СПОСОБ И УСТРОЙСТВО ДЛЯ ПРЕСЛЕДОВАНИЯ ДВИЖУЩЕЙСЯ ЦЕЛИ

... 1. Способ преследования подвижной цели, прежде всего транспортного средства (1), с шагами:а) идентификация цели,б) маркирование цели невидимой в видимом спектре, но световозвращающей в выбранном диапазоне длин волн невидимого светового спектра маркировкой (10),в) преследование промаркированной подвижной цели посредством предусмотренного на подвижной платформе регистрирующего изображение устройства (40), которое является чувствительным в выбранном диапазоне длин волн невидимого спектра.2. Способ по п.1, отличающийся тем, что выбранный диапазон длин волн находится в инфракрасном спектре.3. Способ по п.1 или 2, отличающийся тем,- что маркировка (10) образована невидимой, но световозвращающей в выбранном диапазоне длин волн маркировочной краской, которая содержит лак и внедренные в него световозвращающие частицы, причем частицы в выбранном диапазоне длин волн невидимого светового спектра имеют достаточный для световозвращения коэффициент преломления, и- что лак и внедренные в него частицы являются ...

Vorrichtung zur Justierung eines Lasersendungskanals mit einem passiven Beobachtungskanal

Persistant marking of a target

The present invention relates to a method of marking and identifying a target 110, and in particular, a method of using a Directed Energy Weapon (DEW), for example a laser beam 200, to heat a target without damaging it so that the target may be clearly identified by detectors and systems using thermally sensitive imaging. The temperature of the target may be increased with an identifiable pattern on the target surface (fig.4). Targets may be identified and distinguished from each other by thermal imaging equipment after the thermal designator has been disengaged. While the heat signature will decay over time, there will remain a window of opportunity after the thermal designator has been disengaged whereby the target can still be identified. A designated target may then be re-engaged (possibly in a new position amongst other targets, fig.3) after an interruption of the line of sight to the target.

Guidance head and method

Method and device for suppressing electromagnetic background radiation in an image

Method and defence system for combating threats

It is proposed to make a threat (2) better visible for a defensive measure (3). In this context, the threat (2) should be imaged more intensely for the defensive measure (3). For the purposes of more effective imaging, provision is made for the threat (2) to emit a stronger IR signature and thus be able to stand out sufficiently against the background for the defensive measure (3). The stronger IR signature is caused by heating a surface (9) of the threat (2), which is realized by a laser weapons system (7). The defensive measure (3) can better detect this heating and has an IR seeker head to this end.

METHOD AND DEVICE FOR SUPPRESSING ELECTROMAGNETIC BACKGROUND RADIATION IN AN IMAGE

The invention relates to a method and a corresponding device with which images (A, B) for the same sensing range, however in different wavelength ranges (P, N1, N2), are recorded at the same time or about the same time, and with which a signal to be detected is recorded for an image (A) serving as a P-image, and the wavelength of the signal is suppressed for an image (B) serving as an N-image. The intensity of the background in the P-image (A) is deduced from the N-image (B) while using a model for the interfering radiation or background radiation (2). The position of the signal to be detected is determined by comparing the image contents of the P-image (A) and the background image (C) derived from the N-image (B).

TARGET-TRACKING LASER DESIGNATOR

The present invention provides a laser tracking system including a laser generator for generating a beam of laser energy, a beam steerer for steering the beam of laser energy such that it moves in a search pattern, and a receiving device that receives laser energy reflected from a targeted object and that causes the beam steerer to vary the search pattern in response to the reflected laser energy. A tracking method associated with the laser tracking system includes the steps of generating a beam of laser energy, steering the beam of laser energy in a search pattern, detecting a hit spot formed from laser energy being reflected from a targeted object, diminishing the size of the search pattern in response to the detection of the hit spot, and focusing the diminished search pattern on a feature of the targeted object corresponding to the hit spot. The laser tracking system and associated method presented provide a number of advantages over conventional tracking systems. The laser tracking ...

Système de guidage de missiles, dans lequel une cible est détectée par un avion sans pilote qui éclaire la cible avec un rayon de lumière cohérente. Une station de contrôle éloignée commande l'avion sans pilote par radio et reçoit de cet avion les informations concernant la cible. Un lanceur de missiles, commandé par la station de contrôle envoie un missile selon une trajectoire dirigée vers la cible et le missile porte un système de guidage sensible à la lumière cohérente frappant la cible.

ILLUMINATEUR LASER UTILISABLE COMME BALISE, NOTAMMENT POUR UN SYSTEME D'APPUI AERIEN RAPPROCHE

ILLUMINATEUR PERMETTANT DE CONSTITUER UNE BALISE LASER DE GRANDE PORTEE ET SANS DANGER POUR LA VUE. IL CONSISTE A INTRODUIRE SUR LE TRAJET D'EMISSION D'UN LASER CONVENTIONNEL 1 UNE OPTIQUE DIVERGENTE 2 QUI PERMET DE PRODUIRE UN FAISCEAU LARGE ET CE FAISANT, PERMETTRE D'EXERCER UNE COUVERTURE DETERMINEE EN GISEMENT AG ET EN SITE AS. UN DISPOSITIF DE COMMANDE 3 PEUT ETRE PREVU POUR SUPPRIMER, PAR ESCAMOTAGE PAR EXEMPLE, LA FONCTION DIVERGENTE DE L'OPTIQUE 2 ET PRODUIRE LE MODE D'EMISSION DIRECTIF CONVENTIONNEL. L'INVENTION PEUT S'APPLIQUER DANS UN SYSTEME D'APPUI AERIEN RAPPROCHE AINSI QUE POUR SIMULER UNE CIBLE ILLUMINEE.

동축형 레이저무기의 조준 시스템

... 주반사경과 부반사경을 가지는 반사망원경, 반사망원경에 결합되어 타겟을 지향하도록 광축의 각변위를 담당하는 구동장치, 레이저광을 부반사경에 조사할 수 있는 고출력 레이저 발생기, 외부에서 수집된 광신호 혹은 영상신호를 받는 광센서, 광센서로부터의 신호를 받아 타겟의 위치를 확인하고 반사망원경이 타겟을 정확하고 지속적으로 지향할 수 있도록 구동장치에 구동 신호를 주는 콘트롤러를 구비하며, 반사망원경의 부반사경은 홀을 구비하여 부반사경에 조사되는 레이저광 일부가 홀을 통해 외부로 방출되어 조준용 레이저의 역할을 할 수 있도록 이루어지는 것을 특징으로 하는 동축형 레이저무기 조준 시스템이 개시된다.

Laser designator pulse detection

A laser designator pulse detector includes an InGaAs photodetector configured to convert laser signals into electrical signals. A Read Out Integrated Circuit (ROIC) is operatively connected to the InGaAs photodetector to condition electrical signals from the InGaAs photodetector. The ROIC can be operatively connected to a peripheral device including one or more modules configured to process signals from the ROIC and provide pulse detection, decoding, and tracking. In another aspect, a laser designator pulse detector includes a two-dimensional array of photodetectors configured to convert laser signals into electrical signals. A ROIC as described above is operatively connected to the two-dimensional array of photodetectors.

LOW POWER LASER SENSING

The presently disclosed subject matter includes a laser system and a respective method of detecting a signal reflected from a target illuminated by a modulated CW light source configured to generate a modulated laser signal at a predefined modulation frequency. A signal comprising true laser signal portions reflected from said target, and noise is received; the signal is filtered for selecting laser signal portions at a modulation frequency band; and the true signal portions in the signal are detected, if the energy at the modulation frequency band is greater than a given threshold.

Device and method of illuminating a target by the eye-motion of an operator

A contact lens adapted to fit over the eye of an operator can be employed to focus light impinging on the lens from a light source and reflected therefrom, substantially onto a predetermined region by an eye movement of the operator.

Target designation system

A system including a pulsed laser for illuminating targets. A detector has shutter synchronized by a radio link from the laser, so that the shutter allows the detector only to be energized when the laser pulses.

SYSTEM AND METHOD FOR PREDICTIVE COMPENSATION OF UPLINK LASER BEAM ATMOSPHERIC JITTER FOR HIGH ENERGY LASER WEAPON SYSTEMS

A system includes a target illumination laser (TIL) configured to illuminate an airborne target with a TIL beam. The system also includes a beacon illuminator (BIL) configured to transmit a spot of illumination to an expected location on the target, wherein the spot of illumination is more focused than the TIL beam. The system also includes a camera configured to receive an image of the spot reflected off the target. The system also includes a controller configured to determine an actual location of the spot on the target based on the received image. The controller is also configured to estimate a spot motion by correlating the actual location of the spot on the target with the expected location on the target. The controller is also configured to predict uplink jitter of a high energy laser (HEL) beam generated by a HEL based on the BIL spot motion, the uplink jitter caused by atmospheric optical turbulence. 1. A system comprising:a target illumination laser (TIL) configured to illuminate an airborne target with a TIL beam;a beacon illuminator (BIL) configured to transmit a spot of illumination to an expected location on the target, wherein the spot of illumination is more focused than the TIL beam;a camera configured to receive an image of the spot reflected off the target; and determine an actual location of the spot on the target based on the received image;', 'estimate a spot motion by correlating the actual location of the spot on the target with the expected location on the target; and', 'predict uplink jitter of a high energy laser (HEL) beam generated by a HEL based on the spot motion, the uplink jitter caused by atmospheric optical turbulence., 'a controller configured to2. The system of claim 1 , wherein the controller is further configured to control movement of at least one fast steering mirror (FSM) to substantially cancel the predicted uplink jitter of the HEL beam.3. The system of claim 2 , wherein the controller is configured to predict the uplink ...

Device Controlling Shooting Based on Firearm Movement

New systems, devices and methods for extremely precise aiming and shooting of firearms by relatively unskilled users are provided. In some embodiments, shots may be planned in advance. In some embodiments, a device including specialized computer hardware and software aids a user in planning a shot(s), evaluating the accuracy of the planned shot(s), adjusting the location of the planned shot(s), and executing the planned shots. In some embodiments, the system may prevent shots where motion, acceleration and positioning of the device and/or firearm relative to the planned shot location(s) and/or the surrounding environment may cause an inaccurate shot, but execute shots where those factors facilitate a highly accurate shot. In some embodiments, the control system may similarly account for, counteract and/or otherwise adjust for any other relevant ballistic and other accuracy-impacting factors with a position-actuable firing mechanism to maintain a projected flight path of such a point of ...

Schiesshilfevorrichtung ohne Visier

Covert marking apparatus

Covert marking apparatus suitable for marking, for example, a rendezvous point, comprising a source 1 of monochromatic unmodulated radiation with which an object is illuminated at an intensity which is too low to be noticed in light of ambient radiation. Viewing of the scene through a suitable optical filter 3 which blocks radiation of different wavelength from that selected causes the illuminated object to stand out from the rest of the scene.

Optical device able to change the direction of propagation of a light beam

An optical device is able to change the direction of propagation of a light beam, for example one formed by a collimator or beam expander, and may be of particular use in providing a larger range of directional adjustment when laser marking a target. The device comprises, in the direction of propagation z of the light beam 7, an overall divergent group of lenses 1 and an overall convergent group of lenses 2. The divergent group of lenses 1 itself contains, in the direction of propagation, a fixed lens 1.1, and an optical module comprising at least one movable optical element 1.2 able to change the direction of propagation of the light beam emerging from the divergent group of lenses 1. The optical module may further comprise a displacement unit 4 which displaces the moveable element 1.2 as a function of signals representing a set direction for propagation of light. The movable optical element 1.1 may correspond to a fixed diverging lens and the movable optical element 1.2 may comprise at ...

Sensor system and method

METHOD OF ATTACKING GROUND TARGETS

Means for automatically controlling a beam of electromagnetic radiation

Automatic beam-controlling means has an aiming device controlled, as a function of a reflected laser signal, so that a laser beam remains constantly directed at a target object 15, said aiming device comprising optically- pervious bodies, 2,3, which are variable in their diffraction behaviour, (preferably acousto-optical defectors), and, in addition to an electronic evaluation circuit 7 for registering the reflected laser signal, a control circuit 9, 10, 11, and a switching unit 8 connecting the aiming device to the control and evaluation circuits. The evaluation of the laser signal is effected preferably by phase- sensitive detectors. The apparatus is suitable for guiding steerable flying bodies. If initially the beam does not detect body 15, the beam is controlled, via a first component 9 of the control circuit so that it scans a predetermined region until it detects body 15. A second component 10,11 generates A.C. voltage signals for modulating the beam. ...

Helicopter location and attack systems

A device for the detection of and defense against low-flying helicopters which are masked or hidden by ground cover has a heat-sensitive sensor and an optical filter to detect heat radiation which is modulated at a frequency corresponding to the frequency of rotation of the helicopter blades. The helicopter motor and drive train provide a heat source, and the detector is positioned above the helicopter so that heat radiation reaching the detector from the helicopter is modulated by the rotating blades so that the detector can distinguish the helicopter heat source from other ground heat sources. The detector can be positioned by deployment from a tank and suspended above an area by a parachute, or may be contained in a remote piloted vehicle. The detector may relay a position signal to ground artillery for combat of the helicopter, or may be equipped with an explosive device which may be deployed after detection of a helicopter.

Processing images for target tracking

ACTIVE PARTIAL-BEAM ALIGNMENT SYSTEMS FOR SENSOR-TO-LASER BORESIGHT MAINTENANCE

An apparatus includes a reflector (206) having one or more reflective faces (302) and an opening (304). The reflector is selectively movable into and out of an optical path of an alignment beam (108). When the reflector is located within the optical path of the alignment beam, (i) the one or more reflective faces are configured to reflect a first portion of the alignment beam and (ii) the opening is configured to allow passage of a second portion of the alignment beam through the reflector. The reflector may include a retro-reflector, the retro-reflector may include multiple reflective faces, and the multiple reflective faces may be positioned around the opening.

OPTICAL SENSOR FOR RANGE FINDING AND WIND SENSING MEASUREMENTS

Techniques are disclosed for providing an optical sensor that can be used for wind sensing and an optical scope. The optical sensor can include a photodiode, an electrical switch, a trans-impedance amplifier (TIA), and a capacitive trans-impedance amplifier (CTIA), enabling the optical sensor to perform both wind-sensing and range-finding functions. Some embodiments may include some or all of these components in an application-specific integrated circuit (ASIC), depending on desired functionality.

DEVICE AND SYSTEM FOR REPRESENTING HITS BY SHOTS AND/OR ROCKETS AND METHOD FOR SAME

The present invention relates to a device (10) for representing hits by shots and/or rockets, a corresponding system for same and an associated method. Disclosed is a device (10) which is capable of flight and provides means (12) for optical and/or acoustic representation of hits. The device (10) and the means (12) can be remotely controlled and can be controlled from a control centre (30). For the purpose of control, the control centre (30) can locate objects capable of being located via positioning satellites (50) and control the device (10) according to the location.

PROCESS AND DEVICE TO CORRECT the POINTING Of an OPTICAL ILLUMINATOR ON an AIMED TARGET.

A METHOD FOR BEATING an OBJECTIVE BY MEANS OF PASSIVE PROJECTILES AND SYSTEM OF TIR FOR the EXECUTION OF THIS PROCESS

SYSTEME DE DESIGNATION D'OBJECTIF PAR LASER

SYSTEME PERMETTANT D'ALIGNER AVEC PRECISION L'AXE D'EMISSION LASER AVEC CELUI DU SENSEUR D'IMAGE VIDEO ABOUTISSANT AU CENTRE DE L'IMAGE BALAYEE. IL UTILISE UNE SOURCE LUMINEUSE PONCTUELLE 20 ET UNE OPTIQUE DE FOCALISATION 21 ASSOCIEE; LA RECEPTION EXTERIEURE PEUT ETRE INTERROMPUE PAR UN MIROIR DE RENVOI 22 ESCAMOTABLE. L'ECARTOMETRE 4 DU SYSTEME MESURE LES ECARTS SX, SY DE L'IMAGE DE LA SOURCE. LE SENSEUR 2 EST ENTRAINE EN ROTATION 13-14 POUR OCCUPER PLUSIEURS POSITIONS ANGULAIRES SUCCESSIVES PREDETERMINEES. UN ENSEMBLE ELECTRONIQUE 23 DE COMMANDE ET DE CALCUL DELIVRE, A PARTIR DES INFORMATIONS D'ECART SUCCESSIVES, LES SIGNAUX DE CORRECTION DX, DY DE BALAYAGE PERMETTANT D'ASSERVIR LE CENTRE DE L'IMAGE COINCIDANT AVEC LE POINT INVARIANT DE L'IMAGE CORRESPONDANT A L'AXE DE ROTATION.

Appareil d'asservissement en poursuite automatique d'un faisceau laser.

