiming method

FIELD: weapons and ammunition. SUBSTANCE: invention relates to weapons. Light small arms with automatic electro-optical sighting system comprises fore grip with butt, barrel, mounted on fore grip with possibility of its position angular change in two mutually perpendicular planes by means of piezoelectric actuator, located between barrel and fore grip in fore grip middle zone, and barrel to fore grip attachment mechanism to fore grip front zone. Gun also comprises electro-optical device with laser range-finder installed with possibility of angular position change relative to barrel in two mutually perpendicular planes and angular position sensors relative to barrel and control unit, made with possibility of manual and/or automated data input on value of angles between barrel axis and electro-optical device optical axis, distance to target, wind speed and direction, temperature and humidity, ammunition ballistic parameters, connected with electro-optical device and actuator. Actuator is installed with help of spring mechanism and made in form of piezoelectric activators, placed in mounting bracket and providing for barrel movement by azimuth and elevation angle. Electro-optical device consists of optical system, light-sensitive matrix and screen. Also disclosed is method of automated electro-optical aiming, according to which at least one of following parameters are input into control unit: distance to target, wind speed and direction, temperature and humidity, ammunition ballistic parameters, produced using electron-optical sensor video signal is processed, using it determining outlines of at least one target and relevant aiming mark, performing preliminary aiming. Then calculating correcting angles between direction of firing by aiming mark and shot hit calculated point, after which generating control signal to actuator piezoelectric activators, converting received signal into barrel angular displacement relative to fore grip at least in one plane. After matching ...

Remote gunshot system and method to observed target

본 발명은 화기와 사람이 이격된 상태에서 은폐된 사람의 관측과 표적선정에 연동하여 화기를 발사 명중시킬 수 있는 원격 화기 사격제어 시스템 및 방법에 관한 것이다. The present invention relates to a remote weapon fire control system and method capable of firing and hitting a firearm in conjunction with observation and target selection of a concealed person in a spaced apart state. 본 발명의 시스템은, 화기에 연결되어 제어신호에 따라 화기를 표적에 조준하고 격발명령에 따라 사격을 개시하며 표적을 촬영하여 표적영상을 전송하는 화기제어장치;와, 상기 화기제어장치와 이격되어 있고, 사격자가 선정한 표적의 위치좌표를 계산하여 표적 좌표정보를 상기 화기제어장치로 전송하며, 상기 화기제어장치로부터 표적영상을 수신받아 표적을 정밀 조준하도록 제어신호를 상기 화기제어장치로 전송하며, 정조준시에 사격명령을 전송하는 원격사격 조정장치를 구비한다. The system of the present invention is connected to a firearm, the firearm control device for aiming the firearm to the target in accordance with the control signal, initiating shooting according to the triggering command and shooting the target to transmit the target image; It calculates the position coordinates of the target selected by the fire target and transmits the target coordinate information to the fire control device, receives a target image from the fire control device and transmits a control signal to the fire control device to precisely aim the target, It is provided with a remote fire control device which transmits a fire command at the time of aiming. 본 발명은 전장에서 화기와 이격된 위치에서 화기를 정밀 조준 사격하는 시스템으로서, 병사의 안전성 증가는 물론 사격효율을 극대화할 수 있고, 정면의 다중표적을 원격지에서 정밀 사격이 가능하므로 현재의 병사에 의한 지역방어체계를 네트웍 기반의 미래전 체계로 발전시키는데 중심역할을 할 수 있다. The present invention is a system for precise aiming and firing a firearm in a spaced apart position on the battlefield, can increase the safety of the soldiers as well as maximize the shooting efficiency, it is possible to precisely shoot the multi-target in front of the current soldiers Can play a central role in developing regional defense systems into network-based future warfare systems. 원격 화기 시스템, 센서, 레이저 거리측정, 유/무선 네트웍 기술 Remote firearm system, sensor, laser distance measurement, wired / wireless network technology

Movable system for intercepting drone and intercept method of drone using the same

본 발명은 이동식 드론 요격 장치 및 이를 이용한 드론 요격 방법에 관한 것으로, 탐지장비(110)가 장착된 감시차량(100)과 화기장비(210)가 장착된 요격차량(200)이 서로 연결되어서 표적 드론(1)을 요격하기 위한 감시장소(5)로 원활히 이동 가능하고, 선회동작과 고각(높이)조절이 가능한 화기장비(210)를 사용해서 표적 드론(1)을 요격하는 구성으로, 공격용 드론에 대해 보다 효과적인 방어체계를 구축할 수 있도록 된 것이다. The present invention relates to a mobile drone intercepting apparatus and a drone intercepting method using the same, wherein a monitoring vehicle 100 equipped with a detection device 110 and an intercepting vehicle 200 equipped with a firearms equipment 210 are connected to each other and target drone It is a configuration that intercepts the target drone (1) using a firearms equipment 210 that can smoothly move to the monitoring location (5) for intercepting (1), and that can adjust the turning motion and height (height). It is possible to build a more effective defense system against

Method for improving geo-pointing performance of electro-optical device in aircraft

본 명세서는 항공기에 장착된 전자광학장비의 좌표 지향 방법을 제시한다. 상기 방법은 관성항법장치(INS)로부터 항공기의 항법 정보 및 상기 항공기의 속도 정보를 수신하는 단계와; 상기 수신한 항법 정보를 기반으로 시선 위치 명령(LOS angle command)을 계산하는 단계와; 상기 수신한 항법 정보 및 표적의 위치 정보에 기반하여 레인지를 계산하는 단계와, 상기 레인지는 상기 항공기와 상기 표적간의 거리이며; 상기 레인지, 상기 항공기의 속도 정보 및 상기 전자광학장비의 시선 각도(LOS angle)에 기반하여 각속도 명령을 계산하는 단계와; 상기 계산된 각속도 명령을 시선제어기에 피드 포워드(feed forward) 방식으로 입력하고, 상기 입력된 각속도 명령 및 상기 시선 위치 명령에 기반하여 상기 전자광학장비의 시선을 제어하는 단계를 포함할 수 있다. This specification presents a coordinate-oriented method of electro-optical equipment mounted on an aircraft. The method includes receiving navigation information of an aircraft and speed information of the aircraft from an Inertial Navigation System (INS); Calculating a LOS angle command based on the received navigation information; Calculating a range based on the received navigation information and the location information of the target; and the range is a distance between the aircraft and the target; Calculating an angular velocity command based on the range, the velocity information of the aircraft, and the LOS angle of the electro-optical equipment; Inputting the calculated angular velocity command to the gaze controller in a feed forward manner and controlling the gaze of the electro-optical device based on the input angular velocity command and the gaze position command.

Fuze system for the height of burst automatically varing and control method thereof

본 발명의 일 실시예에 따르는 신관 시스템은 탄이 발사되면, 신관 내의 발사감지센서가 동작하면서 제어회로부에 발사시점 정보를 전송하는 단계와, 발사시점 정보가 수신되면 제어회로부가 비행시간을 카운트하도록 시한장치를 동작시키고, 비행고도를 측정하는 단계와, 측정된 비행고도와 비행시간으로부터 고도변화율을 구하고, 고도변화율로부터 탄의 사거리를 연산하는 단계와, 연산된 사거리에 근거하여 탄의 하강여부를 판단하고, 탄의 하강시 고도측정구간을 설정하는 단계 및 상기 고도측정구간에 탄이 도달하면 측정된 비행고도들로부터 최종 사거리를 결정하고, 상기 최종 사거리와 메모리에 저장된 사표 자료를 근거로 탄의 폭발고도를 결정하는 단계를 포함한다.

Method for increasing accuracy of firing of a combat vehicle on a target (versions) and a system for its implementation

FIELD: military equipment. SUBSTANCE: invention relates to weapons and military equipment, in particular, to firing of a combat vehicle (CV) along the target. Problem is solved by method of increasing firing accuracy of artillery weapons of combat vehicle (CV) on the target, including selection of a certain type of weapon and type of shot, which is part of the weapon system, using the weapon system control system CV, determination by on-board processor of firing settings control system from mathematical expressions, wherein input parameters are data received from gunner sight (GS) or commander sight (CS), control element respectively GS or CS in "manual" tracking mode of target or automatic tracking device in automatic tracking mode of target, weapon stabilizer, as well as from sensors of external medium, which are part of control system, constant deviation taking into account angular corrections of barrels of the weapon relative to the line of sight during firing on the target. Implementing these methods the weapon system fire control system CV, which comprises first and second adders, gunner sight (GS) or commander sight (CS) indicator, control element respectively GS or CS in "manual" tracking mode of target or automatic tracking in automatic tracking mode of target, control unit, onboard computer, tracking drive and indicator GS or CS, horizontal or vertical guidance drive of weapon stabilizer, feedback sensor, sensors of navigation system and ambient sensors. System is additionally equipped with a device for correcting the initial firing rate. EFFECT: task of the proposed method and implementing its system is to increase accuracy and, accordingly, efficiency of firing weapons CV. 3 cl, 4 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 692 844 C1 (51) МПК F41G 5/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК F41G 5/00 (2019.05) (21)(22) Заявка: 2018131085, 28.08.2018 (24) Дата начала ...

Target simulator with mechanical turn

FIELD: training means. SUBSTANCE: invention relates to simulating devices. Target simulator with mechanical turn comprises radiating antenna, main carriage mounted on fixed guides with toothed rack, drive motor with reduction gear and drive gear of carriage, additional carriage with small-module rack, fixed on it and parts of instrument gear. Instrument transmission provides a constant guidance point of the seeker during carriage movements. EFFECT: control system simplification at synchronization of turn angle at carriage linear motion. 1 cl, 2 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 690 965 C1 (51) МПК G09B 9/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК G09B 9/00 (2019.02); F41G 5/02 (2019.02) (21)(22) Заявка: 2018136139, 12.10.2018 (24) Дата начала отсчета срока действия патента: Дата регистрации: Приоритет(ы): (22) Дата подачи заявки: 12.10.2018 (45) Опубликовано: 07.06.2019 Бюл. № 16 A1, 31.08.1951. SU 1840212 A1, 20.08.2006. RU 2012845 C1, 15.05.1994. SU 47457 A1, 30.06.1936. (54) Имитатор цели с механическим доворотом (57) Реферат: Изобретение относится к моделирующим устройствам. Имитатор цели с механическим доворотом содержит антенну-излучатель, основную каретку, установленную на неподвижные направляющие с зубчатой рейкой, приводной электродвигатель с редуктором и приводной шестерней каретки, дополнительную R U 2 6 9 0 9 6 5 (56) Список документов, цитированных в отчете о поиске: SU 1370435 A1, 30.01.1988. SU 84963 Стр.: 1 каретку с закрепленной на ней мелкомодульной зубчатой рейкой, деталями приборной передачи. Приборная передача обеспечивает постоянную точку наведения ГСН при перемещениях каретки. Технический результат – упрощение системы управления при синхронизации угла доворота при линейном движении каретки. 2 ил. C 1 C 1 Адрес для переписки: 125319, Москва, ул. Викторенко, 7, ФГУП "ГосНИИАС", Патентное подразделение, Протасенко Г.А. 2 6 9 0 9 6 5 (73) Патентообладатель(и): ...

Laser-sight and computer for anti-aircraft gun fire control system

A gun fire control system for pointing a gun at rapidly moving targets such as an aircraft is disclosed. The system comprises a vibration isolated control unit including a gunner''s sight assembly which is provided with line of sight indicating instrumentation and uses common optical elements both for visual sighting by the gunner to generate manual acquisition commands and for a continuously operable laser transmitter-receiver rangefinder. The control unit also includes a solid state hybrid computer for providing continuous implicit separate solutions of lead angle equations and aided tracking equations respectively, and for generating commands for directing the fire of the gun in response to signals derived from solution of appropriate lead angle equations, and supplied to gun servos. The computer uses signals derived from the rangefinder in its automatic tracking aid circuits to generate commands to the sight assembly, but the gunner retains override and trim capability over these commands. Measurement of the velocity vector of the moving target is made in a moving coordinate system having one of its three mutually orthogonal axes always lying along the line of sight from the gunner to the target. The measured vector components of target velocity expressed in this first moving coordinate system are then transformed to quantities expressed in a second inertial coordinate system having its origin at the position of the gun and the observer and one axis lying along the local gravitational vector in order to generate the appropriate tracking aid commands and to afford a more accurate basis for the real time continuous solution of the three simultaneous lead angle equations.

A kind of the firefighting cartridge launcher and adjusting method of adjustable pitching and orientation

本发明涉及一种可调俯仰和方位的消防弹发射架及调节方法，属于飞行器发射技术领域，解决了现有发射架无法进行俯仰和方位调节的技术问题。本发明的可调俯仰和方位的消防弹发射架，包括：弹体安装挂架、调平水准器、俯仰调节单元以及方位调节单元；弹体安装挂架、调平水准器、俯仰调节单元以及方位调节单元自上而下依次设置；俯仰调节单元包括俯仰单元连接板、俯仰调节单元右侧板、蜗轮蜗杆减速器、主动转轴、连接块、锁紧螺母、滚动轴承、俯仰调节单元左侧板和被动转轴；方位调节单元包括方位调节连接板、立柱、基板、锁紧旋钮、底座和推力球轴承。本发明的可调俯仰和方位的消防弹发射架能够进行俯仰调节和方位调节。

Real-time digital automatic boresighting system

본 발명은 실시간 디지털 자동조준감사장치에 관한 것으로서, 특히, 일정 단위 시간별 자동으로 제어/보정하는 실시간 디지털 자동조준 감사장치에 관한 것이다. 본 발명에 따른 실시간 디지털 자동조준감사장치는, 주포 레이저 빔; 조준선 보정장치; 탄도계산장치; 및 사격통제전자유닛을 구비하며, 포수조준경 조준선, 전차장 조준경 조준선과 주포 조준점간의 오차를 조준선 보정장치에 의해 발생되는 DCT 값을 직접 탄도계산장치에 의해 계산하여 사격통제유닛으로 전달하기 때문에, 조준경의 보정과정, 즉, 조준감사를 간단하게 행할 수 있다. The present invention relates to a real-time digital automatic aiming audit device, and more particularly, to a real-time digital automatic aiming audit device that automatically controls / corrects for a predetermined unit of time. Real-time digital automatic aiming and auditing device according to the invention, the gun laser beam; Aiming line correction device; Ballistic calculator; And a fire control electronic unit, and calculates the error between the gun sight sight, the commander's sight sight and the gun aiming point, and calculates the DCT value generated by the sight line compensator directly to the fire control unit, The calibration process, that is, the aiming audit, can be performed simply. 전차, 조준감사 Tank, aiming audit

Method and apparatus for selecting target from radar tracking data

FIELD: physics. SUBSTANCE: data source provides tracking data for at least one possible target in real time, from which can be selected the leading route associated with one target which satisfies a predetermined threshold condition for attack by an electronic jamming system. EFFECT: high accuracy of selecting a target from radar tracking data. 9 cl, 2 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) 2 463 621 (13) C2 (51) МПК G01S 7/36 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (21)(22) Заявка: 2009146042/07, 14.05.2008 (24) Дата начала отсчета срока действия патента: 14.05.2008 (73) Патентообладатель(и): РЭЙТЕОН КОМПАНИ (US) R U Приоритет(ы): (30) Конвенционный приоритет: 14.05.2007 US 60/917,782 (72) Автор(ы): МАКГУАЙР Патрик М. (US) (43) Дата публикации заявки: 20.06.2011 Бюл. № 17 2 4 6 3 6 2 1 (45) Опубликовано: 10.10.2012 Бюл. № 28 (56) Список документов, цитированных в отчете о поиске: US 20030228032 A1, 11.12.2003. US 7104496 B2, 12.09.2006. RU 2207589 C2, 27.06.2003. RU 42302 U1, 27.11.2004. FR 2734368 A1, 22.11.1996. 2 4 6 3 6 2 1 R U (86) Заявка PCT: US 2008/063604 (14.05.2008) C 2 C 2 (85) Дата начала рассмотрения заявки PCT на национальной фазе: 14.12.2009 (87) Публикация заявки РСТ: WO 2009/023322 (19.02.2009) Адрес для переписки: 129090, Москва, ул.Б.Спасская, 25, стр.3, ООО "Юридическая фирма Городисский и Партнеры", пат.пов. А.В.Мицу, рег.№ 364 (54) СПОСОБЫ И УСТРОЙСТВО ДЛЯ ВЫБОРА ЦЕЛИ ИЗ ДАННЫХ РАДИОЛОКАЦИОННОГО СОПРОВОЖДЕНИЯ (57) Реферат: Способы и устройство для выбора цели из радиолокационных данных в соответствии с различными особенностями настоящего изобретения работают в сочетании с источником данных в реальном масштабе времени и системой радиоэлектронного подавления. Источник данных в реальном масштабе времени предоставляет данные слежения, по меньшей мере, для одной возможной цели, из которых может выбираться ведущий маршрут, ассоциированный с одной целью, удовлетворяющий заранее установленному ...