Appareil destiné à asservir automatiquement en poursuite un faisceau laser devant se réfléchir sur un objet-cible mobile, comportant un récepteur, un dispositif de pointage présentant deux unités déflectrices pouvant etre pilotées séparément, et un montage d'éxploitation électronique agissant sur le dispositif de pointage. Les unités déflectrices comprennent deux corps 2, 3 optiquement transparents faisant un angle l'un par rapport à l'autre, au moyen desquels on peut obtenir un faisceau laser dévié d'un certain angle par rapport à la direction de rayonnement initiale, dont la direction peut être modifiée en fonction du type de la grandeur du signal, il comporte en plus du montage d'exploitation électronique 7 un autre montage de commande comprenant au moins deux composants 9, 10, 11 agissant également sur le dispositif de pointage, ainsi qu'une unité de commutation 8 reliant les composants 9, 10, 11 du montage de commande et le montage d'exploitation électronique 7 au dispositif de pointage ...

BOAT REPAIR UNIT FOR

LIGHT IRRADIATION DEVICE AND LIGHT IRRADIATION SYSTEM

A light irradiation device includes: at least one imaging means that images a monitoring region to continue to accurately irradiate a moving target with light; at least one projection means that irradiates the monitoring region with signal light; a control means that controls the imaging means to image the monitoring region and controls the projection means to emit the signal light; at least one propeller that moves the own device in the air; and a flight control means that controls flight of the own device by controlling the propeller, the control means controlling, when recognizing a light irradiation target to be irradiated with the signal light on image data imaged by the imaging means, the projection means to emit the signal light toward the light irradiation target. 1. An irradiation system comprising: detect an irradiation target to be irradiated in a captured image; and', 'control a projector to emit a light in such a way that, if the irradiation target moves in a direction away from a monitoring region, the projector does not emit the light even if the irradiation target is detected, and to otherwise emit the light if the irradiation target is detected., 'at least one processor configured to2. The irradiation system according to claim 1 , wherein the projector is included in a flight device claim 1 , and while detecting the irradiation target which is moving, control a flight of the flight device to follow the irradiation target, and', 'control the projector to keep emitting the light., 'wherein at least one processor is further configured to3. The irradiation system according to claim 1 , wherein the at least one processor is configured to claim 1 , if a plurality of irradiation targets are detected moving toward a direction other than the direction away from the monitoring region claim 1 , control the projector to emit the light to the plurality of the irradiation targets.4. The irradiation system according to claim 1 , wherein the at least one processor ...

Portable integrated laser optical target tracker

A portable integrated laser optical target tracker and designator (PILOTT device) in a single housing is provided having a laser designator assembly to produce a focused laser beam that is projected from the housing. A laser energy detector is located in the housing that detects reflected laser energy from any designation source (ground or airborne based), provides steering information, decodes the laser's frequency, and is used as a range finding receiver. The location of the laser energy provides automatic field alignment of the laser designator. An optical magnification scope is mounted in the housing and has an optical field of view that is parallel to and aligned with a beam path defined by the laser beam focusing optics. Any night scope can be added to the system to provide night situational awareness by being shown in the display. A visual electronic display is overlaid with the optical field of view. A main controller communicates with the controller of the laser energy detector ...

Marker system

A marker system includes at least one emitter. The emitter(s) emit light responsive to a flow of electrical current there through. The marker system includes a device for acquiring an incoming signal and a circuit for processing the incoming signal. The circuit for processing the incoming signal monitors the device for acquiring the incoming signal to determine if the incoming signal includes any of a plurality of incoming Identification Friend or Foe (IFF) and/or munitions-targeting signals. The circuit emits one of a plurality of responses by sending electrical current selectively through the emitter(s) and/or other feedback devices based upon which of the plurality of incoming Identification Friend or Foe (IFF) and/or munitions-targeting signals is detected by the means for processing.

METHOD AND DEVICE FOR SUPPRESSING ELECTROMAGNETIC BACKGROUND RADIATION IN AN IMAGE

The invention relates to a method and a corresponding device with which images (A, B) for the same sensing range, however in different wavelength ranges (P, N1, N2), are recorded at the same time or about the same time, and with which a signal to be detected is recorded for an image (A) serving as a P-image, and the wavelength of the signal is suppressed for an image (B) serving as an N-image. The intensity of the background in the P-image (A) is deduced from the N-image (B) while using a model for the interfering radiation or background radiation (2). The position of the signal to be detected is determined by comparing the image contents of the P-image (A) and the background image (C) derived from the N-image (B).

Boresight alignment measuring apparatus and method for electro-optic systems

The apparatus comprises a main optic (40, 46) for receiving the second radiation from the electro-optic system and focusing the second radiation about a focal point in a focal plane substantially perpendicular to a principal radiation path (44). The apparatus comprises a first radiation source (52) for generating a target beam of the first radiation and for directing the target beam along said principal radiation path (44) sequentially to the secondary (48) and primary (42) reflectors, and to the sensor of the electro-optic system, the target beam causing the sensor to set the direction of the target vector in substantial correspondence with the target beam, and a detector responsive to the second radiation for detecting the location of the illumination beam relative to the location of the target vector.

Method of attacking ground targets

A method of attacking a ground target 1 uses a target marking projectile 10 which is fired from weapon 9 at close range and which impacts the target to produce high temperature radiation. Subsequently a missile 13 is launched and this homes onto the target radiation guided by a seeker head 14. The missile 13 does not require active guidance from the firing point after launch. ...

MISSILES INCLUDING LASERS SUITABLE FOR MISSILE AND/OR TARGET TRACKING AND FOR ILLUMINATION PURPOSES

Sensor system and method

PROCEDURE AND SYSTEM FOR THE DETERMINATION OF A GOAL AND FOR THE EXECUTION OF GOAL-REFERRED MEASURES

Viewfinder with mobile red dot and illuminator

The present invention relates to a viewfinder with a mobile red dot comprising a first stationary light source (30) and a first reflective strip (34, 53), the light source generating a first collimated light beam which is projected onto the reflective strip (34, 53) so as to materialise a red dot or grid visible for the shooter by the reflection on the reflective strip (34, 53), the first beam being projected onto the reflective strip (34, 53) by means of a rotary mirror (32) with adjustable angle of inclination relative to the first light beam.

METHOD FOR TARGET COMBATTING BY MEANS OF PASSIVE PROJECTILES AND A FIRING SYSTEM FOR CARRYING OUT THE METHOD

A method and a firing system for combatting a target by firing of explosive projectiles having homing devices or proximity fuses operating with reception of electromagnetic energy. In order to achieve an increased accuracy of aim with use of simple control circuits the homing devices and the proximity fuses, respectively are made passive, i.e. purely receiving, and with regular intervals in the burst of fire a transmitting projectile is fired, which illuminates the target with electromagnetic energy.

METHOD AND DEFENSE SYSTEM FOR COMBATING THREATS

It is proposed to make a threat (2) better visible for a defensive measure (3). In this context, the threat (2) should be imaged more intensely for the defensive measure (3). For the purposes of more effective imaging, provision is made for the threat (2) to emit a stronger IR signature and thus be able to stand out sufficiently against the background for the defensive measure (3). The stronger IR signature is caused by heating a surface (9) of the threat (2), which is realized by a laser weapons system (7). The defensive measure (3) can better detect this heating and has an IR seeker head to this end.

用于对图像中的电磁背景辐射进行抑制的方法和装置

... 通过一种方法和一种属于该方法的装置来同时或近似同时记录相同捕获范围、但在不同波长范围(P，N1，N2)内的图像(A，B)，该方法和该装置为用作P图像的图像(A)捕获要检测的信号，并为用作N图像的图像(B)抑制信号波长。在使用干扰辐射或背景辐射(2)用模型时，从N图像(B)推断出P图像(A)中的背景强度。通过把P图像(A)和从N图像(B)推导出的背景图像(C)的图像内容加以比较来确定要检测信号的位置。 ...

ASSEMBLY AND METHOD OF POSITIONING AND ALIGNING A DISRUPTER FOR THE DISMANTLING OF A TARGET

DEVICE COMBINES OBSERVATION AND Of EMISSION, AND PROCEEDED OF VISUALIZATION Of a DIRECTION Of EMISSION Of SUCH a DEVICE

REMOTE CONTROL DEVICE FOR A TARGET DESIGNATOR FROM AN ATTACK MODULE, ATTACK MODULE AND DESIGNATOR IMPLEMENTING SUCH A DEVICE

LASER ILLUMINATOR USABLE AS BEACON, IN PARTICULAR FOR a SYSTEM Of AIR SUPPORT BRINGS closer

METHOD AND DEVICE INTEND TO ELIMINATE FROM THE UNDERGROUND MINES

IMAGING INSTRUMENT FOR MONITORING A TARGET DESIGNATION

Unmanned aerial vehicle i.e. unmanned combat air vehicle, has guided munition firing device oriented towards rear side, where firing axis of device makes azimuth angle equal to 180 degree with respect to displacement direction of vehicle

The vehicle has a controllable optronic ball fixed under the vehicle, where the optronic ball is intended to attain a target (C). A firing device of a guided munition such as rocket and missile, is oriented towards a rear side, where firing axis of the firing device makes an azimuth angle equal to 180 degree, with respect to a displacement direction of the vehicle. A rear wheel and a nose wheel permit the landing of the vehicle. A target illumination unit of the optronic ball illuminates the target to guide the guided munition fired by the firing device towards the target. An independent claim is also included for a method for firing a munition guided towards a target from an unmanned aerial vehicle.

SYSTEME DE CONDUITE DE TIR A LUNETTE D'OBSERVATION ASSERVIE PAR UN DISPOSITIF DE POURSUITE AUTOMATIQUE

L'INVENTION CONCERNE UN SYSTEME DE CONDUITE DE TIR DESTINE A ETRE MONTE NOTAMMENT SUR UN HELICOPTERE. UN DISPOSITIF 20 DE POURSUITE AUTOMATIQUE DE CIBLE ET UNE LUNETTE GROSSISSANTE 10 D'OBSERVATION SONT ASSERVIS L'UN A L'AUTRE POUR QU'EN PHASE DE RECHERCHE LE DISPOSITIF DE POURSUITE SUIVE L'ORIENTATION DE LA LUNETTE ET QU'EN PHASE DE POURSUITE AUTOMATIQUE LA LUNETTE SUIVE LE DISPOSITIF DE POURSUITE. POUR LE RECALAGE DE L'ORIENTATION DE LA LUNETTE PAR RAPPORT AU DISPOSITIF DE POURSUITE, UN EMETTEUR LASER 56 PEUT EMETTRE UN FAISCEAU LASER DANS L'AXE DU DISPOSITIF DE POURSUITE; CE FAISCEAU LASER SE REFLECHIT SUR UN OBSTACLE OU UNE CIBLE ET EST RECU PAR UN DETECTEUR 54 PORTE PAR LA LUNETTE. UN CIRCUIT D'ECARTOMETRIE 52 FOURNIT DES SIGNAUX D'ERREUR REPRESENTANT LE DECALAGE DU FAISCEAU LASER RECU PAR RAPPORT AU CENTRE DU DETECTEUR 54. CES SIGNAUX D'ERREUR, ENREGISTRES DANS UNE MEMOIRE 42 EN PHASE DE RECALAGE, SONT RESTITUES ET PRIS EN COMPTE PAR UN CIRCUIT D'ASSERVISSEMENT 38, 40, 16 ENTRE LA ...

EMETTEUR LASER PORTABLE ET AUTONOME

LA PRESENTE INVENTION CONCERNE UN EMETTEUR LASER PORTABLE ET AUTONOME COMPRENANT UNE SOURCE EMETTRICE D'UN RAYON LASER, UN REDUCTEUR DE DIVERGENCE DE FAISCEAU, UNE VISEE OPTIQUE, ET UNE ALIMENTATION PORTABLE A COMMUTATIONS TEMPORAIRES. CE DISPOSITIF COMPORTE ESSENTIELLEMENT UN BATI INTERMEDIAIRE 2 DE FORME CYLINDRIQUE CONTENANT DANS UN LOGEMENT ALLONGE 15 UN EMETTEUR LASER 3, PROLONGE PAR UN REDUCTEUR DE DIVERGENCE DE FAISCEAU I. UNE VISEE OPTIQUE PAR LUNETTE 5 EST FIXEE SUR LE BATI 2 PAR UNE FIXATION REGLABLE 4. L'ENSEMBLE DE CES ELEMENTS EST FIXE MECANIQUEMENT SUR LA CROSSE 7. UNE ALIMENTATION PAR CABLAGE ELECTRIQUE 6.14 20 EST ASSUREE EN PROVENANCE D'UN SAC 9 COMPRENANT UN ACCUMULATEUR ELECTRIQUE 10, UNE ALIMENTATION ELECTRIQUE 11, UN AMPLIFICATEUR DE COURANT 12. LE CALAGE EST ASSURE PAR DE LA MOUSSE SYNTHETIQUE 16. UN INTERRUPTEUR 8 EST MONTE SUR LA CROSSE, LES FILS ETANT CONNECTES DE FACON DEMONTABLE PAR DES CONNEXIONS 13 23. APPLICATIONS AUX TELECOMMANDES, ILLUMINATIONS ET EBLOUISSEMENTS ...

TOGETHER OF OPTICAL AIMING, OF DESIGNATION AND CONTINUATION Of OBJECTIVE

L'ENSEMBLE COMPREND UN EMETTEUR LASER 100, UN LOCALISATEUR 200 POUR FOURNIR UNE INFORMATION ECARTOMETRIQUE ENTRE UNE CIBLE ET UN PROJECTILE, UN BLOC DE VISEE 300 PERMETTANT LA VISEE OPTIQUE DE LA CIBLE PAR UN OPERATEUR, ET DES MOYENS COLLIMATEURS 400 PERMETTANT LE CENTRAGE PAR CE DERNIER DU CHAMP DE VISEE SUR LA CIBLE. SELON L'INVENTION, IL EST PREVU DES MOYENS HARMONISATEURS 500, PAR EXEMPLE UN DIASPORAMETRE 501, 502 INTERPOSE ENTRE LES MOYENS COLLIMATEURS ET LE BLOC DE VISEE, POUR AJUSTER L'ORIENTATION ANGULAIRE DE LA DIRECTION DE COLLIMATION, DE MANIERE A FAIRE COINCIDER CELLE-CI O D AVEC LA DIRECTION DE REFERENCE A B OU DE VISEE A B, C D - C'EST-A-DIRE CELLE CORRESPONDANT A LA DIRECTION REELLE DE DESIGNATION ET DE VISEE DE LA CIBLE - ET AVEC LA DIRECTION DE LOCALISATION J K - C'EST-A-DIRE CELLE SOUS LAQUELLE LE LOCALISATEUR VOIT LA CIBLE DESIGNEE. THE SET INCLUDES A LASER EMITTER 100, A LOCATOR 200 TO PROVIDE ECARTOMETRIC INFORMATION BETWEEN A TARGET AND A PROJECTILE, A SIGHTING BLOCK 300 ALLOWING THE OPTICAL VIEWING OF THE TARGET BY AN OPERATOR, AND 400 COLLIMATORS ALLOWING CENTERING MEANS. LAST OF THE FIELD OF VIEW ON THE TARGET. ACCORDING TO THE INVENTION, HARMONIZING MEANS 500 ARE PROVIDED FOR, FOR EXAMPLE A DIASPORAMETER 501, 502 INTERPOSED BETWEEN THE COLLIMATORS AND THE AIMING BLOCK, TO ADJUST THE ANGULAR ORIENTATION OF THE COLLIMATION DIRECTION, SO AS TO MAKE IT COINCIDATE. CI OD WITH THE DIRECTORATE OF REFERENCE AB OR DIRECTORATE AB, CD - IT IS THAT CORRESPONDING TO THE ACTUAL DIRECTORATE OF DESIGNATION AND VIEW OF THE TARGET - AND WITH THE DIRECTORATE OF LOCATION JK - THIS IS A -DIRE THE ONE UNDER WHICH THE LOCATOR SEES THE DESIGNATED TARGET.

METHOD AND DEVICE AIMING AID FOR THE LASER GUIDANCE OF A PROJECTILE

La présente invention concerne un procédé et un dispositif d'aide à la visée d'une cible (5) destinée notamment à améliorer la précision du guidage par un faisceau laser (9) d'un projectile (10) vers ladite cible (5). Ce procédé utilise une caméra (2) permettant d'enregistrer une image complète de l'environnement ou bien une image sélective de ladite cible (5) dans ledit environnement. Ensuite, ce procédé permet de vérifier que ledit faisceau laser (9) pointe réellement ladite cible (5) en affichant le point de contact (91) dudit faisceau laser (9) dans ledit environnement sur l'image enregistrée par ladite caméra (2), puis de déterminer la précision avec laquelle ledit faisceau laser (9) pointe réellement ladite cible (5). En fonction de ladite précision, le lancement dudit projectile (10) peut être confirmé ou bien annulé. Ce procédé permet également d'identifier le code dudit faisceau de guidage (9) illuminant ladite cible (5).