Method of fire control for gun-based anti-aircraft defence

본 발명은 보호 대상물의 위치를 알고 있는 상태에서, 보호 대상물로 향하여 다가오는 공중 표적에 대한 사격 통제 방법으로서, 공중 표적의 위치를 측정하는 단계와, 공중 표적의 위치를 추정하는 단계와, 공중 표적의 속도를 추정하는 단계와, 공중 표적의 유도 법칙의 모델을 적용하는 단계와, 보호 대상물을 타격하기 위해 공중 표적이 적용해야 하는 가속도를 계산하는 단계와, 보호 대상물의 위치, 공중 표적의 추정된 위치, 공중 표적의 추정된 속도, 공중 표적의 계산된 가속도에 기초하여 공중 표적의 미래 궤적을 예측하는 단계와, 상기 예측된 궤적에 따라 조준점을 계산하는 단계를 포함한 사격 통제 방법에 관한 것이다. 또한, 본 발명은 시간의 함수로서 공중 표적의 위치를 측정하는 적어도 하나의 센서를 포함한 공중 표적에 대한 사격 통제용 사격 통제 시스템에 관한 것이다.

Method of remote detonation of projectile

FIELD: weapons and ammunition.SUBSTANCE: invention relates to munitions of barrel artillery and can be used in fuses of artillery shells. Method of remote detonation of the projectile consists in the fact that several sensors are installed in the fuse of the projectile and with their help determine the parameters of the flight of a specific projectile, that set the response time of the remote fuse. Sensor is installed to continuously monitor the atmospheric pressure in the projectile zone as a function of time. Position sensor is used to record the change in the position of the nose of the projectile relative to the horizon line and the bottom of the projectile. Connect all sensors and the device for positioning the projectile to the fuse device. Produce a shot with a projectile. During the flight of the projectile, the data from the sensors installed in the fuse are continuously analyzed. With the help of the computing device, a control pulse is generated according to a predetermined algorithm, that is applied to the fuse device. Fuse device is equipped with a temporary timer, that operates from the moment the projectile emits from the barrel bore.EFFECT: invention makes it possible to reduce the field of scattering of projectiles.1 cl, 3 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 666 378 C1 (51) МПК F41J 5/00 (2006.01) F41G 5/06 (2006.01) G01S 13/50 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК F41G 5/00 (2006.01); F41G 5/06 (2006.01); G01S 13/50 (2006.01) (21)(22) Заявка: 2017143423, 12.12.2017 (24) Дата начала отсчета срока действия патента: 07.09.2018 Приоритет(ы): (22) Дата подачи заявки: 12.12.2017 применения дистанционных взрывательных устройств, Научно-технический сборник ГНЦ РФ ФГУП "ЦНИИХМ им. Д.И. Менделеева", Боеприпасы, N1, 2016, с. 64-68. RU 2205353 C2, 27.05.2003. RU 2230277 C1, 10.06.2004. RU 2564686 C1, 10.10.2015. RU 2565834 C1, 20.10.2015. US 3324468 A1, 06.06.1967. (45) Опубликовано ...

Guidance and stabilization system

FIELD: automatic control system. SUBSTANCE: invention relates to the field of automatic control systems and can be used in guidance and stabilization systems of weapons and optoelectronic devices of infantry combat vehicles, antiaircraft-missile and antiaircraft-rocket-gun complexes. Essence of the disclosed solution lies in the fact that a guidance and stabilization system comprising a first integrator, series-connected adder, adder amplifier, power amplifier and actuating motor, a first rate gyroscope, a second rate gyroscope, a first multiplier unit, first input of which is connected to second rate gyroscope output, second input is connected to first integrator output, second integrator, input of which is connected to first multiplier output, second multiplier, first input of which is connected to second rate gyroscope output, second input is connected to second integrator output, and output is connected to adder second input, wherein adder first input is connected to first integrator output, the output of the first rate gyroscope and the output of the rate generator are connected to the second and third inputs of the summing amplifier, the rate generator input is mechanically connected to the output of the actuator. EFFECT: technical result when implementing disclosed solution consists in improvement of stabilization accuracy. 1 cl, 1 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 735 789 C1 (51) МПК F41G 5/00 (2006.01) F41F 3/04 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК F41G 5/00 (2020.08); F41G 3/04 (2020.08); F41G 7/24 (2020.08) (21)(22) Заявка: 2020109439, 03.03.2020 (24) Дата начала отсчета срока действия патента: Дата регистрации: Приоритет(ы): (22) Дата подачи заявки: 03.03.2020 (56) Список документов, цитированных в отчете о поиске: RU 2294515 C1, 27.02.2007. RU 2207487 C1, 27.06.2003. RU 7489 U1, 16.08.1998. Учебное пособие: "Автоматические системы управления вооружением", Изд-во ОмГТУ, ...

Gun fire control system

내용 없음. No content.

Servo drive

FIELD: automatic control.SUBSTANCE: invention relates to the field of automatic control, namely to drives for guidance and stabilization of inertial objects, for example, to the artillery armament drives of movable objects. Tracking drive comprises devices that provide short-term disconnection of control signal at input of actuator at the moment of change of control sign at input of error signal former.EFFECT: improved servo drive reliability in reverse motion mode.1 cl, 2 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 723 331 C1 (51) МПК G05B 13/02 (2006.01) F15B 9/00 (2006.01) F15B 9/17 (2006.01) F41G 5/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК G05B 13/02 (2020.02); F15B 9/00 (2020.02); F15B 9/17 (2020.02); F41G 5/00 (2020.02) (21)(22) Заявка: 2019118508, 14.06.2019 (24) Дата начала отсчета срока действия патента: Дата регистрации: 09.06.2020 (73) Патентообладатель(и): Акционерное общество "Всероссийский научно-исследовательский институт "Сигнал" (RU) (45) Опубликовано: 09.06.2020 Бюл. № 16 (54) Следящий привод (57) Реферат: Изобретение относится к области автоматического регулирования, а конкретно к приводам наведения и стабилизации инерционных объектов, например приводам наведения артиллерийского вооружения подвижных объектов. Следящий привод содержит устройства, которые обеспечивают кратковременное R U 2 7 2 3 3 3 1 (56) Список документов, цитированных в отчете о поиске: RU 2664866 C1, 23.08.2018. SU 802924 А2, 07.02.1981. SU 1068889 А1, 23.01.1984. RU 2473822 С2, 27.01.2013. RU 2529965 С1, 10.10.2014. DE 10135220 А1, 20.02.2003. Стр.: 1 C 1 C 1 Адрес для переписки: 601903, Владимирская обл., г. Ковров, ул. Крупской, 57, АО "ВНИИ "Сигнал" 2 7 2 3 3 3 1 Приоритет(ы): (22) Дата подачи заявки: 14.06.2019 R U 14.06.2019 (72) Автор(ы): Бабкин Алексей Валерьевич (RU), Ловушкин Юрий Анатольевич (RU), Путилин Константин Сергеевич (RU), Смирнов Александр Юрьевич (RU), Смирнов Борис Алексеевич (RU), ...

Device for automatic control of coupled machine gun

Изобретение относится к области военной техники, в частности к конструкциям установок, наводящих оружие в горизонтальной и вертикальной плоскостях. Устройство автоматического управления спаренным пулеметом содержит станок с подвижной и неподвижной частями, установку с оружием, размещенную на подвижной части, закрепленный на неподвижной части привод горизонтального наведения, механизм вертикального наведения, кинематически связывающий привода с установкой. Установка разделена на первую и вторую части, соединенные соответственно через первую и второю части механизма вертикального наведения с первым и вторым приводами этого механизма. Стволы соответственно размещены на первой и второй частях установки. Достигается расширение функциональных возможностей и улучшение эксплуатационных характеристик устройства управления. 8 з.п. ф-лы, 4 ил. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 642 222 C2 (51) МПК F41A 27/00 (2006.01) F41G 5/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ На основании пункта 1 статьи 1366 части четвертой Гражданского кодекса Российской Федерации патентообладатель обязуется заключить договор об отчуждении патента на условиях, соответствующих установившейся практике, с любым гражданином Российской Федерации или российским юридическим лицом, кто первым изъявил такое желание и уведомил об этом патентообладателя и федеральный орган исполнительной власти по интеллектуальной собственности. (52) СПК (21)(22) Заявка: 2016115649, 21.04.2016 (24) Дата начала отсчета срока действия патента: (73) Патентообладатель(и): Оленев Евгений Александрович (RU) Дата регистрации: 24.01.2018 (56) Список документов, цитированных в отчете о поиске: RU 2384809 C1, 20.03.2010. RU Приоритет(ы): (22) Дата подачи заявки: 21.04.2016 (43) Дата публикации заявки: 26.10.2017 Бюл. № 30 2088877 C1, 27.08.1997. RU 2256138 C1, 10.07.2005. US 2011/0030544 A1, 10.02.2011. RU 2054154 C1, 10.02.1996. US 5570606, 05.11.1996. 2 6 4 2 2 2 2 R U ...

Night sighting device for vulcan using thermal camera and method thereof

본 발명은 열 영상 카메라를 이용하는 발칸포용 야간조준기 및 그 방법에 관한 것으로서, 상기 열 영상 카메라를 이용하는 발칸포용 야간조준기는 표적에서 방출되는 적외선 에너지를 검출하고, 상기 검출된 적외선 에너지를 열 영상 데이터로 변환하여 출력하는 열 영상 카메라, 상기 열 영상 카메라에 부착 되어 상기 열 영상 카메라가 상기 표적을 향하도록 회전시키는 선도각 구동부 및 상기 열 영상 카메라에서 변환된 열 영상 데이터를 화면에 전시하는 모니터를 포함하도록 구성될 수 있다. 또한, 상기 발칸포용 야간조준기는 상기 변환된 열 영상 데이터에 탐지 추적 알고리즘을 적용하여 영상 내에 위치한 표적을 탐지하고, 상기 탐지된 표적 데이터를 상기 모니터로 출력하는 자동 표적 탐지부를 더 포함할 수 있다. 상기와 같은 열 영상 카메라를 이용하는 발칸포용 야간조준기 및 그 방법에 따르면, 발칸포의 야간 운용 시 야시장비보다 탐지거리 및 화질이 좋은 열 영상 카메라를 이용함으로써, 온도차를 이용하여 사물을 명확하게 구분하고 식별할 수 있으며, 야간뿐만 아니라 주간에도 운용이 가능하고 연막, 먼지 또는 포연 등이 있는 실제 야전전투조건에서도 투과관측이 가능하여 전투능력을 극대화할 수 있다. The present invention relates to a night vision apparatus for a tocano camera using a thermal imaging camera, and a night vision apparatus using the thermal imaging camera for detecting a infrared energy emitted from a target, and for converting the detected infrared energy into thermal image data And a monitor for displaying the thermal image data converted by the thermal image camera on the screen, wherein the thermal image camera is attached to the thermal image camera and rotates the thermal image camera so as to face the target Lt; / RTI > The night vision target for the forklift may further include an automatic target detection unit for detecting a target located in the image by applying a detection tracking algorithm to the converted thermal image data and outputting the detected target data to the monitor. According to the night sneaker for a tokuno using the thermal imaging camera and the method thereof, by using a thermal image camera having a better detection range and a better image quality than the night view equipment in nighttime operation of the volcano, And can be operated in the daytime as well as at night, and it is possible to observe penetration even in actual field combat conditions such as smoke, dust, or smoke, thereby maximizing the combat ability.

Method for illuminating a target to ensure the use of ammunition with a laser semi-active homing head

FIELD: high-precision weapons. SUBSTANCE: invention relates to means of ensuring the use of high-precision weapons with a laser semi-active homing head. The method includes determining the topographic coordinates of the target designator and firing position, detecting and measuring the spherical coordinates of the target with the target designator, determining the topographic coordinates of the target, calculating and implementing firing settings, firing an ammunition shot. The hardware components used are mounted on a quadcopter capable of hovering over a target. A laser target illuminator made as a separate component is installed on the quadcopter in the nadir position, which is ensured by the self-orientation of the illuminator due to gravity. For this, the illuminator is fixed at the lower end of a rigid rod, the upper end of which is attached to the bottom of the quadcopter by means of a hinge joint. The height of the quadcopter hovering over the target is determined by the values ​​of the angle of divergence of the laser beam of the illuminator and the minimum planned overall size of the target. EFFECT: ease of implementation and expansion of the scope of laser target illumination for high-precision homing ammunition. 1 cl, 1 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 755 134 C1 (51) МПК F41G 5/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК F41G 5/00 (2021.05); F41G 7/34 (2021.05) (21)(22) Заявка: 2021104397, 20.02.2021 (24) Дата начала отсчета срока действия патента: (73) Патентообладатель(и): Открытое акционерное общество "РАДИОАВИОНИКА" (RU) Дата регистрации: 13.09.2021 (56) Список документов, цитированных в отчете о поиске: RU 2584210 C1, 20.05.2016. RU 2726460 C1, 14.07.2020. RU 2635299 C1, 09.11.2017. US 10215534 B1, 26.02.2019. JP 2002341032 A, 27.11.2002. (45) Опубликовано: 13.09.2021 Бюл. № 26 2 7 5 5 1 3 4 R U (54) Способ подсвета цели для обеспечения применения боеприпасов с лазерной ...

Method and motorized aiming device

FIELD: means of guidance. SUBSTANCE: group of inventions refers to a motorized aiming or orientation of an element in a predetermined direction and, in particular, to aligning the implement with a line of sight. Method for controlling the pickup device comprises the steps of automatically adjusting the motor drive depending on the difference between the nominal speed setpoint and the angular velocity sensor measurement, and in the case of saturation, the correction value of the nominal speed setpoint is determined, depending on the deviation between the reference inertial position before saturation and the current inertial position and apply the correction value to the nominal set speed. EFFECT: increase the accuracy of alignment of the motorized bracket in the event of a shock or any other physical phenomenon resulting in engine saturation. 4 cl, 2 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 658 555 C1 (51) МПК F41G 5/06 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК F41G 5/06 (2006.01) (21)(22) Заявка: 2018103946, 01.07.2016 (24) Дата начала отсчета срока действия патента: (73) Патентообладатель(и): САФРАН ЭЛЕКТРОНИКС ЭНД ДИФЕНС (FR) Дата регистрации: 21.06.2018 2002074486 A1, 20.06.2002. DE 102013006939 A1, 23.10.2014. RU 2045734 C1, 10.10.1995. 03.07.2015 FR 1556304 (45) Опубликовано: 21.06.2018 Бюл. № 18 (85) Дата начала рассмотрения заявки PCT на национальной фазе: 05.02.2018 (86) Заявка PCT: 2 6 5 8 5 5 5 R U (87) Публикация заявки PCT: WO 2017/005656 (12.01.2017) C 1 C 1 EP 2016/065586 (01.07.2016) 2 6 5 8 5 5 5 (56) Список документов, цитированных в отчете о поиске: US 2001039874 A1, 15.11.2001. US Приоритет(ы): (30) Конвенционный приоритет: R U 01.07.2016 (72) Автор(ы): ТЬЕФРИ Ролан (FR) Адрес для переписки: 109012, Москва, ул. Ильинка, 5/2, ООО "Союзпатент" (54) СПОСОБ И МОТОРИЗОВАННОЕ УСТРОЙСТВО НАВОДКИ (57) Реферат: Группа изобретений относится к заданного значения скорости в зависимости от ...

Shooting Control System and Method Using Thereof

사격 제어 시스템 및 이를 이용하는 사격 제어 방법이 개시된다. 본 발명의 일 실시예에 따른 사격 제어 시스템은, 사격 목표물을 촬영하고 상기 목표물까지의 거리 및 선회각의 크기를 측정하는 촬영 장치, 상기 목표물을 사격하는 사격 장치 및 상기 촬영 장치로부터, 상기 촬영 장치, 상기 사격 장치 및 상기 목표물의 위치 정보를 수신하고, 수신한 상기 위치 정보를 이용하여 상기 사격 장치의 사격 동작을 제어하는 제어부를 포함하고, 상기 제어부는 상기 촬영 장치의 위치 및 촬영 방향을 제어하고, 상기 사격 장치의 위치 및 사격 방향을 제어한다. A shooting control system and a shooting control method using the same are disclosed. A shooting control system according to an embodiment of the present invention is a shooting control system that includes a shooting device shooting a shooting target and measuring a distance to the target and a magnitude of a turning angle, a shooting device shooting the target, And a control unit for receiving the position information of the shooting device and the target and controlling the shooting operation of the shooting device using the received position information, wherein the control unit controls the position and the shooting direction of the shooting device , The position of the shooting device and the shooting direction.

Method of aircraft control with satellite navigation equipment and device for its implementation

FIELD: aircraft engineering. SUBSTANCE: invention relates to control, in particular to guided weapons, it can be useful in aircraft control systems, shells and missiles, in which the flight trajectory in the initial and middle sections is corrected according to the data of the signals receiver from a navigation spacecraft. To do this, the definition of the current coordinates of the aircraft is duplicated by a second satellite navigation equipment in which the antenna axis of the receiving antenna is rotated about the axis of the receiving antenna of the first satellite navigation equipment by an angle, in which the total radiation pattern of a system of two receiving antennas provides in all directions a directivity factor of at least 0.5, while the number of visible satellites in navigation and the geometric factor of their position (GDOP), determined by the first and second satellite navigation equipment, the level of reliability of navigation information is assessed, and the correction of the flight trajectory of the aircraft is carried out at the current coordinates determined by the satellite navigation equipment with a higher level of reliability. In this case, in the control system of an aircraft, the assigned task is achieved due to the fact that the aircraft is equipped with a second satellite navigation equipment with a receiving antenna, connected in series by a comparison unit and a switch whose output is connected to the input of the on-board calculator, the first output of the first satellite navigation equipment and the first output of the second satellite navigation equipment being connected to the first and second inputs of the comparison unit, respectively, and the second output of the first satellite navigation equipment and the second output of the second satellite navigation equipment are respectively connected to the second and third switch inputs. EFFECT: technical result is higher reliability of communication between the aircraft and the ...