DISPOSITIF POUR L'IDENTIFICATION A DISTANCE D'UN INSTRUMENT OPTIQUE D'OBSERVATION

DISPOSITIF DESTINE A ETRE ANNEXE A UN INSTRUMENT OPTIQUE DE RECHERCHE ET D'OBSERVATION. IL COMPREND DES MOYENS POUR EMETTRE UN FAISCEAU OPTIQUE DE REPONSE LORSQU'UN FAISCEAU D'ENTREE PENETRE DANS L'INSTRUMENT ET DANS LA MEME DIRECTION QUE LE FAISCEAU D'ENTREE. LE DISPOSITIF EST UTILISABLE NOTAMMENT, POUR LA RECHERCHE DE PORTEURS D'ARMES AU COURS D'OPERATIONS MILITAIRES.

ABSOLUTE TIME ENCODED SEMI-ACTIVE LASER DESIGNATION

SAL designation uses absolute time coding of the pulse-stream to disambiguate the designator in a manner that reduces the number of pulses in a pulse-stream and reduces the total pulse energy on the target. This requires timing synchronization between the designator and receiver. For improved rejection of unintended returns, more precise time gating (narrower absolute time window) is required. This can be achieved by removing the path length and or firing time uncertainty errors. Absolute time coding reduces the number of pulses and total energy on target in two ways. First, the designator may only have to transmit the pulse-code once. The "spot" appears for the brief time associated with a pulse-stream and disappears; continuous lasing of the target is not required. Second, the designator can be disambiguated using a combination of pulse-code (relative spacing of pulses) and pulse-position (absolute timing of pulses) modulation. This allows the pulse-stream to be shortened considerably ...

Image-aided illumination assembly and method

An illumination assembly includes a laser for producing a laser beam of light and an optical fiber disposed adjacent the laser and extending between a beam receiving end for receiving the laser beam of light from the laser and a beam emitting end for emitting the laser beam of light therefrom. A beam splitter splits the laser beam into a target beam and a feedback beam and directs the target beam toward the targeted object. A feedback sensor receives the feedback beam and generates a feedback signal to identify a targeted image portion correlated to the targeted object. A motor is operatively connected to the vehicle with the beam emitting end fixedly secured thereto. A controller receives the feedback signal generated by the feedback sensor and generates a control signal transmittable to the motor to position the beam emitting end of the optical fiber such that the target beam continues to be directed toward the targeted object.

VIEWFINDER WITH MOBILE RED DOT AND ILLUMINATOR

The present invention relates to a viewfinder with a mobile red dot comprising a first stationary light source (30) and a first reflective strip (34, 53), the light source generating a first collimated light beam which is projected onto the reflective strip (34, 53) so as to materialise a red dot or grid visible for the shooter by the reflection on the reflective strip (34, 53), the first beam being projected onto the reflective strip (34, 53) by means of a rotary mirror (32) with adjustable angle of inclination relative to the first light beam.

ENCODED SIGNAL DETECTION AND DISPLAY

A target marking system includes a light source emitting a thermal beam having a predetermined temporal modulation, and an optics assembly directing the thermal beam to impact a target, the target directing radiation to the optics assembly in response to the impact. A portion of the radiation having the predetermined temporal modulation. The target marking system further includes a detector configured to distinguish the portion of the radiation having the predetermined temporal modulation from a remainder of the radiation, the portion of the radiation passing to the director through the optics assembly. The system also includes a readout integrated circuit, the detector directing an input signal to the readout integrated circuit, and the readout integrated circuit producing a digitally enhanced output signal in response to receipt of the input signal. 114-. (canceled)15. A system , comprising:a housing;an optics assembly disposed at least partly within the housing, the optics assembly configured to receive thermal radiation directed to enter the housing; identify a characteristic of the thermal radiation received by the optics assembly; and', 'generate an output signal indicative of the characteristic; and, 'a detector configured to an object disposed external to the housing;', 'at least part of the thermal radiation extending from the object; and', 'visual indicia of the characteristic., 'a display operably connected to the detector, the display configured to display an image based at least partly on the output signal, the image illustrating16. The system of claim 15 , wherein the detector comprises an uncooled microbolometer array.17. The system of claim 15 , wherein the detector comprises an array of heat-sensitive pixels.18. The system of claim 15 , wherein the detector comprises a first array of pixels and the display comprises a second array of pixels corresponding to the first array of pixels.19. The system of claim 18 , further comprising a readout ...

RECOIL SPRING GUIDE MOUNTED TARGET MARKER

In an exemplary embodiment of the present disclosure, a target marker for a firearm may comprise a module having a first portion, and a second portion electrically connected and coupled to the first portion. A light source may be disposed within and electrically connected to the second portion. An optical component may be coupled to the first portion at a first fixed distance from the light source. A circuit board may be electrically connected to the light source via at least one lead, wherein the lead may permit relative movement between the circuit board and the light source and may maintain a second fixed distance between the circuit board and the light source.

METHOD AND EQUIPMENT FOR STATICALLY AND DYMICALLY TESTING ALIGNMENT OF LINE OF SIGHT IN INNER CAVITY OF ELECTROOPTIC SYSTEM

PURPOSE: To detect the position of a radiation beam with respect to the position of a target vector in response to a second radiation from an electrooptic system by arranging a main optic coupled optically with an system while being aligned with a main radiation path and converging the second radiation around a focal plane vertical to the second radiation. CONSTITUTION: The electrooptic system (E-O system) 10 is provided with a control section 14 connected with a test head 12, a remote display 16, a computer 18, a printer 20, etc. The test head 12 is mounted on a five axis flight simulation system 22 and an E-0 system 32 to be tested is mounted directly under the test head 12 around the plane 24 of a motion table 22 with the FLIR and laser designator of system 32 being arranged contiguous to an optical aperture 32'. A radiation is transferred through the aperture 32' and the FLIR detects infrared rays radiated from the test aperture 12 which is irradiated from the laser designator. COPYRIGHT ...

Drohnenverbund und Markierverfahren für eine markergelenkte Maßnahme

Bei einem Drohnenverbund (2), mit mindestens zwei Drohnen (4a,b), enthalten wenigstens zwei der Drohnen (4a,b) eine Zielmarkiervorrichtung (6) zur Markierung eines Zielobjekts (22a-c) mit einer Zielmarkierung (12, 12a-d) für eine markergelenkte Maßnahme, wobei mindestens zwei der Drohnen (4a,b) dazu eingerichtet sind, das selbe Zielobjekt (22a-c) mit ihrer Zielmarkierung (12,12a-d) zu markieren.Bei einem Verfahren zur Markierung eines Zielobjekts (22a-c) mit einer Zielmarkierung (12, 12a-d) für eine markergelenkte Maßnahme, markieren mindestens zwei Drohnen (4a-b) des Drohnenverbandes (2) das selbe Zielobjekt (22a-c) gleichzeitig und/oder abwechselnd mit der Zielmarkierung (12,12a-d).

Method and device for detecting and eliminating land mines

Detecting and eliminating land mines

For detecting and eliminating land mines, a site (40) is observed from an aircraft (10) by means of an image resolving sensor (26) on which an image of the site surface is generated. The sensor (26) responds to differences in the radiation and/or reflection of the land mine or the ground surface over the land mine with respect to the surroundings. The position of the land mine is determined from image data of the sensor (26). An aiming device (20), for example, a gun is aimed at the position of the land mine thus detected. Thereby, the land mine is caused to detonate. Alternatively, the aiming device (20) may be a marking device for marking the position of the land mine for a subsequent clearing of the mine on the ground.

Optical device able to change the direction of propagation of a light beam

An optical device is able to change the direction of propagation of a light beam, for example one formed by a collimator or beam expander, and may be of particular use in providing a larger range of directional adjustment when laser marking a target. The device comprises, in the direction of propagation z of the light beam 7, an overall divergent group of lenses 1 and an overall convergent group of lenses 2. The divergent group of lenses 1 itself contains, in the direction of propagation, a fixed lens 1.1, and an optical module comprising at least one movable optical element 1.2 able to change the direction of propagation of the light beam emerging from the divergent group of lenses 1. The optical module may further comprise a displacement unit 4 which displaces the moveable element 1.2 as a function of signals representing a set direction for propagation of light. The movable optical element 1.1 may correspond to a fixed diverging lens and the movable optical element 1.2 may comprise at ...

PROCEDURE AND DEVICE FOR THE SUPPRESSION OF ELECTROMAGNETIC BACKGROUND RADIATION IN A PICTURE

Riflescope with integrated wind sensor and targeting display

Techniques are disclosed for providing the weapon-mounted optical scope that provides for wind sensing and the display a ballistic solution without the need for a separate device. Embodiments may include various additional sensors housed within the weapon-mounted optical scope to provide data for the ballistic solution calculation. Embodiments may further include a display at the input aperture rather than internally at the first-focal-plane, enabling for simpler, more cost effective embodiments. Additionally or alternatively, embodiments may include a laser, separate from the wind sensing laser, to perform range-finding functions, and/or an enhanced-image assembly.

Method and defence system for combating threats

It is proposed to make a threat (2) better visible for a defensive measure (3). In this context, the threat (2) should be imaged more intensely for the defensive measure (3). For the purposes of more effective imaging, provision is made for the threat (2) to emit a stronger IR signature and thus be able to stand out sufficiently against the background for the defensive measure (3). The stronger IR signature is caused by heating a surface (9) of the threat (2), which is realized by a laser weapons system (7). The defensive measure (3) can better detect this heating and has an IR seeker head to this end.

METHOD AND DEFENSE SYSTEM FOR COMBATING THREATS

It is proposed to make a threat (2) better visible for a defensive measure (3). In this context, the threat (2) should be imaged more intensely for the defensive measure (3). For the purposes of more effective imaging, provision is made for the threat (2) to emit a stronger IR signature and thus be able to stand out sufficiently against the background for the defensive measure (3). The stronger IR signature is caused by heating a surface (9) of the threat (2), which is realized by a laser weapons system (7). The defensive measure (3) can better detect this heating and has an IR seeker head to this end.

METHOD FOR TARGET COMBATTING BY MEANS OF PASSIVE PROJECTILES AND A FIRING SYSTEM FOR CARRYING OUT THE METHOD

METHOD AND DEVICE FOR TRACKING A MOVING TARGET OBJECT

A method for tracking a moving target object, in particular a vehicle (1), with the steps a) Identification of the target object; b) Marking the target object with a marking (10) invisible in the visible spectrum but retro-reflective in a selected wavelength range of the invisible spectrum of light; c) Tracking the marked moving target object with an image capture device (40) provided on a moving platform, which image capture device is sensitive in the selected wavelength range of the invisible spectrum.

TARGET-TRACKING LASER DESIGNATOR

The present invention provides a laser tracking system including a laser generator for generating a beam of laser energy, a beam steerer for steering the beam of laser energy such that it moves in a search pattern, an d a receiving device that receives laser energy reflected from a targeted object and that causes the beam steerer to vary the search pattern in response to t he reflected laser energy. A tracking method associated with the laser tracking system includes the steps of generating a beam of laser energy, steering the beam of laser energy in a search pattern, detecting a hit spot formed from l aser energy being reflected from a targeted object, diminishing the size of the search pattern in response to the detection of the hit spot, and focusing th e diminished search pattern on a feature of the targeted object corresponding to the hit spot. The laser tracking system and associated method presented provide a number of advantages over conventional tracking systems. The laser tracking ...

DEVICE OF TIR OF AMMUNITION STARTING FROM A DRONE ARMS

La présente invention concerne le domaine des véhicules aériens sans pilote, plus couramment désignés sous l'appellation de drone. Plus précisément, l'invention s'applique à un système de drone armé (10), équipé notamment d'un dispositif de tir et d'une boule optronique (B) pilotable comprenant des moyens d'illumination de cibles (C). L'invention propose que le dispositif de tir soit orienté vers l'arrière, de manière à réduire les problèmes de masquage de la boule optronique (B) par des éléments situés dans son axe de visée, telle qu'une roulette avant (FW) par exemple. Par ailleurs, du fait d'un emploi opérationnel impliquant une phase (10S) de tir de munition et d'illumination de la cible (C) par l'arrière, le drone armé (10) s'éloignant de la cible visée, la vulnérabilité du drone (10) est amoindrie.

Laser illuminator for aerial approach back-up system - has beam selectively directed into diverging unit to produce controlled, uniform 360 degree illumination

The illuminator includes a laser source (1a) and an emission lens (1b) supplying a widened laser beam to a divergent unit (2). The diverging unit produces a fanned beam covering predetermined angles of direction and altitude (aS and aG). The illumination is not specifically directed and is uniform in the corresponding solid angle. The angles may attain maximum values of 2pi in the case of panoramic illumination. The diverging unit is formed from a diverging lens spreading light on to a conical mirror surface, the light arriving along the axis of the cone. The mirror may alternatively be a solid of revolution formed using a curved generating line, thus making for uniform distribution. The divergent optical system may be by-passed to provide a conventional target illumination system. The system may be used for simulation and training purposes.

PROCESS AND DEVICE TO CORRECT the POINTING Of an OPTICAL ILLUMINATOR ON an AIMED TARGET.

DEVICE FOR the Remote IDENTIFICATION Of an OPTICAL INSTRUMENT Of OBSERVATION

SYSTEM OF FIRE CONTROL SYSTEM HAS GLASSES Of OBSERVATION CONTROLLED BY an AUTOMATIC DEVICE OF CONTINUATION

Procédé pour combattre des cibles, de préférence blindées, utilisant un repérage par rayonnement.

Procédé pour combattre des cibles, avec repérage des cibles par rayonnement sur une arme au moyen d'un dispositif identifiant le rayonnement. On applique sur la cible un corps émettant le rayonnement correspondant à une température supérieure à celle de l'environnement de la cible et l'on dirige et l'on actionne l'arme sur le rayonnement émis. Applications notamment aux cibles blindées, pour le combat nocturne.

A METHOD FOR FIGHTING TARGETS, PREFERABLY BLINDEES, USING A LOCATION BY RADIATION

Procédé pour combattre des cibles, avec repérage des cibles par rayonnement sur une arme au moyen d'un dispositif identifiant le rayonnement. On applique sur la cible un corps émettant le rayonnement correspondant à une température supérieure à celle de l'environnement de la cible et l'on dirige et l'on actionne l'arme sur le rayonnement émis. Applications notamment aux cibles blindées, pour le combat nocturne. Method for fighting targets, with targeting by radiation on a weapon by means of a device identifying the radiation. A body emitting radiation corresponding to a temperature higher than that of the environment of the target is applied to the target and the weapon is directed and actuated on the emitted radiation. Applications in particular to armored targets, for night combat.

DEVICE OF DETECTION OF SPOT HAS MATRIC ECARTOMETRE.

La présente invention se situe dans le domaine des écartomètres utilisés pour la détection et la localisation de taches laser, et concerne plus précisément un détecteur de tache laser à écartomètre matriciel. Le dispositif selon l'invention comprend un circuit de lecture (ROIC) présentant une matrice de pixels (INT), une matrice de photodiodes (PH) réalisée sur un substrat unique (S), lesdites photodiodes (PH) comprenant chacune une électrode individuelle, et un dispositif de détection d'impulsion laser (D). La particularité de ce dispositif réside dans le fait que ladite matrice de photodiodes (PH) est hybridée sur ledit circuit de lecture (ROIC) par l'intermédiaire de bille (B) en matériau souple et conducteur, tel que de l'indium, mises au contact des pixels (INT) du circuit de lecture (ROIC), de sorte que ledit substrat unique (S) constitue une électrode commune à l'ensemble des photodiodes (PH) et que lesdites électrodes individuelles sont reliées auxdits pixels (INT) par lesdites ...

A METHOD AND APPARATUS FOR A STRIKE ON A TARGET

A method of conducting a strike against a target (1) using a designator (3) and a missile (5). The following steps are conducted: (i) the designator (3) designates the target (5) using a first signal (7), such as a laser; (ii) the missile (5) detects the laser (7') reflected off the target (1); (iii) after detecting the reflected laser, the missile (5) emits a second signal (9), such as a LADAR signal, to designate the target (1); (iv) the missile (5) tracks the so-designated target; (v) the designator (5) detects the LADAR signal (9") reflected off the target (1); and (vi) in response to detecting the reflected LADAR signal (9"), the designator stops the designation of the target (1). This may enable the designator (3) to perform other tasks, whilst the missile (5) tracks and engages the target.

LIGHTWEIGHT LASER DESIGNATOR RANGER FLIR OPTICS

A Midwave FLIR imaging optical apparatus (100) has both a narrow and wide field of view. The imaging optical apparatus (100) has a See Spot mode of operation, where a laser designator spot image is superimposed on the FLIR image in the narrow field of view. A laser rangefinder (108) receiver path is also provided. A shared aperture (112) collects incident radiation (110), which after manipulation by a plurality of optically significant surfaces (116), projects radiation to a detector (118). The imaging optical system (100) is lightweight and compact and efficiently transmits FLIR energy and a narrow band of laser energy so that a signal due to a source outside the pass bands of interest (including solar energy) will not adversely effect operation of the imaging optical apparatus (100).