Firing apparatus and method for compensating an aiming angle thereof

본 발명은 무장 장치 및 이의 조준 각도 보상 방법에 관련된 것이다. 본 발명의 일 측면에 따른 무장 장치는 프레임과, 상기 프레임에 결합되며, 목표물의 영상을 촬영할 수 있는 카메라와, 상기 카메라의 주시 방향에 대하여 상대적으로 발사 방향의 변동이 가능하도록 상기 프레임에 결합되며 상기 카메라와 이격되게 배치되는 화기와, 상기 프레임에 결합되며 상기 목표물까지의 거리를 측정할 수 있는 거리 측정 장치와, 상기 목표물까지의 거리 및 상기 화기와 상기 카메라와의 이격 거리를 이용하여 상기 화기의 발사 방향의 보상 값을 산출하는 연산부를 구비한다. The present invention relates to an arming apparatus and a method for compensating aiming angle thereof. A weapon device according to one aspect of the present invention includes a frame, a camera coupled to the frame, a camera capable of capturing an image of a target, and a camera coupled to the frame such that a variation in a firing direction relative to a viewing direction of the camera is possible A distance measuring device coupled to the frame and capable of measuring a distance to the target; and a distance measuring device that measures a distance to the target and a distance between the camera and the firearm, And a calculation unit for calculating a compensation value in a shooting direction of the vehicle.

Aiming system for automatic shooting

본 발명은 쌍안경을 통해 목표물을 주시하고 확인 보턴을 누르면 자동으로 목표물을 향해 총열을 조준하는 자동사격 조준장치에 관한 것으로서, 본 발명에 의한 자동사격 조준장치에 의하면 사격을 위한 목표물을 향한 총열의 조준이 자동적으로 이루어지므로써 비숙달된 사격자도 정확한 사격을 할 수 있다는 뛰어난 효과가 있다. The present invention relates to an automatic shooting aiming apparatus for automatically aiming a barrel toward a target by pressing the confirmation button and watching the target through binoculars. This is done automatically so that an unskilled shooter can have an accurate shot.

SUPERSONIC AIRCRAFT AND METHOD FOR IMPLEMENTING ITS FLIGHT

1. Сверхзвуковой летательный аппарат, содержащий стартовый двигатель с механизмом разделения ступеней, маршевую ступень с функциональными блоками, отличающийся тем, что маршевая ступень помещена в защитный обтекатель, раскрывающийся при отделении двигателя, а планер маршевой ступени выполнен по самолетной схеме «низкоплан» с элементами вертикального оперения, обеспечивающими устойчивость планера по крену, заневоленными защитным обтекателем и переходящими в рабочее положение при его раскрыве.2. Способ реализации полета сверхзвукового летательного аппарата, в котором используют программируемую амплитуду рикошетирования, при этом на этапе погружения в атмосферу изменение вектора аэродинамической силы осуществляют путем выбора оптимального угла атаки, соответствующего достижению максимальной дальности полета аппарата, отличающийся тем, что запуск летательного аппарата осуществляют с наземной пусковой установки под траекторным углом от 50 до 85° к горизонту, и летательный аппарат выводят по баллистической траектории в разреженные слои атмосферы на высоты от 50 до 70 км. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2015 115 561 A (51) МПК F41G 5/00 (2006.01) F42B 15/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ЗАЯВКА НА ИЗОБРЕТЕНИЕ (21)(22) Заявка: 2015115561, 24.04.2015 (71) Заявитель(и): Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации (RU) Приоритет(ы): (22) Дата подачи заявки: 24.04.2015 (43) Дата публикации заявки: 20.11.2016 Бюл. № 32 A 2 0 1 5 1 1 5 5 6 1 R U Стр.: 1 A (57) Формула изобретения 1. Сверхзвуковой летательный аппарат, содержащий стартовый двигатель с механизмом разделения ступеней, маршевую ступень с функциональными блоками, отличающийся тем, что маршевая ступень помещена в защитный обтекатель, раскрывающийся при отделении двигателя, а планер маршевой ступени выполнен по самолетной схеме «низкоплан» с элементами вертикального оперения, обеспечивающими устойчивость планера по крену, ...

Line-of-sight stabilising system

FIELD: physics. SUBSTANCE: invention relates to automatic control and regulation systems, in particular to gyrostabilizing devices, and is used to provide stabilisation of the view field and control of the line of sight of optical devices (sights) deployed on mobile military targets such as tanks, IFV, AAV, APCs, etc. The stabilisation system contains an aiming complex with control and power electronics connected to an external control signal, sensors, an engine electrically connected to the first output of the control and power electronics, optical nodes and mechanisms. Herewith the system is divided into an electric unit located in the OBD and containing control and power electronics and an electromechanical unit located in the aiming complex mounted on the OBD and containing sensors, a motor, optical nodes and mechanisms, as well as a memory unit and a serial memory port. Elements of the stabilisation system are connected according to the block diagram in Fig. 1. EFFECT: increasing operational capabilities due to the preservation of structural installation dimensions in the modernized military facility with the installation of a new sighting complex with an independent line of sight, improving the maintainability of the military facility under operating conditions, when installing a modernized sighting system with an independent line of sight. 1 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 627 563 C1 (51) МПК G01C 21/18 (2006.01) F41G 5/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (21)(22) Заявка: 2016112878, 04.04.2016 (24) Дата начала отсчета срока действия патента: 04.04.2016 Дата регистрации: Приоритет(ы): (22) Дата подачи заявки: 04.04.2016 (45) Опубликовано: 08.08.2017 Бюл. № 22 Адрес для переписки: 601919, Владимирская обл., г. Ковров, ул. Крупской, 55, ОАО "Специальное конструкторское бюро приборостроения и автоматики", БПИР (56) Список документов, цитированных в отчете о поиске: RU 2430392 C1 27.09 ...

Electrically driven turret test system

An electrically driven turret test system is provided to judge whether test equipments are normal or not by extracting contents of communication signals between test equipments in a turret without interrupting a signal flow. An electrically driven turret test system(100) comprises a power supply unit(110) for supplying power to each test equipment(150,160) in a turret; a break out box(120) for receiving signals including a CAN signal(170) and an RS422 signal(180) from test equipments in the turret, extracting only the desired contents from the received signals, and transmitting the extracted contents to a data acquisition unit(140); a coupler(130) for receiving signals including an MIL-1553B signal(190) from test equipments in the turret, extracting only the desired contents from the received signals, and transmitting the extracted content to the data acquisition unit; and the data acquisition unit for judging whether test equipments in the turret are normal or not on the basis of the signal acquired from the break out box and the coupler.

Method of calculating firing settings of a guided projectile with a laser semi-active homing head in cloud conditions

FIELD: military equipment. SUBSTANCE: invention relates to military equipment, in particular to guided artillery projectiles (GAP) and guided missiles with laser half-active homing heads (HH). Method for calculating firing settings of a guided projectile with a laser semi-active HH in cloud conditions includes inputting a target and instruments into the coordinate command console, as well as values of ballistic corrections, measurement and subsequent input of atmospheric pressure, temperature, speed and direction of wind into commander's console, measurement of height of lower boundary of cloudiness and input of its value into commander's panel, calculation in command console of firing settings, determination of guided missile trajectory height under current conditions and calculated firing installations, determination of trajectory height in target capture time of target HH of projectile, comparison of flight height of guided projectile with height of terrain, adjustment of firing settings taking into account this comparison. For the given terrain relief, the calculated flight path of the guided projectile is compared at the calculated moment of capturing the target HH with the height of the lower cloud boundary and, if it exceeds the height of the lower cloud boundary, firing settings are selected from the memory of the commander's console and simultaneously meet requirements that the height of the trajectory of the projectile at the calculated moment of capturing the target HH does not exceed the height of the lower boundary of the cloud and the height of the trajectory of the flight of the shell exceeds the altitude of the terrain on the entire trajectory of the missile's flight. If these conditions are not met, firing settings are selected from the memory of the commander's console with the height of the trajectory of the missile above the relief height, and a warning on reducing the probability of falling of the projectile due to low clouds ...

Firing method with guided missiles with laser semi-active self-guidance head

FIELD: weapons and ammunition. SUBSTANCE: invention relates to the field of weapons, in particular to the artillery guided projectiles with the laser semi-active homing head capturing the illuminated target on the trajectory final section. Method of firing projectiles with laser semi-active homing head from battery guns involves topographical linkage of target designator, target and weapons of firing position to area, detection of target, measurement of target polar coordinates by target designator and their transfer to scout panel of appropriate target indicator, calculation of firing settings on coordinates of target and weapon and their implementation, establishment of single computer time in scout panels and in gun control panels, and firing. After the shot is fired, the time for switching on the laser radiation of the target designator through a digital radio link is transmitted to the reconnaissance station, and the projectile is aimed at the target, which is illuminated with laser radiation of the target designator by the signal from the reconnaissance panel. At that, the target designation topography is carried out with the coordinate updating frequency of up to 100 Hz, the targets coordinates transfer is performed from each scout panel by digital radio communication to the commander's panel, arbitrarily located on the area between the observation post and the firing position, transmission of coordinates of weapons is carried out from each control panel of the weapon by digital radio communication to the commander's console, in the commander's console a computer time is set, which is the same as the time of the scout consoles and the gun control panels, command for production of shot is issued by commander's console, transmission of time for switching on of laser radiation of target designator is carried out via digital radio communication from control panel of firing gun to commander's panel, and then from commander's panel to ...

Apparatus for inspecting sensor

A sensor inspection device according to an embodiment comprises: a base including a plurality of supports and a horizontal block to which the plurality of supports are fixed; a rotating shaft that rotates while being supported by the plurality of supports; an encoder fixed to a horizontal block and measuring a rotation angle of the rotating shaft; an upper limit physically indicating the rotation angle of the rotating shaft; and a holder connected to the rotating shaft, rotating integrally with the rotating shaft, and holding the sensor and the upper limit. An objective of an embodiment is to provide the sensor inspection device capable of checking the accuracy of a sensor by checking an error between the sensor and the upper limit.

Firing control system and operation method of the same

The present invention relates to a firing control system and an operation method thereof. According to an embodiment of the present invention, the firing control system comprises: an indirect firing apparatus for discharging a bullet toward a target based on firing information; a trajectory measuring apparatus which measures a trajectory of the bullet discharged by the indirect firing apparatus, and generates trajectory data; a weather condition measuring apparatus which measures the weather condition at the time when the bullet is discharged by the indirect firing apparatus, and generates weather data; an impact measuring apparatus which measures an impact point of the bullet discharged by the indirect firing apparatus, and generates impact data; and a firing control apparatus which generates the firing information including a fire angle and a firing direction based on the trajectory data, the weather data, and the impact data, and transmits the firing information to the indirect firing apparatus. The present invention aims to provide a firing control system and an operation method thereof, which are able to improve the accuracy in calculating firing data.

Fire controlling system

FIELD: evaluation of periodic component of trajectory of target. SUBSTANCE: effective fast-setting circuit of evaluation is realized by way of evaluation of period and then amplitude of specified periodic component on basis of measurements closest in time. EFFECT: increased speed of response of system. 16 cl, 4 dwg па (19) 13) ВИ "2131 106 Сл 5 МК" [ 41 © 5/08, С 01 $ 13/72 РОССИЙСКОЕ АГЕНТСТВО ПО ПАТЕНТАМ И ТОВАРНЫМ ЗНАКАМ 12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ РОССИЙСКОЙ ФЕДЕРАЦИИ (21), (22) Заявка: 97113716109, 09.02.1996 (71) Заявитель: Холландсе Сигнаалаппаратен Б.В. (М) (30) Приоритет: 16.02.1995 МЕ 9500285 . (72) Изобретатель: Маас Абрахам Иоханнес (М) (46) Дата публикации: 27.05.1999 (73) Патентообладатель: (56) Ссылки: МО 94/09382 А, 28.04.94. ЕР 0347968 Холландсе Сигнаалаппаратен БВ. (МЕ) А, 27.12.89. \МО 8100149 АЛ, 22.01.91. \МО 88/02841 АЛ, 21.04.88. Ц$ 4665401 А, 12.05.87. ОЕ 2912587 СЛ, 07.05.86. $Ц 434349 А, 31.10.14. С1 (85) Дата перевода заявки РСТ на национальную фазу: 07.08.97 (86) Заявка РСТ: ЕР 96/00548 (09.02.96) (87) Публикация РСТ: М/О 96/25675 (22.08.96) (98) Адрес для переписки: 113556, Москва, ул.Болотниковская 1ОА, кв.101, патентному поверенному Моравскому А.В. 2131106 (54) СИСТЕМА УПРАВЛЕНИЯ ОГНЕМ (57) Реферат: 3 Данное изобретение относится к системам управления огнем и особенно к способам =“ \_, оценки периодического компонента траектории цели. Эффективная быстроустанавливающаяся схема оценки реализована путем оценки периода, а затем о амплитуды указанного периодического : 7 компонента на основе ближайших по времени Ч о измерений. Технический результат ь | 6 заключается в повышении быстродействия системы. 1 си 15 з.п.ф-лы, 4 ил. КО Фиг.1 зе рсС Го эорггсгс ПЫ Го (19) КУЗЗАМ АСЕМСУ ГОК РАТЕМТ$ АМО ТКАОЕМАКК$ 12) АВЗТКАСТ ОЕ 1МУЕМТОМ ВИ” 2131 106. (51) 1пЕ. С1.6 13) С1 Е 41С 5/08, С 01 $ 13/72 (21), (22) АррИсаНоп: 97113716109, 09.02.1996 (30) Рпогйу: 16.02.1995 МЕ 9500285 (46) Рае ог рибИсаНоп: 27.05.1999 (85) Соттепсетеп+{ о{ панопа! ...

The sighting device and method of motor driving

本发明涉及一种控制马达驱动的瞄准装置的方法，包括以下步骤：根据标称速度设定值与角速度传感器的测量值之间的差对马达进行控制；以及，在饱和的情况下，根据饱和之前的参考惯性位置与当前惯性位置之间的偏差来确定标称速度设定值的校正值，并将该校正值施加至标称速度设定值。本发明还涉及一种用于实施所述方法的瞄准装置。

Method and system for destroying rockets

A system that includes a synchronized network of three search and track radars and associated processing means and communication channels. The radars are configured to detect and track the target. In response to detected target, an interceptor is launched towards the target. The radars are configured to measure and track the target and the interceptor. The target and interceptor ranges are accurately measured by the radars in the synchronized network, giving rise to synchronized accurate range measurements that are combined by range triangulation to provide accurate target and interceptor position measurements irrespective of the angular measurement accuracy of each radar. The processing means are configured to utilize the measurements to calculate interceptor maneuvers required to overcome errors and bring the interceptor close to a target. The maneuver commands are transmitted to the interceptor using the communication channel. The interceptor is equipped with kill mechanism designed to destroy a target warhead when the interceptor approaches the target.

Method and system for destroying rockets

A system that includes a synchronized network of three search and track radars and associated processing means and communication channels. The radars are configured to detect and track the target. In response to detected target, an interceptor is launched towards the target. The radars are configured to measure and track the target and the interceptor. The target and interceptor ranges are accurately measured by the radars in the synchronized network, giving rise to synchronized accurate range measurements that are combined by range triangulation to provide accurate target and interceptor position measurements irrespective of the angular measurement accuracy of each radar. The processing means are configured to utilize the measurements to calculate interceptor maneuvers required to overcome errors and bring the interceptor close to a target. The maneuver commands are transmitted to the interceptor using the communication channel. The interceptor is equipped with kill mechanism designed to destroy a target warhead when the interceptor approaches the target.

ELDGIVNINGSANORDNING

Mock bullet lounching apparatus

PURPOSE: A shooting device for dummy ammunition is provided to analyze performance of devices like radar, infrared exploration devices, and a CCD(Charge-Coupled Device). CONSTITUTION: A shooting device(200) for dummy ammunition comprises a foci, a first chamber, a second chamber, a first diaphragm, and a second diaphragm. The first diaphragm bursts by a pressure difference between the first chamber and the second chamber, when a valve is opened and a second gas is compressed inside the second chamber while gas inside the foci, the first chamber, and the second chamber are in equilibrium. The second diaphragm bursts by a pressure difference inside the foci and the second chamber when inserting a first gas into the second chamber after the first diaphragm bursts.