Computerized simultaneous laser marking and targeting system

What is new in this invention, it is the complete automation of the remote marking process. It is completely computer controlled and made possible by laser printer type marking/pointer equipment. Also, completely new is the concept of embedding digital information into a laser beam or other coherent information vector and attaching this way data/information to any object or place. New is the idea of using a discrete information vector not only as a beacon but also as a selector for the marking of more than one target objects. New is the idea of completely software controlled computerized digital marking of places or objects for closing motion control loops. No on-site human operators/soldiers needed. No position sensors needed anymore, nothing is bolted down, easy to reconfigure any environment. The invention is a major step in robotics and controls, improving considerably the eye-hand coordination of robots, making fully possible the action of the digital world on the real/physical world ...

DEVICE FOR DETECTING LASER SPOT WITH MATRIX DEVIOMETER

СПОСОБ БОРЬБЫ С ПОДВИЖНОЙ ЦЕЛЬЮ (ВАРИАНТЫ)

Изобретение относится к способам борьбы с подвижной целью, прежде всего транспортным средством. Способ борьбы с подвижной целью включает следующие шаги: а) идентификация цели, б) маркирование цели маркировкой (10), невидимой в видимом спектре, но световозвращающей в выбранном диапазоне длин волн невидимого светового спектра, в) сопровождение промаркированной подвижной цели посредством предусмотренного на летательном аппарате, оснащенном ракетой, регистрирующего изображение устройства (40), которое является чувствительным в выбранном диапазоне длин волн невидимого спектра, г) поражение промаркированной подвижной цели ракетой, при этом маркировка (10) образована невидимой маркировочной краской, световозвращающей в выбранном невидимом диапазоне длин волн и содержащей лак и внедренные в него световозвращающие частицы, которые в выбранном диапазоне длин волн невидимого светового спектра имеют коэффициент преломления, достаточный для световозвращения, лак и внедренные в него частицы являются ...

Fernbedienbare Waffenstation und Verfahren zum Betreiben einer fernbedienbaren Waffenstation

Es wird eine fernbedienbare Waffenstation vorgeschlagen, bei welcher die Waffe und die Sensor-Einrichtung zur Zielerfassung starr verbunden sind. Die Sensor-Einrichtung umfasst zumindest eine Kamera und einen Laserentfernungsmesser zur Bestimmung einer Zielentfernung. Ferner umfasst die Waffenstation eine Nachführ-Einrichtung zur Nachführung einer Sichtlinie des Laserentfernungsmessers auf das Zielobjekt mittels eines bestimmten Aufsatzes und eines bestimmten Vorhalts sowie eine Verschiebe-Einheit zum Verschieben eines Mittenbereichs des von der Kamera aufgenommenen Zielbereichs in Abhängigkeit des bestimmten Aufsatzes und des bestimmten Vorhalts derart, dass das Bild des Zielobjekts in einem Zentrumbereich des verschobenen Mittenbereichs dargestellt wird.

Covert marking apparatus

Improvements in and relating to laser designator pods (LDP)

Dual-mode focal plane array for missile seekers

Machine to machine targeting maintaining positive identification

A method of targeting, which involves capturing a first video of a scene about a potential targeting coordinate by a first video sensor (102) on a first aircraft (100); transmitting the first video (232) and associated potential targeting coordinate by the first aircraft; receiving the first video on a first display in communication with a processor, the processor also receiving the potential targeting coordinate; selecting the potential targeting coordinate to be an actual targeting coordinate (226) for a second aircraft (116) in response to viewing the first video on the first display; and guiding a second aircraft toward the actual targeting coordinate; where positive identification of a target (114) corresponding to the actual targeting coordinate is maintained from selection of the actual targeting coordinate.

COVERT TARGET ACQUISITION WITH CODED SHORT-WAVE INFRARED GLASSES

Infrared vision systems, headpieces, and methods include an eyepiece and a body module. The eyepiece is configured to be worn over a user's eyes. The eyepiece includes an infrared sensor, configured to detect external infrared information. For example, the infrared sensor may include a plurality of short-wave infrared (SWIR) sensors. The eyepiece includes a display, configured to visually provide external infrared information to the user. For example, the display may include a see-through color display. The body module is in wired or wireless communication with the eyepiece. The eyepiece may include an adjustable strap, coupled to the eyepiece. The adjustable strap is configured to wrap around the user's head.

IMAGING INSTRUMENT FOR CONTROLLING A TARGET DESIGNATION

Un instrument d'imagerie pour contrôler une désignation de cible permet de visualiser une tache de désignation de cible (SP) au sein d'une scène (SC), tout en n'utilisant qu'un seul capteur d'image. Pour cela, un filtre est disposé sur le capteur d'image, dans une zone (ZC) restreinte de celui-ci. Le filtre permet d'augmenter un contraste et un rapport signal-sur-bruit pour une image de la tache de désignation de cible, lorsqu'un dépointage (DP) est effectué pour amener l'image de la tache de désignation de cible dans la zone du filtre.

MACHINE TO MACHINE TARGETING MAINTAINING POSITIVE IDENTIFICATION

A method of targeting, which involves capturing a first video of a scene about a potential targeting coordinate by a first video sensor (102) on a first aircraft (100); transmitting the first video (232) and associated potential targeting coordinate by the first aircraft; receiving the first video on a first display in communication with a processor, the processor also receiving the potential targeting coordinate; selecting the potential targeting coordinate to be an actual targeting coordinate (226) for a second aircraft (116) in response to viewing the first video on the first display; and guiding a second aircraft toward the actual targeting coordinate; where positive identification of a target (114) corresponding to the actual targeting coordinate is maintained from selection of the actual targeting coordinate.

TO-AIM FIRING AID

Dispositif d'aide au tir sans visée pour une arme (1), comportant un pointeur laser (2) placé sur l'arme (1), caractérisé en ce qu'il comporte également d'une part une micro caméra (4) pourvue de moyens pour localiser le point d'impact (6) du rayon laser (7) du pointeur (2) sur la cible (8) par analyse du signal reçu, et d'autre part un dispositif de visualisation (5) de ce point d'impact (6) devant l'oeil du tireur.

ENSEMBLE DE VISEE OPTIQUE, DE DESIGNATION ET DE POURSUITE D'OBJECTIF

L'ENSEMBLE COMPREND UN EMETTEUR LASER 100, UN LOCALISATEUR 200 POUR FOURNIR UNE INFORMATION ECARTOMETRIQUE ENTRE UNE CIBLE ET UN PROJECTILE, UN BLOC DE VISEE 300 PERMETTANT LA VISEE OPTIQUE DE LA CIBLE PAR UN OPERATEUR, ET DES MOYENS COLLIMATEURS 400 PERMETTANT LE CENTRAGE PAR CE DERNIER DU CHAMP DE VISEE SUR LA CIBLE. SELON L'INVENTION, IL EST PREVU DES MOYENS HARMONISATEURS 500, PAR EXEMPLE UN DIASPORAMETRE 501, 502 INTERPOSE ENTRE LES MOYENS COLLIMATEURS ET LE BLOC DE VISEE, POUR AJUSTER L'ORIENTATION ANGULAIRE DE LA DIRECTION DE COLLIMATION, DE MANIERE A FAIRE COINCIDER CELLE-CI O D AVEC LA DIRECTION DE REFERENCE A B OU DE VISEE A B, C D - C'EST-A-DIRE CELLE CORRESPONDANT A LA DIRECTION REELLE DE DESIGNATION ET DE VISEE DE LA CIBLE - ET AVEC LA DIRECTION DE LOCALISATION J K - C'EST-A-DIRE CELLE SOUS LAQUELLE LE LOCALISATEUR VOIT LA CIBLE DESIGNEE.

A METHOD FOR BEATING an OBJECTIVE BY MEANS OF PASSIVE PROJECTILES AND SYSTEM OF TIR FOR the EXECUTION OF THIS PROCESS

METHOD AND DEVICE INTEND TO ELIMINATE FROM THE UNDERGROUND MINES

Afin d'éliminer des mines souterraines par une méthode pour laquelle des mines souterraines sont détectées et localisées depuis un aéronef, le terrain est observé depuis l'aéronef (10) à l'aide d'un capteur à définition d'image (26) sur lequel est générée une image de la surface du terrain. Le capteur (26) répond à des différences de rayonnement et/ ou de réflexion de la surface du sol située au-dessus de la mine souterraine par rapport au milieu. La position de la mine souterraine est recherchée à partir de données d'image du capteur (26). Une installation de visée (20), un canon p. ex., est dirigé sur la position de la mine souterraine ainsi saisie. On fait détoner la mine souterraine par ce moyen.

System and method for identifying non-cooperative pulsed radiation sources in a field-of-view of an imaging sensor

A system and method for identifying a pulsed radiation source may include an imaging sensor having a frame rate that is less than a pulse repetition frequency (PRF) of the pulsed radiation source. A processing unit may be in communication with the imaging sensor, and be configured to (i) process a sequence of image data of a scene captured by the imaging sensor to determine whether radiation of the pulsed radiation source is detected, (ii) determine a PRF code of the pulsed radiation source from possible multiple different PRF codes based on the processed sequence of image data, and (iii) notify a user of the PRF code or information associated with the PRF code.

Marking system and method

A system for use in identifying a user includes a portable emitter transported with the user. The emitter includes a quantum cascade laser configured to emit a thermal beam identifying a location of the user in response to a command, the thermal beam having a wavelength between approximately 2 μm and approximately 30 μm.

Micro-radian class line of sight and centration stabilization system

This document discusses apparatus and methods for aligning and centering an articulated laser projection system. In an example, a laser projection system can include an alignment stabilization system configured to align an optical path to a reference and a centration stabilization system configured to center the optical path within an aperture. The alignment stabilization system can have an alignment stabilization processing path configured to receive alignment information from an alignment sensor, and the centration stabilization system can have a centration stabilization processing path configured to receive centration information from a centration sensor.

View-point guided weapon system and target designation method

A passive guidance system including a viewpoint capture system (VCS) including a first processor in communication with first memory and a first SWIR imager for creating a viewpoint image database having a plurality of images, at least one of the images having a target point. A weapon guidance module is in communication with the VCS and coupled to a weapon. The weapon guidance module includes a second processor in communication with second memory and a second SWIR imager for storing the viewpoint image database and correlating in-flight images from the second SWIR imager to provide guidance commands directing the weapon to the target point.

THERMAL MARKING SYSTEMS AND METHODS OF CONTROL

A target marking system includes a light source emitting a thermal beam and an optics assembly directing the thermal beam to impact a target, the target directing radiation to the optics assembly in response to the impact. The target marking system further includes a detector, and an optics assembly optically connected to the detector. 1. A target marking system , comprising:a light source configured to emit a beam of radiation;a controller connected to the light source and configured to pulse the beam emitted by the light source, the controller including a drive circuit comprising a first converter connected in series with a second converter, and a capacitor connected in series between the first and second converters; anda power source connected to the light source via the drive circuit.2. The target marking system of claim 1 , wherein at least one of the first and second converters comprises one of a buck converter claim 1 , a boost converter claim 1 , a SIPEX converter claim 1 , a flyback converter claim 1 , and an inverting converter.3. The target marking system of claim 1 , wherein the first converter is configured to maintain a voltage of the capacitor between approximately 2 volts and approximately 8 volts while the light source emits the beam.4. The target marking system of claim 1 , wherein the beam comprises a beam of thermal radiation.51. The target marking system claim 1 , wherein claim 1 , while the light source emits the beam claim 1 , the first converter is configured to draw a substantially constant current from the power source and to direct the substantially constant current to the capacitor.6. The target marking system of claim 1 , wherein the second converter is configured to convert a stored voltage of the capacitor to a desired voltage for driving the light source.7. The target marking system of claim 6 , wherein the light source comprises a quantum cascade laser claim 6 , and the desired voltage comprises between approximately 12 volts and ...

Marker System

A marker system includes at least one emitter. The emitter(s) emit light responsive to a flow of electrical current there through. The marker system includes a device for acquiring an incoming signal and a circuit for processing the incoming signal. The circuit for processing the incoming signal monitors the device for acquiring the incoming signal to determine if the incoming signal includes any of a plurality of incoming Identification Friend or Foe (IFF) and/or munitions-targeting signals. The circuit emits one of a plurality of responses by sending electrical current selectively through the emitter(s) and/or other feedback devices based upon which of the plurality of incoming Identification Friend or Foe (IFF) and/or munitions-targeting signals is detected by the means for processing. 1. A marker system , comprising:at least one emitter, each of the at least one emitter emits light responsive to a flow of electrical current through the emitter;means for acquiring incoming signals, the means for acquiring incoming signals detecting light in one or more wavelengths of light;means for processing the incoming signals, the means for processing the incoming signals monitors the means for acquiring the incoming signals and determines if the incoming signals includes any of a plurality of incoming Identification Friend or Foe (IFF) and munitions-targeting signals;means for notifying;upon detecting an incoming Identification Friend or Foe (IFF), the means for processing notifies regarding the Identification Friend or Foe (IFF); andupon detecting an incoming munitions-targeting signal, the means for processing notifies regarding the munitions-targeting signals.2. The marker system of claim 1 , whereby the means for acquiring the signal comprises two or more photo detectors claim 1 , each the photo detectors responsive to at least one wavelength of light selected from visible light claim 1 , near infrared light claim 1 , short-wave infrared claim 1 , mid-wave infrared ...

METHOD AND DEFENSE SYSTEM FOR COMBATING THREATS

It is proposed to make a threat better visible for a defensive measure. In this context, the threat () should be imaged more intensely for the defensive measure. For the purposes of more effective imaging, provision is made for the threat to emit a stronger IR signature and thus be able to stand out sufficiently against the background for the defensive measure. The stronger IR signature is caused by heating a surface of the threat, which is realized by a laser weapons system. The defensive measure can better detect this heating and has an IR seeker head to this end. 1. A method for defense from a threat comprising:detecting the threat;emitting a laser beam of a laser system onto the threat;striking the laser beam on a surface of the threat;heating, via the laser beam, the surface of the threat at least in a punctiform manner; anddetecting the heating by an IR seeker of a defense measure.2. The method as claimed in claim 1 , wherein the heating takes place in the front region of the threat.3. The method as claimed in claim 2 , wherein the front region is a tip claim 2 , ogive claim 2 , or hood of the threat.4. The method as claimed in claim 1 , wherein fuselage claim 1 , wings claim 1 , and also tail unit of the threat are adapted to be heated claim 1 , individually or in combination.5. A defense system for protecting an object from a threat claim 1 , the system comprising:at least one detection device;at least one laser weapon system for heating a surface of the threat; andat least one weapon for discharging a defense measure.6. The defense system as claimed in claim 5 , wherein the threat is stationary or moving.7. The defense system as claimed in claim 5 , wherein the defense measure is a rocket having an IR seeker.8. The defense system as claimed in claim 5 , wherein a laser is incorporated for the illumination.9. An object comprising a defense system as claimed in .10. The object as claimed in claim 9 , wherein the object is stationary or moving. This ...

VISION ENHANCEMENT APPARATUS

A vision apparatus implemented as an optical device is disclosed. The optical device comprises a plurality of small apertures in an opaque material that is attached to a pair of eyeglasses or is a contact lens. The number and arrangement of small apertures defines the field of view and brightness of the image projected onto the user's retina. The opaque material is a collimator, and only small areas of the user's retina are illuminated by cones of light passing through the small apertures. Therefore, all of the light is rendered in focus. The optical device resolves the refractive errors of the eye of the user, improving the visual acuity of the user in any activity that requires depth of field with a large and bright field of view. Two optical devices, one for each eye, provide binocular vision with a variety of aperture arrangements to suit the user's needs. 1. An apparatus , comprising:a collimator of static cling vinyl, the static cling vinyl having electrostatic attraction to a lens of eyeglasses, the attraction sufficient to attach the static cling vinyl to the lens, the lens having a length and a width, the collimator made of opaque material that is substantially circular having a diameter, the diameter being less than the length and less than the width of the lens of the eyeglasses;wherein the collimator has a plurality of apertures formed as holes in the opaque material, the apertures limiting light to cones of rays passing through the apertures and around an outside of the opaque material.2. The apparatus of claim 1 , wherein the plurality of apertures is arranged in a pattern claim 1 , the pattern of apertures forming a field of view of a desired shape claim 1 , size claim 1 , and brightness.3. The apparatus of claim 2 , wherein the shape of the field of view is substantially circular.4. The apparatus of claim 2 , wherein the shape of the field of view is substantially ellipsoid.5. The apparatus of claim 1 , wherein the eyeglasses are one of vision ...