Patent FR2439974B1

Fire control calculation control system and method based on dynamic scale

本发明提供了一种基于动态标尺的火控解算控制系统及方法，所述火控解算控制系统包括显示装置、信息采集装置、信息处理装置和操控装置，本发明把距离信息仅作为中间变量，使操作人员不必考虑距离设定而能精确进行火控解算，打击目标，是一种方便快捷、成本低、方式隐蔽的火控解算方式。

OPTICAL SYSTEM AND METHOD FOR LASER POINTING ACROSS THE ATMOSPHERE

Methods and apparatus for selecting a target from radar tracking data

根据本发明的各个方面的从雷达数据选择目标的方法和装置，与实时数据源和对抗措施系统联合操作。实时数据源为至少一个潜在目标提供跟踪信息，对抗措施系统可从所述至少一个潜在目标中选择符合预定阈值要求的与一个目标关联的导引轨迹以交战。

Aiming system for gun firing at moving targets - computes firearm azimuth and elevation rotations separately

The pivoted firearm on a base is moved so that it is compensated for interception, factors for target speed, average projectile speed and vector angles between target and projectile velocity. The overall correction is resolved into correction for rotation about a vertical axis and correction for elevation. Successive corrections are computed separately for these two rotations. The increments of the components of the overall correction are computed separately in relation to the increase of the component of the two successive rotating movements. Both increments evaluated in this manner are used separately for the azimuthal and elevation correction of the firearm. The input factors for the computer reproduce the increments as electrical analogue magnitudes which are fed into two electric motors for producing the two separate rotations of the firearm.

MOTORIZED METHOD AND DEVICE FOR SCORING

System for point of impact and method performing the same

본 발명에 따른 탄착점 확인 시스템은 포탄 발사 장치, 상기 포탄 발사 장치에 의해 목표물을 향해 발사되며, 상기 목표물을 향해 이동하는 과정에서 탄착점을 촬영하여 탄착점 이미지를 생성하는 이미지 촬영 모듈 및 특정 위치에서 상기 탄착점 이미지를 제공하는 무선 송신 모듈을 포함하는 포탄 및 상기 포탄으로부터 수신된 탄착점 이미지를 이용하여 상기 목표물까지의 오차 정보를 생성하고, 상기 오차 정보를 이용하여 상기 포탄 발사 장치를 제어하는 포탄 발사 장치 제어부를 포함한다. 따라서, 본 발명은 포탄이 목표물을 향해 이동하는 과정에서 촬영한 탄착점 이미지를 이용하여 목표물까지의 오차 정보를 생성하고, 오차 정보를 이용하여 포탄 발사 장치를 제어함으로써, 다음 포탄의 탄착점을 보상할 수 있다는 효과가 있다.

Patent FR2378318B1

SHOOTING DEVICE FOR ANTI-AIR DEFENSE SYSTEM, ESPECIALLY MOBILE

Ce dispositif comporte une sellette (10) pivotant autour d'un axe vertical (11) , un dispositif (12, 13) de tir de missiles téléguidés pivotant autour d'un axe horizontal (14) , un capteur de poursuite de cible (25) accouplé rigidement au dispositif de tir et déterminant des données concernant la cible, un calculateur d'angles de pointage (42) calculant le point de rencontre estimé du missile et de la cible et les angles " de correction de pointage en gisement " et " de correction de pointage en site " , un calculateur de poursuite (41) qui, à partir des écarts de la position de la cible vis-à-vis de la ligne de visée du capteur de poursuite de cible, produit des signaux de poursuite en gisement et en site, et une unité de commande (46) qui, en fonction des signaux de poursuite, provoque un pivotement de la sellette en gisement et un pivotement du dispositif de tir en site et, avant le déclenchement du tir, applique la correction de pointage en gisement à la sellette et la correction de pointage en site au dispositif de tir.Suivant l'invention, la ligne de visée du capteur de poursuite de cible est envoyée sur un miroir pivotant (29) à pivotement vertical et à pivotement horizontal et un dispositif d'entraînement de miroir (331, 332) est commandé par l'unité de commande d'une façon telle que le miroir pivotant est déplacé, dans des sens opposés aux sens de déplacement de la sellette et du dispositif de tir, d'un angle d'azimut (a) et d'un angle de hausse (E) correspondant respectivement à la correction de pointage en gisement et à la correction de pointage en site. This device comprises a harness (10) pivoting around a vertical axis (11), a device (12, 13) for firing unmanned missiles pivoting around a horizontal axis (14), a target tracking sensor (25 ) rigidly coupled to the firing device and determining data relating to the target, a aiming angle calculator (42) calculating the estimated meeting point of the ...

Method and device for predicting the state of a moving target

Les modes de réalisation de l’invention fournissent un procédé de prédiction de l’état d’une cible mobile (101) mis en œuvre dans un système de surveillance (100) comprenant un viseur optronique (104) et un dispositif de tir de projectiles (105) configuré pour tirer un ou plusieurs projectiles selon une séquence de tir donnée. Le procédé de prédiction comprend les étapes consistant à : - recevoir une pluralité de mesures brutes ; - sélectionner parmi les mesures brutes une ou plusieurs mesures brutes valides en fonction de la séquence de tir et en fonction d’un ou de plusieurs paramètres d’erreur ; - estimer à partir des mesures valides et à partir de la séquence de tir une cinématique courante de la cible mobile (101) et un modèle dynamique de mouvement vraisemblable ; - déterminer un point de rendez-vous spatio-temporel ; - calculer une pluralité de paramètres de tir permettant d’intercepter la cible mobile (101). Figure pour l’abrégé : Fig. 1A Embodiments of the invention provide a method for predicting the state of a moving target (101) implemented in a surveillance system (100) comprising an optronic sight (104) and a projectile firing device (105) configured to fire one or more projectiles according to a given firing sequence. The prediction method comprises the steps of: - receiving a plurality of raw measurements; - select from the raw measurements one or more valid raw measurements according to the firing sequence and according to one or more error parameters; - estimating from the valid measurements and from the firing sequence a current kinematics of the moving target (101) and a probable dynamic movement model; - determine a space-time rendezvous point; - calculating a plurality of firing parameters making it possible to intercept the moving target (101). Figure for the abstract: Fig. 1A

Device for tracking an object advancing on a path

MODULAR WEAPON STATION SYSTEM

Une station d'armes modulaire (10) comprend un bâti rotatif (24) adapté de façon à être monté sur une plateforme, et comporte un berceau amovible avec une arme (21) montée sur celui-ci. Le bâti rotatif (24) peut également comprendre une goulotte de chargement de munitions amovible (20), une unité de visée optique, et des entraînements d'azimut et d'élévation. La station d'armes modulaire (10) peut également comprendre un tambour rotatif et un ensemble de chargement de munitions couplés à l'ensemble de bâti rotatif (24). Le tambour rotatif et l'ensemble de chargement de munitions peuvent être disposés dans une position sous le blindage, de telle sorte qu'un opérateur puisse effectuer un ravitaillement en munitions à partir d'une position sous le blindage sans être exposé à un tir hostile. Des cartouches de munitions en bande peuvent se déplacer le long d'un trajet de chargement de munitions allant de l'ensemble de chargement à l'intérieur du tambour rotatif à une arme (21) sélectionnée. A modular weapon station (10) includes a rotatable frame (24) adapted to be mounted on a platform, and includes a removable cradle with a weapon (21) mounted thereon. The rotatable frame (24) may also include a removable ammunition loading chute (20), an optical sighting unit, and azimuth and elevation drives. The modular weapon station (10) may also include a rotating drum and an ammunition loading assembly coupled to the rotatable frame assembly (24). The rotating drum and the ammunition loading assembly can be disposed in a position under the shield so that an operator can perform ammunition refueling from a position under the armor without being exposed to hostile fire. . Cartridge ammunition cartridges may move along an ammunition loading path from the loading assembly within the rotating drum to a selected weapon (21).

MODULAR WEAPON STATION SYSTEM

Une station d'armes modulaire (10) comprend un bâti rotatif (24) adapté de façon à être monté sur une plateforme, et comporte un berceau amovible avec une arme (21) montée sur celui-ci. Le bâti rotatif (24) peut également comprendre une goulotte de chargement de munitions amovible (20), une unité de visée optique, et des entraînements d'azimut et d'élévation. La station d'armes modulaire (10) peut également comprendre un tambour rotatif et un ensemble de chargement de munitions couplés à l'ensemble de bâti rotatif (24). Le tambour rotatif et l'ensemble de chargement de munitions peuvent être disposés dans une position sous le blindage, de telle sorte qu'un opérateur puisse effectuer un ravitaillement en munitions à partir d'une position sous le blindage sans être exposé à un tir hostile. Des cartouches de munitions en bande peuvent se déplacer le long d'un trajet de chargement de munitions allant de l'ensemble de chargement à l'intérieur du tambour rotatif à une arme (21) sélectionnée. A modular weapon station (10) includes a rotatable frame (24) adapted to be mounted on a platform, and includes a removable cradle with a weapon (21) mounted thereon. The rotating frame (24) may also include a removable ammunition loading chute (20), an optical sight unit, and azimuth and elevation drives. The modular weapon station (10) may also include a rotating drum and ammunition loading assembly coupled to the rotating frame assembly (24). The rotating drum and ammunition loading assembly can be disposed in an underarmor position, such that an operator can refuel ammunition from an underarmor position without being exposed to hostile fire . Banded ammunition cartridges can move along an ammunition loading path from the loading assembly inside the rotating drum to a selected weapon (21).