COMPACT LASER AND GEOLOCATING TARGETING SYSTEM

A handheld targeting device that includes a geolocating system and a laser targeting system is provided. The geolocating system includes a laser range finder operable to emit a first pulsed laser beam toward an object from the first end of the housing and receive a returned first pulsed laser beam to calculate a distance to a target. By combining the calculated distance with a compass direction and position of the targeting device, a location of the object can be calculated. The laser targeting system includes a laser targeting marker operable to emit a second pulsed laser beam toward the object from the first end of the housing. Other vehicles or weapons can detect the second pulsed laser beam for indication of or guidance to the target. In one aspect, the laser range finder can share an optical lens with a thermal imager that captures infrared images. 1. A targeting device comprising;a housing;a laser range finder arranged in the housing;a laser targeting marker arranged in the housing;a digital imaging camera arranged in the housing;a first lens configured to transmit visible light to the digital imaging camera;a display screen;computer memory in communication with a controller, said computer memory storing a plurality of risk-estimate distances for respective ones of a plurality of munitions and a plurality of locations associated with other entities; and display on the display screen at least one image based on data obtained from the digital imaging camera;', 'instruct the laser rangefinder to emit a first pulsed laser beam;', 'calculate a location of an object based on the first pulsed laser beam as reflected by the object within a path of the first pulsed laser beam from the laser range finder;', 'calculate the distance from the object having reflected the first pulsed laser beam to any of the entity locations stored in the computer memory and compare said distance to the risk-estimate distance stored in the computer memory;', 'overlay on the at least one ...

Weapon Targeting System

A wearable electronic device displays an impact location that shows where a projectile fired from a weapon will hit a target and displays a bullseye location that shows a desired location where to hit the target. The wearable electronic device indicates firing the weapon when the impact location overlaps with the bullseye location.

MARKING SYSTEM AND METHOD

A system for use in identifying a user includes a portable emitter transported with the user. The emitter includes a quantum cascade laser configured to emit a thermal beam identifying a location of the user in response to a command, the thermal beam having a wavelength between approximately 2 μm and approximately 30 μm. 130-. (canceled)31. A system , comprising:a housing;a light source disposed within the housing and configured to emit a beam of infrared radiation;an optical system optically downstream from the light source, the optical system being configured to receive the beam and to direct the beam to exit the housing; and 'due to the characteristic being varied, the beam is distinguishable from a background object in a corresponding image generated by a thermal imager detecting the beam.', 'the controller being configured to vary a characteristic of the beam, during emission of the beam, such that, 'a controller operably connected to at least the light source,'}32. The system of claim 31 , wherein the characteristic comprises one of a divergence claim 31 , a wavelength claim 31 , a power claim 31 , or an intensity of the beam.33. The system of claim 31 , wherein the beam of radiation received by the optical system from the light source comprises a divergent beam.34. The system of claim 31 , wherein the housing defines a hermetically sealed environment claim 31 , and at least the light source and the optical system are disposed within the hermetically sealed environment.35. The system of claim 31 , wherein the optical system comprises a beam shaping optic claim 31 , and the characteristic is varied claim 31 , at least in part claim 31 , by changing a distance along an optical path between the beam shaping optic and the light source.36. The system of claim 31 , wherein the optical system comprises a first beam shaping optic and a second beam shaping optic claim 31 , and the first beam shaping optic is movable relative to at least the second beam shaping optic.37 ...

COVERT TARGET ACQUISITION WITH CODED SHORT-WAVE INFRARED GLASSES

Infrared vision systems, headpieces, and methods include an eyepiece and a body module. The eyepiece is configured to be worn over a user's eyes. The eyepiece includes an infrared sensor, configured to detect external infrared information. For example, the infrared sensor may include a plurality of short-wave infrared (SWIR) sensors. The eyepiece includes a display, configured to visually provide external infrared information to the user. For example, the display may include a see-through color display. The body module is in wired or wireless communication with the eyepiece. The eyepiece may include an adjustable strap, coupled to the eyepiece. The adjustable strap is configured to wrap around the user's head. 1. An infrared vision system , comprising: an infrared sensor, configured to detect external infrared information, and', 'a display, configured to visually provide external infrared information to the user; and, "an eyepiece, configured to be worn over a user's eyes, wherein the eyepiece includes:"}a body module in wired or wireless communication with the eyepiece.2. The infrared vision system of claim 1 , wherein the infrared sensor is a short-wave infrared sensor.3. The infrared vision system of wherein the infrared sensor detects at least one of a 1035 nm infrared laser and a 1550 nm infrared laser.4. The infrared vision system of claim 1 , wherein the display is a see-through color display.5. The infrared vision system of claim 1 , wherein the eyepiece further includes at least one camera configured to capture a field of view of the user.6. The infrared vision system of claim 1 , wherein the eyepiece further includes at least one infrared diode configured to emit a detectable infrared signal.7. The infrared vision system of claim 1 , wherein the external infrared information includes at least one of a ground based laser designator and an airborne laser designator.8. The infrared vision system of claim 1 , further comprising a weapon including an infrared ...

Imaging systems and methods

An imaging method includes receiving electromagnetic radiation at a focal plane array of a handheld device. The electromagnetic radiation is processed within the handheld device, and visible images are displayed on the handheld device. The displayed visible images are indicative of a scene, and include a designator and a designator identifier when a high frequency laser pulse is in the scene. The designator and designator identifier represent the high frequency pulsed electromagnetic radiation received by the focal plane array when a high frequency pulse is present in the scene.

Unmanned aerial vehicle

An unmanned aerial vehicle (UAV) adapted for transit in and deployment from a projectile casing is provided. The UAV includes a wing assembly coupled to the projectile casing and the wing assembly moveable between a closed position and a deployed position. The UAV further includes a propulsion system including at least one rotor disposed on the wing assembly to generate lift, wherein in the closed position, the wing assembly is substantially integral with the projectile casing and in the deployed position, the wing assembly is extended outwards from the projectile casing.

VERTICAL DROP SEGMENTED MUNITIONS DISPENSER

A munitions dispenser employs a plurality of launch tubes mounted in an array as a segmented dispenser assembly. Each tube in the array is configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture. A frame, mountable to an air vehicle, carries the array of launch tubes. A skin covers the array of launch tubes with the skin and frame with the array configured for nested engagement of multiple segmented assemblies. 1. A munitions dispenser comprising:a plurality of launch tubes mounted in an array as a segmented dispenser assembly, each tube in the array configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture;a frame carrying the array of launch tubes, said frame mountable to an air vehicle; and,a skin covering the array of launch tubes, said skin and frame with the array configured for nested engagement of multiple segmented assemblies.2. The munitions dispenser as defined in further comprising at least one sleeve mountable in the cylindrical bore of at least one of the plurality of tubes claim 1 , said sleeve adapted to closely receive one type of munition available as a selected munition.3. The munitions dispenser as defined in further comprising a retention mechanism adapted to releasably constrain the selected munition in the cylindrical bore.4. The munitions dispenser as defined in wherein the array of launch tubes comprise a plurality of US Common Launch Tubes claim 1 , tubes sleeved with US Common Launch Tubes claim 1 , tubes containing sleeves of a diameter accommodating expandable folded wings equipped munitions claim 1 , un-sleeved tubes or a combination thereof.5. The munitions dispenser as defined in wherein the array of tubes are inclined to a rear of the munitions dispenser to enhance munitions separation.6. The munitions dispenser as defined in further comprising ...

THERMAL MARKING SYSTEMS AND METHODS OF CONTROL

A target marking system includes a light source configured to emit a beam of thermal radiation and to impinge the beam onto a target. The system also includes a detector configured to collect radiation passing from the target to the detector along a path. The radiation passing from the target in response to impingement of the beam onto the target. The system further includes an optics assembly disposed optically upstream of the detector along the path. The optics assembly includes at least one of an afocal power changer, a camera objective, a catadioptric lens, and a zoom system configured to condition the radiation passing from the target to the detector. 1. A target marking system , comprising:a light source configured to emit a beam of thermal radiation and to impinge the beam onto a target; 'the detector being configured to collect radiation passing from the target to the detector along a path, the radiation passing from the target in response to the beam impinging the target; and', 'a detector comprising a plurality of pixels and at least one display component, the at least one display component being configured to assist in forming an image of the beam impinging the target,'}an optics assembly disposed optically upstream of the detector along the path, the optics assembly comprising at least one of an afocal power changer, a camera objective, a catadioptric lens, and a zoom system configured to condition the radiation passing from the target to the detector.2. The target marking system of claim 1 , further including a connector removably coupling the optics assembly to the detector.3. The target marking system of claim 2 , wherein the connector is disposed at least partially between the detector and the optics assembly.4. The target marking system of claim 2 , wherein the connector comprises a first component removably connected to the optics assembly and a second component removably connected to the detector.52. The target marking system claim 2 , wherein a ...

Integrated Targeting Device

An integrated targeting device comprising a housing, the housing comprising an input aperture and an output aperture, a geolocation module configured to estimate the geolocation of a selected target, an imaging module comprising an imaging camera, a laser comprising a seed laser configured to emit a seed laser beam and a moveable optical reflector, a display; and a processor operatively coupled to the laser module, the imaging module, the geolocation module; and the display.

RETROREFLECTOR ARRAY AND COVER FOR OPTICAL BULLET TRACKING

Systems, devices, and methods including a bullet; a retroreflector array adhered to a base of the bullet, the retroreflector array having prism facets with a periodicity between 0.2 mm-2.0 mm; and a cover disposed over the retroreflector array and hermetically sealed at the base of the bullet; where the cover is disposed over the retroreflector array in a first position prior to firing, and where the cover is released from the base of the bullet in a second position after firing. 1. A system comprising:a bullet;a retroreflector array adhered to a base of the bullet;a cover disposed over the retroreflector array and hermetically sealed at the base of the bullet; andan o-ring disposed between the cover and the base of the bullet, the o-ring hermetically sealing the retroreflector array at the base of the bullet.2. The system of wherein the retroreflector array is disposed on top of the base of the bullet.3. The system of wherein the cover is clamped onto a perimeter of the retroreflector array.4. The system of wherein the bullet comprises an indentation in the base of the bullet claim 1 , and wherein the retroreflector array is disposed in the indentation in the base of the bullet.5. The system of wherein the cover is clamped onto the base of the bullet.6. The system of wherein the cover is disposed over the retroreflector array in a first position prior to firing claim 1 , and wherein the cover is released from the base of the bullet in a second position after firing.7. The system of wherein the base of the bullet comprises three or more equidistant dimples cut into the base of the bullet.8. The system of wherein the cover comprises three or more equidistant fingers that mate into each of the three or more equidistant dimples.9. The system of wherein the three or more equidistant fingers detach from the three or more equidistant dimples in the second position due to at least one of: wind resistance on the three or more equidistant fingers and centrifugal force on the ...

TARGET MARKING DEVICE AND TARGET TRACKING AND PROCESSING SYSTEMS COMPRISING SUCH A DEVICE

The target marking device () comprises a drone () which is provided with at least one transmitter (), the transmitter () comprising an activation element () for activating it so that it transmits at a given time a signal (S) which represents a position information item, the transmitter () being configured to transmit at least one of the following signals: an infrared signal, a light signal, a sound signal, a signal generated by a chemical substance, the target marking device () being part of a target tracking system () and/or a target processing system which is provided with movable machinery (). 1124. A target marking device , said device () comprising at least one drone () provided with at least one emitter () capable of emitting a positional information ,{'b': 4', '10', '4', '4, 'characterized in that the emitter () comprises an activation element () for activating said emitter () so that it emits at least one signal (S) representing the positional information at least at a given time, and in that the emitter () is configured to emit at least one of the following signals: an infrared signal, a light signal, a sound signal, a signal generated by a chemical substance.'}24. The device according to claim 1 , characterized in that the emitter () configured to emit an infrared signal comprises one of the following heat sources: a heat source of chemical type claim 1 , a heat source of electrical type.34. The device according to claim 1 , characterized in that the emitter () configured to emit a light signal is configured to emit a continuous light signal and/or a discontinuous light signal and/or a modulated light signal.44. The device according claim 1 , characterized in that the emitter () configured to emit a sound signal is configured to emit a modulated sound signal.5. The device according to claim 4 , characterized in that the modulated sound signal is encrypted.64. The device according claim 1 , characterized in that the emitter () configured to emit a signal ...

RECOIL SPRING GUIDE MOUNTED TARGET MARKER

In an exemplary embodiment of the present disclosure, a target marker for a firearm may comprise a module having a first portion, and a second portion electrically connected and coupled to the first portion. A light source may be disposed within and electrically connected to the second portion. An optical component may be coupled to the first portion at a first fixed distance from the light source. A circuit board may be electrically connected to the light source via at least one lead, wherein the lead may permit relative movement between the circuit board and the light source and may maintain a second fixed distance between the circuit board and the light source. 1. A target marker for a firearm , comprising:a module having a first portion, and a second portion electrically connected and coupled to the first portion;a light source disposed within and electrically connected to the second portion;an optical component coupled to the first portion at a first fixed distance from the light source; anda circuit board electrically connected to the light source via at least one lead, wherein the at least one lead permits relative movement between the circuit board and the light source and maintains a second fixed distance between the circuit board and the light source.2. The target marker of claim 1 , wherein the optical component comprises a lens configured to collimate a beam of radiation emitted by the light source.3. The target marker of claim 1 , wherein the first portion is made from a first conductive material claim 1 , and the second portion is made from a second conductive material that is less conductive than the first conductive material.4. The target marker of claim 1 , wherein the first portion is made from a first conductive material claim 1 , and the second portion is made from a second conductive material wherein the first conductive material is substantially equally as conductive as the second conductive material.5. The target marker of claim 1 , wherein ...

THERMAL MARKING SYSTEMS AND METHODS OF CONTROL

A target marking system includes a light source configured to emit a beam of thermal radiation and to impinge the beam onto a target. The system also includes a detector configured to collect radiation passing from the target to the detector along a path. The radiation passing from the target in response to impingement of the beam onto the target. The system further includes an optics assembly disposed optically upstream of the detector along the path. The optics assembly includes at least one of an afocal power changer, a camera objective, a catadioptric lens, and a zoom system configured to condition the radiation passing from the target to the detector. 1. A target marking system , comprising:a light source configured to emit a beam of thermal radiation and to impinge the beam onto a target;a detector comprising a plurality of pixels and at least one display component, the at least one display component being configured to assist in forming an image of the beam impinging the target,the detector being configured to collect radiation passing from the target to the detector along a path, the radiation passing from the target in response to the beam impinging the target; andan optics assembly disposed optically upstream of the detector along the path, the optics assembly comprising at least one of an afocal power changer, a camera objective, a catadioptric lens, and a zoom system configured to condition the radiation passing from the target to the detector.226-. (canceled) The present application is a continuation-in-part of U.S. patent application Ser. No. 13/359,069, filed Jan. 26, 2012, which is a continuation-in-part of U.S. patent application Ser. No. 13/271,924, filed Oct. 12, 2011, which claims the benefit of U.S. Provisional Application No. 61/392,697, filed Oct. 13, 2010. The entire disclosures of each of these applications are incorporated herein by reference.Not applicable.Not applicable.The present disclosure relates to systems and methods for marking a ...

Multi-Target Optical Designator

A device and method for selectively illuminating and designating multiple targets in the air or on the ground simultaneously. The device comprises a light source, a switching array and a ball lens. Light from the light source is routed through the switching array, which can addressably output multiple light beams simultaneously. The light beams from the switching array illuminate the backside of a low F-number ball lens. The ball lens creates highly collimated output beams independently (and simultaneously) from any of the output source points of the switching array. These output beams can be used to simultaneously designate multiple targets. When the target illuminating device includes an optional detector array, light scattered from targets can be refracted by the balls lens to impinge on the detector array. Signals from the detector array representing the received light beams can be used for target imaging. 1. A device for optically designating multiple targets simultaneously comprising:a. a light source;b. a switching array, the array configured to output at least a first addressable light beam and a second addressable light beam, the beams generated from light received from the light source; andc. a ball lens configured to receive the first light beam and output the first light beam to a first direction when the first beam is illuminated and to receive the second light beam and output the second beam to a second direction when the second input beam is illuminated,wherein the first direction and the second direction differ.2. The device according to claim 1 , where the ball lens is a spherical lens.3. The device according to claim 1 , wherein the light source is an array of lasers.4. The device according to claim 3 , wherein the laser array comprises vertical-cavity surface-emitting lasers.5. The device according to claim 1 , wherein the light source is an array of light emitting diodes.6. The device according to claim 1 , wherein the light source is modulated.7 ...