Patent FR2125701A6

FIREARMS POINTING DEVICE

Appareil de pointage d'une arme à feu sur une cible en mouvement Il comprend un viseur monté sur l'arme, pour observer la cible, et au moins un système permettant à un opérateur de pointer l'arme sur la cible Ce système comprend des dispositifs qui, au moment du tir, agissent sur un commutateur de ce système, de façon à maintenir constantes pendant la durée du tir la position angulaire de l'arme ou une ou plusieurs de ses dérivées. Application : pointage de canons anti-aériens sur des cibles (avions) se déplaçant rapidement Apparatus for aiming a firearm at a moving target It comprises a sight mounted on the weapon, to observe the target, and at least one system allowing an operator to point the weapon at the target This system includes devices which, at the time of firing, act on a switch of this system, so as to maintain constant during firing the angular position of the weapon or one or more of its derivatives. Application: aiming anti-aircraft guns at rapidly moving targets (planes)

METHOD OF DETERMINING THE TRACK OF A BALLISTIC MISSILE

L'invention se situe dans le domaine de la détection et de la trajectographie de missiles balistiques. Elle concerne un procédé de détermination de la trajectoire d'un missile balistique à l'aide de mesures d'angles de site et d'azimut. Le procédé comprend : - une étape (103, 104) de détermination, à différents instants où le missile balistique est en phase exoatmosphérique non propulsée, d'un angle d'azimut et d'un angle de site du missile balistique, - une étape (105) de détermination des positions en trois dimensions du missile balistique auxdits instants à partir des différents couples d'angles et d'un modèle cinématique de trajectoire balistique non freinée. The invention lies in the field of the detection and tracking of ballistic missiles. It relates to a method for determining the trajectory of a ballistic missile using angle of elevation and azimuth measurements. The method comprises: - a step (103, 104) of determining, at different times when the ballistic missile is in the unpulsed exoatmospheric phase, an azimuth angle and a ballistic missile site angle, - a step (105) determining the three-dimensional positions of the ballistic missile at said instants from the different pairs of angles and a kinematic model of unbraked ballistic trajectory.

SHOOTING CONTROL DEVICE

L'invention concerne la commande automatique du pointage d'une arme. Le dispositif de l'invention comporte essentiellement un pupitre 11 qui permet de commander manuellement le pointage du fût 1 d'un canon, et un dispositif de calcul 5 qui élabore un modèle mathématique de la trajectoire de la cible, à partir des informations fournies par les capteurs 3 et 4. Le dispositif de calcul 5 relaie progressivement l'opérateur dans la poursuite de la cible en mouvement, ce qui va améliorer la precision de la poursuite. Application à la commande automatique du tir d'un canon. The invention relates to the automatic control of the aiming of a weapon. The device of the invention essentially comprises a console 11 which makes it possible to manually control the aiming of the barrel 1 of a gun, and a calculating device 5 which develops a mathematical model of the trajectory of the target, from the information supplied by the sensors 3 and 4. The calculation device 5 gradually relays the operator in the pursuit of the moving target, which will improve the precision of the tracking. Application to the automatic control of the firing of a cannon.

Pointing device

Apparatus for measuring the linear speed and orientation of an aerial target in relation to any direction

Target tracking system - firing or triggering signal is function of parameters of moving object

Guided missile firing method

Изобретение относится к области управления и регулирования, а более конкретно - к управляемому вооружению. Задачей предлагаемого изобретения является реализация дистанционной проверки готовности ракетного комплекса к пуску и формирование разрешения на пуск за счет оценки реализуемости зон стрельбы и зоны подсвета цели, а также отсутствия рассогласования углов наведения пусковой установки от рассчитанных установок стрельбы наведения пусковой установки. Указанная задача выполняется за счет того, что осуществляется топографическая привязка целеуказателя и пусковой установки к местности, обнаружение цели целеуказателем, измерение целеуказателем координат цели и передача их в пульт управления огневой позиции, вывод оператору сигнала запрета стрельбы на пульте управления, в пульте управления проверка соответствия дальности до цели с позиции пусковой установки допустимому диапазону дальностей стрельбы, расчет установок стрельбы управляемой ракеты и пусковой установки, в пульте управления проверка соответствия того, что углы наведения пусковой установки находятся вне диапазона углов запрета стрельбы комплекса, передача установок стрельбы по пусковой установке и ракете в блок автоматики пусковой установки и далее в ракету, наведение пусковой установки, контроль в пульте управления готовности ракеты к пуску, формирование разрешения на пуск при готовности ракеты и при отсутствии рассогласования наведения пусковой установки и установок стрельбы пусковой установки с предельно допустимыми отклонениями по углу азимута ±Δβ и углу места ±Δε, абсолютные величины которых принадлежат диапазону величин от 0,1° до 5°, подача с пульта управления огневой позиции в блок автоматики пусковой установки команды на пуск и производство пуска. Кроме того, при формировании разрешения на пуск управляемой ракетой с лазерной полуактивной головкой самонаведения до расчета установок стрельбы выполняют проверку соответствия дальности от целеуказателя до цели допустимому диапазону дальности подсвета, и ...

Semi-automatic tele-altimeter

Remote weapon system and controlling method of the same

본 발명의 실시 예들이 해결하고자 하는 기술적 과제는 사격 정확도를 향상시킬 수 있는 원격 무장 시스템 및 그 제어방법을 제공하는 것으로, 발사 신호에 기초하여 탄환을 발사하는 화기와, 화기의 상하방향의 조준 방향을 검출하는 각도 센서와, 화기의 조준 방향이 이전 사격의 조준 방향인 제1 방향으로부터 미리 설정된 범위인 기준 범위 이내일 때, 외부로부터 인가된 사격 명령 신호에 기초하여 화기의 사격을 제어하는 제어부를 포함하는, 원격 무장 시스템을 제공하여 사격 정확도를 향상시킨다.

Anti-aircraft defense vehicle

ASSISTED MANUAL DESIGNATION SYSTEM FOR A RADAR, OPTICAL OR OPTRONIC DEVICE

SYSTEME DE DESIGNATION MANUEL DE TYPE ACTIF COMBINANT LA STABILITE INERTIELLE DES SYSTEMES BOUCLES EN VITESSE A L'UTILISATION DES MOUVEMENTS REFLEXES DU SERVANT POUR LA COMMANDE. COMPORTE UN MANCHE DE COMMANDE 12 FIXE A UN SUPPORT 15 DU VISEUR 16, PARALLELE A LA LIGNE DE VISEE ET DONT LES SIGNAUX DE SORTIE SONT LES CONSIGNES DES BOUCLES DE REGULATION DES VITESSES DE ROTATION AUTOUR DES AXES AZIMUT ET ELEVATION. LE SERVANT TIENT LE MANCHE 12 DANS SA MAIN DROITE, PLACE SON OEIL DROIT SUR LA LIGNE DE VISEE ET SE MAINTIENT CONTRE LA TOURELLE 11 AU MOYEN D'UNE POIGNEE 13 SUR LAQUELLE SE TROUVE LE BOUTON DE BIEN-POINTE. APPLICATION AUX DISPOSITIFS DE POURSUITE AUTOMATIQUE D'UNE CIBLE AERIENNE.

Device for shooting against aerial targets

SHOOTING DEVICE FOR ANTI-AIR DEFENSE SYSTEM, ESPECIALLY MOBILE

Directing device for the search for airplanes in flight

Patent FR2286361B3

Arrangement and method for balancing a gun barrel of a vehicle mounted weapon system

The present invention relates to an arrangement (A) for balancing a gun barrel (20) of a vehicle mounted weapon system (C). The weapon system comprises the gun barrel (20) mounted to a turret (10) via a weapon cradle (30). The weapon cradle (30) is arranged to allow elevation movement of the gun barrel (20) about an elevation axis (Z1). Said arrangement (A) comprises a suspension system (S) configured to provide a torque opposing imbalance of the gun barrel (20). The arrangement further comprises an adjustment device (50; 150) for automatically adjusting the torque provided by the suspension system (S) based on imbalance of the gun barrel (20) so as to dynamically counteract imbalance of the gun barrel (20).The invention also relates to a vehicle with an arrangement according to the present invention.

Apparatus for determining the position of an objective in the air and its speed and for regulating the firing of firearms and the bursting of their projectiles

Electrical calculating device