SET FOR POSITIONING AND ALIGNING A DISRUPTOR FOR THE DEACTIVATION OF A TARGET

A set for dismantling a target includes a disruptor having a firing axis and a device for aligning and positioning the disruptor in a deactivation direction relative to the target. A firing sub-set includes a movable mounting having a movable carriage mounted thereon to which the disruptor is fastened and provided with components for adjustment translation and orientation relative to the mounting. A mirror is oriented rearward of the disruptor and fastened to the disruptor perpendicular to the firing axis and having a centering mark centered on that axis. A pointing sub-set includes a laser mounted thereto and adapted to emit beams along an aiming line coaxial with the deactivation direction. The pointing sub-set is behind the firing sub-set relative to a target such that the mirror intercepts the laser aiming line at its centering mark and the disrupter firing axis is coaxial with the laser aiming line. 1. A set for dismantling a target comprising a disruptor having a firing axis and a device for aligning and positioning the disruptor in a deactivation direction that is determined relative to the target , the set comprising:a firing sub-set comprising a movable mounting on which is mounted to a movable carriage to which the disruptor is fastened and which is provided with components for adjustment in translation and in orientation relative to the mounting and a mirror fastened to the disruptor and oriented on an opposite side of the disruptor relative to the target and perpendicular to the firing axis, the mirror having a centering mark centered on firing axis; anda pointing sub-set comprising a mount on which is mounted a laser adapted to emit beams along an aiming line coaxial with the deactivation direction, the pointing sub-set being disposed opposite the firing sub-set relative to the target, such that the mirror intercepts the aiming line of the laser at the centering mark and is perpendicular thereto, whereby the firing axis of the disruptor is coaxial with ...

SYSTEM AND METHOD FOR TARGET ACQUISITION, AIMING AND FIRING CONTROL OF KINETIC WEAPON

A target acquisition is disclosed for use with a weapon in acquiring at least one target for the weapon. The system may make use of a mapping sensor subsystem which forms a controllably scanned electromagnetic wave energy subsystem for illuminating a scene where one or more targets are potentially present with selectively scanned electromagnetic wave energy. The system may also incorporate a control subsystem including a target/object recognition software module which uses information supplied by the mapping sensor subsystem to identify at least one target in the scene which forms a valid target to be engaged by the weapon. The system may limit firing of the weapon until a predetermined degree of aiming accuracy is achieved relative to the valid target. 1. A target acquisition system for use with a weapon in acquiring at least one target for the weapon , the system comprising:a mapping sensor subsystem which forms an electromagnetic wave energy subsystem for illuminating a scene where one or more targets are potentially present with selectively scanned electromagnetic wave energy; anda control subsystem including a target/object recognition software module which uses information supplied by the mapping sensor subsystem to identify at least one said target in the scene which forms a valid target to be engaged by the weapon, and to limit firing of the weapon until a predetermined degree of aiming accuracy is achieved relative to the valid target.2. The system of claim 1 , wherein the control subsystem comprises:an electronic controller; andwherein the target/object recognition software module comprises a target/object recognition/prioritization software module which analyzes the one or more targets to determine if the one or more targets form a valid target, and when more than one valid target is identified, prioritizes the valid targets such that a specific one of the valid targets is selected based on it being closest to a user operating the weapon.3. The system of ...

SYSTEM FOR TRACKING AND GRAPHICALLY DISPLAYING LOGISTICAL, BALLISTIC, AND REAL TIME DATA OF PROJECTILE WEAPONRY AND PERTINENT ASSETS

The system includes various components to track and graphically display data related to a user, a weapon, munitions for the weapon, other munitions and equipment used by the user, and similar information about other users. The system can include a display device that can be attached to the weapon. A user can look through the display device while looking down the line-of-sight of the weapon to obtain the data on a heads-up-display. The information displayed can include the point-of-impact of a projectile to be fired from the weapon, the number of unused rounds in the user's inventory, whether a magazine is inserted into the weapon, a map of the field of view, identification of friendlies and hostiles, a distance to a target, a count of other assets (e.g., munitions and other equipment) in the user's inventory, and other information about other users. 122-. (canceled)23. A method for generating a map of a field of view , the method comprising:obtaining GPS sensor data regarding a field of view;processing the GPS sensor data to generate information, the information including identification of an object within the field of view as a friendly or a hostile; andgenerating a map of the field of view with the information superimposed on the map.24. The method recited in claim 23 , further comprising:displaying the map via a heads-up display.25. The method recited in claim 24 , further comprising:using the heads-up display for providing a line-of-sight of a rifle.26. The method recited in claim 25 , wherein:the information further includes a point-of-impact of a projectile.27. The method recited in claim 25 , wherein:the information further includes a position of the heads-up display, a position of the heads-up display relative to another heads-up display identified as a friendly, a position of an object identified as a hostile relative to the heads-up display, and/or a position of an object identified as a hostile relative to another object identified as a hostile.28. The ...

THERMAL MARKING SYSTEMS AND METHODS OF CONTROL

A target marking system includes a light source configured to emit a beam of thermal radiation and to impinge the beam onto a target. The system also includes a detector configured to collect radiation passing from the target to the detector along a path. The radiation passing from the target in response to impingement of the beam onto the target. The system further includes an optics assembly disposed optically upstream of the detector along the path. The optics assembly includes at least one of an afocal power changer, a camera objective, a catadioptric lens, and a zoom system configured to condition the radiation passing from the target to the detector. 1. A target marking system , comprising:a light source configured to emit a beam of thermal radiation and to impinge the beam onto a target;a detector comprising a plurality of pixels and at least one display component, the at least one display component being configured to assist in forming an image of the beam impinging the target,the detector being configured to collect radiation passing from the target to the detector along a path, the radiation passing from the target in response to the beam impinging the target; andan optics assembly disposed optically upstream of the detector along the path, the optics assembly comprising at least one of an afocal power changer, a camera objective, a catadioptric lens, and a zoom system configured to condition the radiation passing from the target to the detector.226-. (canceled) The present application is a continuation-in-part of U.S. patent application Ser. No. 13/359,069, filed Jan. 26, 2012, which is a continuation-in-part of U.S. patent application Ser. No. 13/271,924, filed Oct. 12, 2011, which claims the benefit of U.S. Provisional Application No. 61/392,697, filed Oct. 13, 2010. The entire disclosures of each of these applications are incorporated herein by reference.Not applicable.Not applicable.The present disclosure relates to systems and methods for marking a ...

Systems, Methods and Computer-Readable Media for Improving Platform Guidance or Navigation Using Uniquely Coded Signals

A spatially-distributed architecture (SDA) of antennas transmits respective uniquely coded signals. A first receiver having a known position in a coordinate system defined by the SDA receives reflected versions of the uniquely coded signals. A first processor receives the reflected versions of the uniquely coded signals and identifies a position of a non-cooperative object in the coordinate system. A platform with a platform receiver receives non-reflected versions of the uniquely coded signals. The platform determines a position of the platform in the coordinate system. In an example, the platform uses a self-determined position and a position of the non-cooperative object communicated from the SDA to navigate or guide the platform relative to the non-cooperative object. In another example, the platform uses a self-determined position and information from an alternative signal source in a second coordinate system to guide the platform. Guidance solutions may be generated in either coordinate system. 1. A method , comprising:receiving, with a first receiver connected to a platform, a set of uniquely identifiable signals transmitted from respective spatially-distributed antenna arrays separate from the platform;determining, with a platform processor in communication with the first receiver, one or more of a position, a motion and an orientation of the platform in a first coordinate system, wherein the platform processor identifies at least one of the position, motion and orientation of the platform using one or more characteristics of the uniquely identified signals received by the first receiver;receiving one or more signals containing information about a position of a non-cooperative object, wherein the information about the position of the non-cooperative object is communicated in an established inertial frame or the first coordinate system defined by the spatially-distributed antenna arrays;generating, with the platform processor, a guidance solution responsive ...

Aircraft payload apparatus and method

A method of providing apparatus comprising: providing a first store and a first payload on or in the first store, the first store being for mounting to the outside of an aircraft; acquiring aerodynamic properties, moments of inertia, and the mass distribution of the first store and first payload; providing a second store and a second payload, the second payload being on or in the second store, the second store being for mounting to the outside of the aircraft, the second payload being different to the first, the second payload comprising a sensor and/or a projecting means; and configuring the second store and the second payload such that the aerodynamic properties, moments of inertia, and mass distribution of the second store and the second payload are substantially the same as those of the first store and first payload.

METHOD AND APPARATUS FOR VARIABLE TIME PULSE SAMPLING

Methods and apparatus for variable time sampling of optical pulses by a unit cell are disclosed. The methods may include detecting whether an amplitude of an optical pulse incident on one or more photo-detecting elements exceeds a sampling threshold, and while the pulse amplitude remains above the sampling threshold, iteratively sampling the optical pulse at a sampling rate that varies based on changes in the pulse amplitude. 1. A method of variable time sampling of optical pulses by a unit cell , comprising:detecting whether an amplitude of an optical pulse incident on one or more photo-detecting elements exceeds a sampling threshold; andwhile the pulse amplitude remains above the sampling threshold, iteratively sampling the optical pulse at a sampling rate that varies based on changes in the pulse amplitude.2. The method of claim 1 , wherein iteratively sampling the optical pulse comprises resetting an interval of the sampling rate upon each discrete detection of a change in the pulse amplitude exceeding at least one amplitude change threshold.3. The method of claim 2 , further comprising setting the at least one amplitude change threshold prior to iteratively sampling the optical pulse.4. The method of claim 2 , further comprising dynamically setting the at least one amplitude change threshold in response to an input.5. The method of claim 1 , wherein the sampling rate varies in proportion to changes in an integral of the pulse amplitude.6. The method of claim 5 , wherein iteratively sampling the optical pulse comprises resetting an interval of the sampling rate upon each discrete detection of a change in the pulse amplitude integral exceeding at least one amplitude integral change threshold.7. The method of claim 1 , further comprising increasing the sampling rate with increasing pulse amplitude claim 1 , and decimating the sampling rate with decreasing pulse amplitude.8. The method of claim 1 , wherein further comprising capturing a peak amplitude of the pulse ...

THERMAL MARKING SYSTEMS AND METHODS OF CONTROL

A target marking system includes a light source configured to emit a beam of thermal radiation and to impinge the beam onto a target. The system also includes a detector configured to collect radiation passing from the target to the detector along a path. The radiation passing from the target in response to impingement of the beam onto the target. The system further includes an optics assembly disposed optically upstream of the detector along the path. The optics assembly includes at least one of an afocal power changer, a camera objective, a catadioptric lens, and a zoom system configured to condition the radiation passing from the target to the detector. 127-. (canceled)28. A system , comprising:a handheld housing;a light source disposed within the housing; and first radiation emitted by the light source and having a first wavelength, and', 'second radiation having a second wavelength different from the first wavelength., 'an optics assembly configured to form an emitted beam with radiation received from the light source, the emitted beam comprising29. The system of claim 28 , wherein the second radiation is emitted by the light source.30. The system of claim 28 , wherein:the light source comprises a first light source,the system further comprises a second light source disposed within the housing, andthe second radiation is emitted by the second light source at the second wavelength.31. The system of claim 28 , wherein the first wavelength and the second wavelength are between approximately 2 μm and approximately 30 μm.32. The system of claim 28 , wherein the first wavelength is between approximately 2 μm and approximately 5 μm claim 28 , and the second wavelength is between approximately 8 μm and approximately 30 μm.33. The system of claim 28 , further comprising a controller operably connected to the light source claim 28 , the controller being configured to:operate the light source in at least one of a first duty cycle, or a second duty cycle different from the ...

Marker System

A marker system includes at least one emitter. The emitter(s) emit light responsive to a flow of electrical current there through. The marker system includes a device for acquiring an incoming signal and a circuit for processing the incoming signal. The circuit for processing the incoming signal monitors the device for acquiring the incoming signal to determine if the incoming signal includes any of a plurality of incoming Identification Friend or Foe (IFF) and/or munitions-targeting signals. The circuit emits one of a plurality of responses by sending electrical current selectively through the emitter(s) and/or other feedback devices based upon which of the plurality of incoming Identification Friend or Foe (IFF) and/or munitions-targeting signals is detected by the means for processing. 1. A marker system , comprising:at least one emitter, each of the at least one emitter emits light responsive to a flow of electrical current through the emitter;means for acquiring incoming signals;means for processing the incoming signals, the means for processing the incoming signals monitors the means for acquiring the incoming signals and determines if the incoming signals includes any of a plurality of incoming Identification Friend or Foe (IFF) and munitions-targeting signals;upon detecting an incoming Identification Friend or Foe (IFF), the means for processing emits a first response by flowing electrical current through any or all of the at least one emitter; andupon detecting an incoming munitions-targeting signals, the means for processing emits a second response by flowing electrical current through any or all of the at least one emitter, the second response being different from the first response.2. The marker system of claim 1 , whereby the means for acquiring the signal comprises one or more photo detectors claim 1 , the photo detectors responsive to at least two different wavelengths of light selected from visible light claim 1 , near-wave infrared light claim 1 , ...

THERMAL MARKING SYSTEMS AND METHODS OF CONTROL

A target marking system includes a light source configured to emit a beam of thermal radiation and to impinge the beam onto a target. The system also includes a detector configured to collect radiation passing from the target to the detector along a path. The radiation passing from the target in response to impingement of the beam onto the target. The system further includes an optics assembly disposed optically upstream of the detector along the path. The optics assembly includes at least one of an afocal power changer, a camera objective, a catadioptric lens, and a zoom system configured to condition the radiation passing from the target to the detector. 1. (canceled)2. (canceled)3. (canceled)4. (canceled)5. (canceled)6. (canceled)7. (canceled)8. (canceled)9. (canceled)10. (canceled)11. (canceled)12. (canceled)13. (canceled)14. (canceled)15. (canceled)16. (canceled)17. (canceled)18. (canceled)19. (canceled)20. (canceled)21. (canceled)22. (canceled)23. (canceled)24. (canceled)25. (canceled)26. (canceled)27. A target marking system , comprising:a light source configured to emit a beam of thermal radiation and to impinge the beam onto a target; anda detector having a plurality of thermal radiation sensitive pixels that can be scanned to obtain signals that are used to form a thermal image of a field of view, with the detector being configured to collect thermal radiation passing from the field of view to the detector including radiation passing from the target in response to the beam impinging the target;wherein the light source is energized during a time period in which the detector scans thermal radiation sensors corresponding a portion of the field of view likely to be impinged upon by the emitted beam of the target marking system and wherein the light source does not emit emit a beam of thermal radiation during scanning of at least one other thermal radiation sensitive pixel outside during scanning outside of the portion of the field of view likely to be impinged ...

RIFLESCOPE WITH INTEGRATED WIND SENSOR AND TARGETING DISPLAY

Techniques are disclosed for providing the weapon-mounted optical scope that provides for wind sensing and the display a ballistic solution without the need for a separate device. Embodiments may include various additional sensors housed within the weapon-mounted optical scope to provide data for the ballistic solution calculation. Embodiments may further include a display at the input aperture rather than internally at the first-focal-plane, enabling for simpler, more cost effective embodiments. Additionally or alternatively, embodiments may include a laser, separate from the wind sensing laser, to perform range-finding functions, and/or an enhanced-image assembly. 1. A weapon-mounted optical scope comprising:an objective lens;a display assembly configured to, when displaying an object, emit light such that the emitted light enters the objective lens;an eyepiece configured to enable a user to see an image from light entering the objective lens;one or more orientation sensors;a positioning unit;a first laser;an optical receiver comprising two subassemblies, wherein each subassembly comprises a sensor and a set of one or more lenses configured to direct light toward the sensor; and cause the first laser to emit a laser beam;', 'obtain measurements of reflected light of the laser beam from the optical receiver;', 'calculate a wind measurement based on the obtained measurements of the reflected light;', 'determine a ballistic solution based on the wind measurement and data from the one or more orientation sensors and the positioning unit; and', 'cause the display assembly to display information indicative of the ballistic solution., 'a processing unit communicatively coupled with the first laser, the optical receiver, the one or more orientation sensors, and the positioning unit, wherein the processing unit is configured to2. The weapon-mounted optical scope of claim 1 , further comprising a second laser claim 1 , wherein the processing unit is further configured to: ...

LIGHT IRRADIATION DEVICE AND LIGHT IRRADIATION SYSTEM

A light irradiation device includes: at least one imaging means that images a monitoring region to continue to accurately irradiate a moving target with light; at least one projection means that irradiates the monitoring region with signal light; a control means that controls the imaging means to image the monitoring region and controls the projection means to emit the signal light; at least one propeller that moves the own device in the air; and a flight control means that controls flight of the own device by controlling the propeller, the control means controlling, when recognizing a light irradiation target to be irradiated with the signal light on image data imaged by the imaging means, the projection means to emit the signal light toward the light irradiation target. 1. An irradiation system comprising: a projector;', 'a controller; and', 'a flight controller,, 'a flight device comprisingwherein the projector is configured to emit a light,wherein the flight controller is configured to control flight of the flight device,wherein the controller is configured to control the projector to, if an irradiation target to be irradiated is detected in an image capturing a monitoring region, emit the light as a guidance light to the irradiation target; anda flying object configured to fly toward the guidance light.2. The irradiation system according to claim 1 , wherein the flight device further includes at least on slave device claim 1 ,wherein the slave device is a detachable device including a function for emitting the guiding light.3. The irradiation system according to claim 1 , wherein the controller is configured to control the projector to emit the guidance light toward an estimated position of the irradiation target.4. An irradiation method comprising:detecting, by at least one computer, an irradiation target to be irradiated in an image capturing a monitoring region; andcontrolling, by the at least one computer, a projector to, if the irradiation target is ...

ENCODED SIGNAL DETECTION AND DISPLAY

A target marking system includes a light source emitting a thermal beam having a predetermined temporal modulation, and an optics assembly directing the thermal beam to impact a target, the target directing radiation to the optics assembly in response to the impact. A portion of the radiation having the predetermined temporal modulation. The target marking system further includes a detector configured to distinguish the portion of the radiation having the predetermined temporal modulation from a remainder of the radiation, the portion of the radiation passing to the director through the optics assembly. The system also includes a readout integrated circuit, the detector directing an input signal to the readout integrated circuit, and the readout integrated circuit producing a digitally enhanced output signal in response to receipt of the input signal. 1. A target marking system , comprising:(a) a light source emitting a thermal beam having a predetermined temporal modulation;(b) an optics assembly directing the thermal beam to impact a target, the target directing radiation to the optics assembly in response to the impact, a portion of the radiation having the predetermined temporal modulation;(c) a detector configured to distinguish the portion of the radiation having the predetermined temporal modulation from a remainder of the radiation, the portion of the radiation passing to the detector through the optics assembly; and(d) a readout integrated circuit, the detector directing an input signal to the readout integrated circuit, and the readout integrated circuit producing a digitally enhanced output signal in response to receipt of the input signal.2. The system of claim 1 , wherein the detector comprises an uncooled microbolometer array.3. The system of claim 1 , wherein the detector comprises an array of heat-sensitive pixels.4. The system of claim 1 , further including a display operably connected to the detector.5. The system of claim 4 , wherein the detector ...

RECOIL SPRING GUIDE MOUNTED TARGET MARKER

In an exemplary embodiment of the present disclosure, a target marker for a firearm may comprise a module having a first portion, and a second portion electrically connected and coupled to the first portion. A light source may be disposed within and electrically connected to the second portion. An optical component may be coupled to the first portion at a first fixed distance from the light source. A circuit board may be electrically connected to the light source via at least one lead, wherein the lead may permit relative movement between the circuit board and the light source and may maintain a second fixed distance between the circuit board and the light source. 1. A target marker for a firearm , comprising:a module having a first portion, and a second portion electrically connected and coupled to the first portion;a light source disposed within and electrically connected to the second portion;an optical component coupled to the first portion at a first fixed distance from the light source; anda circuit board electrically connected to the light source via at least one lead, wherein the at least one lead permits relative movement between the circuit board and the light source and maintains a second fixed distance between the circuit board and the light source.2. The target marker of claim 1 , wherein the optical component comprises a lens configured to collimate a beam of radiation emitted by the light source.3. The target marker of claim 1 , wherein the first portion is made from a first conductive material claim 1 , and the second portion is made from a second conductive material that is less conductive than the first conductive material.4. The target marker of claim 1 , wherein the first portion is made from a first conductive material claim 1 , and the second portion is made from a second conductive material wherein the first conductive material is substantially equally as conductive as the second conductive material.5. The target marker of claim 1 , wherein ...

Projectile system with capture net

A modular rocket system includes a guidance module defining a nose and including a guidance system for guiding said modular rocket system toward a target. A flight control module is removably attached to the guidance module and includes a plurality of airfoils that are controllable to control a direction of travel of the modular rocket system. A net module is removably attached to the flight control module and houses a net and a deployment mechanism. The deployment mechanism is configured to eject the net from the net module toward the target. A rocket module is removably attached to the net module, and includes a rocket motor configured to propel the modular rocket system.

Machine to Machine Targeting Maintaining Positive Identification

A method of targeting, which involves capturing a first video of a scene about a potential targeting coordinate by a first video sensor on a first aircraft; transmitting the first video and associated potential targeting coordinate by the first aircraft; receiving the first video on a first display in communication with a processor, the processor also receiving the potential targeting coordinate; selecting the potential targeting coordinate to be an actual targeting coordinate for a second aircraft in response to viewing the first video on the first display; and guiding a second aircraft toward the actual targeting coordinate; where positive identification of a target corresponding to the actual targeting coordinate is maintained from selection of the actual targeting coordinate.

RETROREFLECTOR ARRAY AND COVER FOR OPTICAL BULLET TRACKING

Systems, devices, and methods including a bullet; a retroreflector array adhered to a base of the bullet, the retroreflector array having prism facets with a periodicity between 0.2 mm-2.0 mm; and a cover disposed over the retroreflector array and hermetically sealed at the base of the bullet; where the cover is disposed over the retroreflector array in a first position prior to firing, and where the cover is released from the base of the bullet in a second position after firing. 1. A system comprising:a bullet;a retroreflector array adhered to a base of the bullet, the retroreflector array having prism facets with a periodicity between 0.2 mm-2.0 mm;a cover disposed over the retroreflector array and hermetically sealed at the base of the bullet; andan o-ring disposed between the cover and the base of the bullet, the o-ring hermetically sealing the retroreflector array at the base of the bullet;wherein the cover is disposed over the retroreflector array in a first position prior to firing, and wherein the cover is released from the base of the bullet in a second position after firing.2. The system of wherein the prism facets of the retroreflector array have a periodicity between 0.3 mm-1.0 mm.3. The system of wherein the retroreflector array is disposed on top of the base of the bullet.4. The system of wherein the cover is clamped onto a perimeter of the retroreflector array.5. The system of wherein the bullet comprises an indentation in the base of the bullet claim 1 , and wherein the retroreflector array is disposed in the indentation in the base of the bullet.6. The system of wherein the cover is clamped onto the base of the bullet.7. The system of wherein the base of the bullet comprises three or more equidistant dimples cut into the base of the bullet.8. The system of wherein the cover comprises three or more equidistant fingers that mate into each of the three or more equidistant dimples.9. The system of wherein the three or more equidistant fingers detach ...

GATED CONJUGATION LASER

The presently disclosed subject matter includes a laser system, comprising with a phase conjugation laser receiver and transmitter (PCLRT) and at least one processing unit and configured to enable simultaneous designation of multiple platforms each to a respective target. 125-. (canceled)26. A laser system , comprising:a laser illuminator;a phase conjugation laser receiver and transmitter (PCLRT), the PCLRT including a laser amplifier and a phase conjugation mirror; andat least one processing unit, the at least one processing unit is configured to obtain information in respect of one or more targets; and responsive to obtaining said information, to enable generation of a modified laser signal characterized by an average pulse repetition frequency (PRF) that is equal to a basic average PRF of a given original laser signal multiplied by at least N, N≧the number of targets; the modified laser signal including at least N pulse series; and to assign a respective pulse series to each of at least part of the N targets;wherein the laser illuminator is configured to transmit the modified signal towards the N targets;wherein the PCLRT is configured to receive a reflection of said modified signal, reflected from at least the one or more targets; said reflection including a reflection set for each given pulse in the modified laser signal; each reflection set including at least N pulse reflections, each reflected from a different target;wherein the PCLRT is further configured to perform gating for at least one reflection set, in order to allow, one pulse reflection, reflected from a given target, to be amplified by the amplifier, reflected by the phase conjugation mirror and returned in the direction of the given target.27. The laser system according to wherein the modified laser signal includes a pulse set in each PRI (pulse rate interval) of the original laser signal claim 26 , the pulse set including at least N pulses claim 26 , and wherein each pulse series is associated ...

Red dot sight

The present invention relates to a movable red dot sight comprising a fixed first light source (30) and a first reflective plate (34, 53), the light source generating a collimated first light beam that is projected onto the reflective plate (34, 53) in order to create a red dot or reticle that may be seen by the shooter via reflection from the reflective plate (34, 53), and the first beam being projected onto the reflective plate (34, 53) by way of a rotary mirror (32) the angle of inclination of which with respect to the first light beam is adjustable.

Method and device for suppressing electromagnetic background radiation in an image

The invention relates to a method and a corresponding device with which images (A, B) for the same sensing range, however in different wavelength ranges (P, N1, N2), are recorded at the same time or about the same time, and with which a signal to be detected is recorded for an image (A) serving as a P-image, and the wavelength of the signal is suppressed for an image (B) serving as an N-image. The intensity of the background in the P-image (A) is deduced from the N-image (B) while using a model for the interfering radiation or background radiation (2). The position of the signal to be detected is determined by comparing the image contents of the P-image (A) and the background image (C) derived from the N-image (B).

View-point guided weapon system and target designation method

A passive guidance system including a viewpoint capture system (VCS) including a first processor in communication with first memory and a first SWIR imager for creating a viewpoint image database having a plurality of images, at least one of the images having a target point. A weapon guidance module is in communication with the VCS and coupled to a weapon. The weapon guidance module includes a second processor in communication with second memory and a second SWIR imager for storing the viewpoint image database and correlating in-flight images from the second SWIR imager to provide guidance commands directing the weapon to the target point.

SHUTTLE DRAWING SYSTEM WITH OBSERVATION GLASS CONTROLLED BY AN AUTOMATIC TRACKING DEVICE

L'INVENTION CONCERNE UN SYSTEME DE CONDUITE DE TIR DESTINE A ETRE MONTE NOTAMMENT SUR UN HELICOPTERE. UN DISPOSITIF 20 DE POURSUITE AUTOMATIQUE DE CIBLE ET UNE LUNETTE GROSSISSANTE 10 D'OBSERVATION SONT ASSERVIS L'UN A L'AUTRE POUR QU'EN PHASE DE RECHERCHE LE DISPOSITIF DE POURSUITE SUIVE L'ORIENTATION DE LA LUNETTE ET QU'EN PHASE DE POURSUITE AUTOMATIQUE LA LUNETTE SUIVE LE DISPOSITIF DE POURSUITE. POUR LE RECALAGE DE L'ORIENTATION DE LA LUNETTE PAR RAPPORT AU DISPOSITIF DE POURSUITE, UN EMETTEUR LASER 56 PEUT EMETTRE UN FAISCEAU LASER DANS L'AXE DU DISPOSITIF DE POURSUITE; CE FAISCEAU LASER SE REFLECHIT SUR UN OBSTACLE OU UNE CIBLE ET EST RECU PAR UN DETECTEUR 54 PORTE PAR LA LUNETTE. UN CIRCUIT D'ECARTOMETRIE 52 FOURNIT DES SIGNAUX D'ERREUR REPRESENTANT LE DECALAGE DU FAISCEAU LASER RECU PAR RAPPORT AU CENTRE DU DETECTEUR 54. CES SIGNAUX D'ERREUR, ENREGISTRES DANS UNE MEMOIRE 42 EN PHASE DE RECALAGE, SONT RESTITUES ET PRIS EN COMPTE PAR UN CIRCUIT D'ASSERVISSEMENT 38, 40, 16 ENTRE LA LUNETTE ET LE DISPOSITIF DE POURSUITE, EN PHASE DE RECHERCHE DE CIBLE OU DE POURSUITE DE CIBLE. ON ELIMINE AINSI LES ERREURS DE PARALLAXE OU D'AUTRES ERREURS JOUANT SUR LES ORIENTATIONS DE LA LUNETTE ET DU DISPOSITIF DE POURSUITE. THE INVENTION CONCERNS A FIRE CONDUCT SYSTEM INTENDED TO BE MOUNTED IN PARTICULAR ON A HELICOPTER. A DEVICE 20 FOR AUTOMATIC TARGET TRACKING AND A MAGNIFICENT OBSERVATION SCOPE 10 ARE SLOWED TO ONE ANOTHER SO THAT, IN THE SEARCH PHASE, THE TRACKING DEVICE FOLLOWS THE ORIENTATION OF THE SCOPE AND THAT IN THE PURSUIT PHASE AUTOMATIC THE GLASS FOLLOWS THE PURSUIT DEVICE. FOR THE ALIGNMENT OF THE ORIENTATION OF THE SCOPE IN RELATION TO THE TRACKING DEVICE, A LASER EMITTER 56 CAN EMIT A LASER BEAM IN THE AXIS OF THE TRACKING DEVICE; THIS LASER BEAM REFLECTS ON AN OBSTACLE OR A TARGET AND IS RECEIVED BY A DETECTOR 54 CARRIED BY THE SCOPE. AN ECARTOMETRY CIRCUIT 52 PROVIDES ERROR SIGNALS REPRESENTING THE ...

Apparatus for boresighting a laser beam emitter device

A system for boresighting or aligning the optical axes of a combined infrared laser beam emitter and a low light level television telescope. An optical switch is located in the system where the axes of the telescope and the laser beam are combined, and is effective to divert at least a portion of the laser beam to a lens that focuses the beam on an opaque surface that is capable of being perforated by the laser energy. The opaque surface is backlit, so that after perforation by the laser a bright point of light can be seen in the telescope. If the axes of the laser beam and telescope are aligned, the bright spot will appear at the reticle center of the telescope. If not aligned, the axes are adjusted to produce alignment, or boresighting. The opaque surface is formed on a strip, and an automatic advancing device is operable to advance the strip to present a fresh opaque test surface, upon each boresighting operation.

Fire control system with a sighting telescope controlled by an automatic tracking device

1. A fire control comprising : - an optical device (20) for automatically tracking a target, including motors (22) for the orientation in the azimuth and elevation directions, and angular probes (28) detecting the orientation of its tracking axis (32) in the azimuth and elevation directions ; - an observation telescope (10) having a blow-up factor and being also provided with orientation motors (12) in the azimuth and elevation directions, and with the angular probes (18) detecting the orientation of its tracking axis in the azimuth and the elevation directions, characterized in that : a) the tracking device (20) bears a laser illumination means (56) emitting a laser radiation parallelly to the tracking axis (32) of said device ; b) the telescope bears a laser radiation detector (54) coupled to an associated divergence meter circuit (52) which is able to supply a couple of error signals representative for the azimuth and elevation divergence between the center of the detector (54) corresponding to the tracking axis of the telescope and the focalisation point of the laser radiation received after reflection on an obstacle ; c) a memory (42) is provided for receiving and recording these error signals in a preliminary readjustment phase during which the laser illumination means (56) emits a laser radiation ; d) an electrical circuit (38, 40, 16) is provided for receiving informations supplied by the angular probes (28, 18) of the tracking device (20) and the telescope (10) and for supplying to the orientation motors (12) of the telescope, in a phase of automatic tracking, control signals for adjusting the telescope to the azimuth and elevation movements of the tracking device, the electrical circuit (38, 40, 16) being connected during the tracking phase to the memory (42) in order to receive the error signals recorded during the readjustment phase, said electrical circuit comprising means (40) for submitting the control signals to a correction in accordance with the ...

Device for sighting, recognising and tracking a target

Fire control system with a sighting telescope controlled by an automatic tracking device

aiming device of co-axial type laser weapon system

주반사경과 부반사경을 가지는 반사망원경, 반사망원경에 결합되어 타겟을 지향하도록 광축의 각변위를 담당하는 김발조립체, 레이저광을 상기 부반사경에 조사할 수 있는 고출력 레이저 발생기, 외부에서 반사망원경을 통해 수집된 광신호 혹은 영상신호를 받는 촬상장치, 촬상장치로부터의 처리된 신호를 받아 타겟의 위치를 확인하고 반사망원경이 타겟을 정확하고 지속적으로 지향할 수 있도록 김발조립체에 구동 신호를 주는 콘트롤러를 구비하며, 반사망원경의 부반사경은 광투과성 물질로 이루어져 외부에서 주반사경으로 입사되어 부반사경을 향해 반사된 광신호 혹은 영상신호 일부가 부반사경을 투과하여 부반사경의 후방에 설치된 촬상장치로 투입되도록 이루어지는 것을 특징으로 하는 동축형 레이저무기의 조준장치가 개시된다.

Modular guided missile system

Ein Modulares Lenkflugkörpersystem mit einer Flugkörperstartanlage (10), die mit zumindest einer Lenkflugkörperstarteinrichtung (11, 12) funktional gekoppelt ist; zumindest einem mit einem Wirkmittel ausgestatteten und aus der zumindest einen Lenkflugkörperstarteinrichtung (11, 12) startbaren Lenkflugkörper (13, 14); einer Bedienerkontrolleinheit (20) zur Steuerung von Funktionen der Flugkörperstartanlage (10) und einer Zielüberwachungs- und Zielverfolgungs-Vorrichtung (30), wobei die Bedienerkontrolleinheit (20) mittels einer elektrischen oder optischen Datenübertragungsverbindung (21) oder mittels einer drahtlosen Datenübertragungsverbindung mit der Flugkörperstartanlage (10) verbunden oder verbindbar ist und/oder wobei die Zielüberwachungs- und Zielverfolgungsvorrichtung (30) mittels einer weiteren elektrischen oder optischen Datenübertragungsverbindung (33) oder mittels einer weiteren drahtlosen Datenübertragungsverbindung (36) mit der Flugkörperstartanlage (10) oder der Bedienkontrolleinheit (20) verbunden oder verbindbar ist und wobei die Zielüberwachungs- und Zielverfolgungsvorrichtung (30) an einem von der Flugkörperstartanlage und von der Bedienerkontrolleinheit (20) entfernten Standort angebracht ist. A modular missile system including a missile launch facility (10) operatively coupled to at least one missile launch facility (11, 12); at least one equipped with an active agent and from the at least one guided missile launching device (11, 12) bootable missile (13, 14); an operator control unit (20) for controlling functions of the missile launch system (10) and a target monitoring and tracking device (30), wherein the operator control unit (20) by means of an electrical or optical data transmission connection (21) or by means of a wireless data transmission connection with the missile launch system (20). 10) is connected or connectable and / or wherein the Zielüberwachungs- and target tracking device (30) by means of another electrical or optical data ...

SYSTEM FOR DESIGNATION AND / OR TARGET ILLUMINATION AND AIR RECOGNITION

COMPACT MULTIFUNCTION OPTICAL DEVICE

IMAGING INSTRUMENT FOR CONTROLLING A TARGET DESIGNATION

Un instrument d'imagerie pour contrôler une désignation de cible permet de visualiser une tache de désignation de cible (SP) au sein d'une scène (SC), tout en n'utilisant qu'un seul capteur d'image. Pour cela, un filtre est disposé sur le capteur d'image, dans une zone (ZC) restreinte de celui-ci. Le filtre permet d'augmenter un contraste et un rapport signal-sur-bruit pour une image de la tache de désignation de cible, lorsqu'un dépointage (DP) est effectué pour amener l'image de la tache de désignation de cible dans la zone du filtre. An imaging instrument for controlling a target designation allows viewing of a target designation spot (SP) within a scene (SC), while using only one image sensor. For this, a filter is arranged on the image sensor in a restricted zone (ZC) thereof. The filter makes it possible to increase a contrast and a signal-to-noise ratio for an image of the target designation spot, when a misalignment (DP) is performed to bring the image of the target designation spot into the target designation spot. filter area.

LASER OBJECTIVE DESIGNATION SYSTEM

SYSTEME PERMETTANT D'ALIGNER AVEC PRECISION L'AXE D'EMISSION LASER AVEC CELUI DU SENSEUR D'IMAGE VIDEO ABOUTISSANT AU CENTRE DE L'IMAGE BALAYEE. IL UTILISE UNE SOURCE LUMINEUSE PONCTUELLE 20 ET UNE OPTIQUE DE FOCALISATION 21 ASSOCIEE; LA RECEPTION EXTERIEURE PEUT ETRE INTERROMPUE PAR UN MIROIR DE RENVOI 22 ESCAMOTABLE. L'ECARTOMETRE 4 DU SYSTEME MESURE LES ECARTS SX, SY DE L'IMAGE DE LA SOURCE. LE SENSEUR 2 EST ENTRAINE EN ROTATION 13-14 POUR OCCUPER PLUSIEURS POSITIONS ANGULAIRES SUCCESSIVES PREDETERMINEES. UN ENSEMBLE ELECTRONIQUE 23 DE COMMANDE ET DE CALCUL DELIVRE, A PARTIR DES INFORMATIONS D'ECART SUCCESSIVES, LES SIGNAUX DE CORRECTION DX, DY DE BALAYAGE PERMETTANT D'ASSERVIR LE CENTRE DE L'IMAGE COINCIDANT AVEC LE POINT INVARIANT DE L'IMAGE CORRESPONDANT A L'AXE DE ROTATION. SYSTEM ALLOWS THE PRECISION ALIGNMENT OF THE LASER EMISSION AXIS WITH THAT OF THE VIDEO IMAGE SENSOR ENDING THE CENTER OF THE SCAN IMAGE. IT USES A PUNCTUAL LIGHT SOURCE 20 AND AN ASSOCIATED FOCUSING OPTICAL 21; THE EXTERIOR RECEPTION MAY BE INTERRUPTED BY A RETRACTABLE REFERENCE MIRROR 22. THE DEVICE 4 OF THE SYSTEM MEASURES THE SX, SY DEVIATIONS OF THE SOURCE IMAGE. SENSOR 2 IS DRIVEN IN ROTATION 13-14 TO OCCUPY SEVERAL PREDETERMINED SUCCESSIVE ANGULAR POSITIONS. AN ELECTRONIC CONTROL AND CALCULATION ASSEMBLY 23 DELIVERS, FROM SUCCESSIVE DISTRIBUTION INFORMATION, THE CORRECTION SIGNALS DX, DY OF SCAN ENABLING THE CENTER OF THE IMAGE COINCIDING WITH THE INVARIANT POINT OF THE IMAGE CORRESPONDING TO THE ROTATION AXIS.

TARGET TRACKING AND COMPENSATION SYSTEM AND METHOD FOR ATMOSPHERIC TURBULENCE

- Système et procédé de suivi d'une cible et de compensation de turbulences atmosphériques. - Le système comprend au moins deux sources lumineuses (2) émettant chacune un rayon lumineux (3) vers la cible (4), au moins deux collimateurs (6) pour collimater le rayon lumineux (3) de la source lumineuse (2) associée, un dispositif de référence (7) pour réfléchir une partie (8) du rayon lumineux (3) sortant de tous les collimateurs (6), au moins deux modules de visée (9) pour amener le rayon lumineux (3) de la source lumineuse (2) à atteindre une zone prédéterminée (10) de la cible (4), au moins deux modules de détection (11) pour recevoir et détecter la partie du rayon (8) réfléchie par le dispositif de référence (7), un module de détermination d'angle de déviation (13), un module de détermination d'écart de phase (28) et un module d'ajustement (14) pour ajuster chacune des sources lumineuse (2) pour compenser les turbulences atmosphériques. - System and method for tracking a target and compensating for atmospheric turbulence. - The system comprises at least two light sources (2) each emitting a light ray (3) towards the target (4), at least two collimators (6) for collimating the light ray (3) of the associated light source (2) , a reference device (7) for reflecting a part (8) of the light ray (3) coming out of all the collimators (6), at least two aiming modules (9) for bringing the light ray (3) from the source light (2) to reach a predetermined area (10) of the target (4), at least two detection modules (11) for receiving and detecting the part of the ray (8) reflected by the reference device (7), a deflection angle determination module (13), a phase difference determination module (28) and an adjustment module (14) for adjusting each of the light sources (2) to compensate for atmospheric turbulence.

TARGET MARKING DEVICE AND TARGET LOCATION AND TREATMENT SYSTEMS INCLUDING SUCH A DEVICE

- Dispositif de marquage de cible et systèmes de localisation et de traitement de cible comprenant un tel dispositif. - Le dispositif de marquage de cible (1) comprend un drone (2) pourvu d’au moins un émetteur (4), l’émetteur (4) comportant un élément d’activation (10) pour l’activer afin qu’il émette à un instant donné un signal (S) représentant une information de position, l’émetteur (4) étant configuré pour émettre au moins l’un des signaux suivants : un signal infrarouge, un signal lumineux, un signal sonore, un signal généré par une substance chimique, le dispositif de marquage de cible (1) faisant partie d’un système de localisation de cible (6) et/ou d’un système de traitement de cible pourvu d’un engin mobile (7). Figure pour l'abrégé : Fig. 3 - Target marking device and target location and processing systems comprising such a device. - The target marking device (1) comprises a drone (2) provided with at least one transmitter (4), the transmitter (4) comprising an activation element (10) for activating it so that it emits at a given instant a signal (S) representing position information, the emitter (4) being configured to emit at least one of the following signals: an infrared signal, a light signal, an audible signal, a generated signal by a chemical substance, the target marking device (1) forming part of a target location system (6) and/or a target processing system provided with a mobile machine (7). Figure for abstract: Fig. 3

MATRIX ECARTOMETER TASK DETECTION DEVICE.

La présente invention se situe dans le domaine des écartomètres utilisés pour la détection et la localisation de taches laser, et concerne plus précisément un détecteur de tache laser à écartomètre matriciel. Le dispositif selon l'invention comprend un circuit de lecture (ROIC) présentant une matrice de pixels (INT), une matrice de photodiodes (PH) réalisée sur un substrat unique (S), lesdites photodiodes (PH) comprenant chacune une électrode individuelle, et un dispositif de détection d'impulsion laser (D). La particularité de ce dispositif réside dans le fait que ladite matrice de photodiodes (PH) est hybridée sur ledit circuit de lecture (ROIC) par l'intermédiaire de bille (B) en matériau souple et conducteur, tel que de l'indium, mises au contact des pixels (INT) du circuit de lecture (ROIC), de sorte que ledit substrat unique (S) constitue une électrode commune à l'ensemble des photodiodes (PH) et que lesdites électrodes individuelles sont reliées auxdits pixels (INT) par lesdites billes (B).

Device for the remote identification of an optical observation instrument

Device intended to be appended to an optical search and observation instrument. It comprises means of transmitting a responding optical beam when an input beam penetrates the instrument and in the same direction as the input beam. The device can be used, in particular, for searching for weapon carriers during military operations.

COMPACT MULTIFUNCTION OPTICAL DEVICE

L'invention concerne un dispositif optique multifonctions comprenant un première source de lumière laser destinée à générer un premier faisceau lumineux, au moins une deuxième source de lumière laser destinée à générer un deuxième faisceaux lumineux de longueur d'onde distincte de celle dudit premier faisceaux lumineux et une fibre optique apte à transmettre simultanément lesdits premier et deuxième faisceaux lumineux. Selon l'invention, ladite fibre est couplée à un dispositif optique de collimation monté en sortie dudit dispositif optique multifonctions, de sorte que les rayons desdits premier et deuxième faisceaux lumineux soient parallèles en sortie dudit dispositif optique multifonctions.

Combined observation and emission device for use in pair of binoculars to point out distant object, has radiative source including sufficient emission power such that image point corresponding to emission direction of source is detected

Un dispositif combiné d'observation et d'émission (100) permet de visualiser une direction de l'émission (D ) bien que le rayonnement de ladite émission soit situé en dehors de l'intervalle spectral d'observation. Un tel dispositif permet d'éclairer à distance et sélectivement un objet dans une scène qui est observée en lumière visible, sans que le rayonnement d'émission qui produit l'éclairage soit visible à l'œil nu pour un témoin de la scène.

Method and apparatus for attenuating electromagnetic background radiation in an image.

Shooting aid device without aiming device

The aiming device comprises a laser pointer (2) attached to the barrel of the weapon, and a micro-camera (4) for locating the point of impact (6) of the laser pointer on the target (8). This camera may be mounted on the helmet (3) worn by the marksman, and its output is connected to processing circuitry for analysis of the detecting information. The results of the analysis may be displayed on a screen which is visible in front of the user's eyes on a visor (5). The laser beam may be emitted in the non-visible part of the spectrum - for example in the IR region. The resulting information is displayed in visible light wavelengths on the visor in the form of a reticule.

Patent DE3325755C2

System and method for predictive compensation of uplink laser beam atmospheric jitter for high energy laser weapon systems

A system includes a target illumination laser (TIL) configured to illuminate an airborne target with a TIL beam. The system also includes a beacon illuminator (BIL) configured to transmit a spot of illumination to an expected location on the target, wherein the spot of illumination is more focused than the TIL beam. The system also includes a camera configured to receive an image of the spot reflected off the target. The system also includes a controller configured to determine an actual location of the spot on the target based on the received image. The controller is also configured to estimate a spot motion by correlating the actual location of the spot on the target with the expected location on the target. The controller is also configured to predict uplink jitter of a high energy laser (HEL) beam generated by a HEL based on the BIL spot motion, the uplink jitter caused by atmospheric optical turbulence.

Image acquisition tool for target designation control

FIELD: image processing means. SUBSTANCE: invention relates to imaging and relates to an image acquisition tool for target designation control. Instrument comprises a lens, a matrix image sensor and a filter. Lens is configured to generate a scene image using natural radiation and aiming radiation, which is scattered by the target in reverse direction. Filter covers the limited area of the image sensor (confirmation zone) and is configured to selectively transmit to the pixel elements contained in the confirmation zone the aim radiation without natural radiation. Instrument is oriented towards the scene so that the target is displayed in the zone of confirmation of the image sensor. Target appears on the captured image only due to the visible radiation scattered in the closed direction. EFFECT: technical result consists in improvement of distance and accuracy of target designation. 12 cl, 5 dwg РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 2 735 352 C1 (51) МПК F41G 7/22 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ИЗОБРЕТЕНИЯ К ПАТЕНТУ (52) СПК F41G 7/2206 (2020.08) (21)(22) Заявка: 2020111133, 11.07.2018 (24) Дата начала отсчета срока действия патента: (73) Патентообладатель(и): САФРАН ЭЛЕКТРОНИКС ЭНД ДИФЕНС (FR) Дата регистрации: 30.10.2020 (56) Список документов, цитированных в отчете о поиске: US 4737028 A1, 12.04.1988. US 2013/ 0112879 A1, 09.05.2013. WO 2001/040733 A2, 07.06.2001. RU 167202 U1, 27.12.2016. 24.08.2017 FR 17 00873 (45) Опубликовано: 30.10.2020 Бюл. № 31 (85) Дата начала рассмотрения заявки PCT на национальной фазе: 24.03.2020 (86) Заявка PCT: 2 7 3 5 3 5 2 R U (87) Публикация заявки PCT: WO 2019/038486 (28.02.2019) Адрес для переписки: 101000, ул. Мясницкая, д. 13, стр. 5, Москва, Россия, ООО "Союзпатент" (54) ИНСТРУМЕНТ ПОЛУЧЕНИЯ ИЗОБРАЖЕНИЙ ДЛЯ КОНТРОЛЯ ЦЕЛЕУКАЗАНИЯ (57) Реферат: Изобретение относится к области получения пиксельные элементы, содержащиеся в зоне изображений и касается инструмента получения ...

Method and system for aiming a small caliber weapon

Method and apparatus for removing electromagnetic background radiation in an image

本発明は、同一視野の画像Ａと画像Ｂであって、波長範囲が一方はＰで他方はＮ１とＮ２の２範囲からなるそれぞれの画像を、同時にまたはほとんど同時に記録し、検出すべき信号の波長成分を含む画像ＡをＰ画像として記録し、該信号の波長成分を除去した画像ＢをＮ画像として記録する、背景放射除去方法及び関連する装置に関する。 Ｐ画像（Ａ）の背景信号強度を、妨害放射モデル又は背景放射モデル（２）を用いてＮ画像（Ｂ）から求める。検出すべき信号は、Ｐ画像（Ａ）の内容とＮ画像（Ｂ）から求められた背景画像（Ｃ）を比較して決定する。

Shot Planning and Smart Bullets with Active Electronics

New systems, devices and methods for extremely precise aiming and shooting of firearms are provided. In some embodiments, predicted projectile impacts may be selected and adjusted, prior to execution. In some embodiments, a device including specialized computer hardware and software aids a user in planning a shot(s), evaluating the accuracy of the planned shot(s), adjusting the location of the planned shot(s), and executing the planned shots. In some embodiments, smart bullets with on-board electronics, active aerodynamics, and wireless communications capabilities adjust a flight path of the smart bullet in-flight, to match a selected target location and/or flight path. In some embodiments, an active firearm barrel may counteract and/or otherwise adjust for any other relevant ballistic and other accuracy-impacting factors with a position-actuable firing mechanism to maintain a projected flight path of such a point of impact.

Method and defense system for combating threats

يقترح الاختراع الحالي أسلوبًا لجعل تهديد threat (2) مرئيًا بشكل أفضل لتدبير دفاعي defensive measure (3). في هذا السياق، ينبغي أن يتم تصوير التهديد (2) بشكل أكثر كثافة للتدبير الدفاعي (3). لأغراض التصوير الأكثر فعالية تتم تهيئة التهديد (2) بحيث يصدر أثر أقوى للأشعة تحت الحمراء infrared (IR) وبالتالي يكون قادرًا على البروز بشكل كافٍ إزاء الخلفية للتدبير الدفاعي (3). ينجم الأثر الأقوى للأشعة تحت الحمراء عن تسخين سطح (9) التهديد (2)، والذي يتم تحقيقه بواسطة نظام سلاح ليزري laser weapons system (7). يمكن أن يكشف التدبير الدفاعي (3) بشكل أفضل عن هذا التسخين ويتسم برأس باحث seeker head عن الأشعة تحت الحمراء من أجل هذه الغاية. شكل1 The present invention suggests a method for making a threat (2) better visible to a defensive measure (3). In this context, the threat (2) should be depicted more intensely than the defensive measure (3). For more effective imaging purposes the threat (2) is configured to emit a stronger infrared (IR) effect and thus be able to stand out sufficiently against the background for defensive measure (3). The strongest infrared effect is caused by heating the surface of the threat (9), which is achieved by the laser weapons system (7). Defensive measure (3) can better detect this heating and feature an infrared seeker head for this purpose. shape1

Pod repair unit

La présente invention concerne une unité de réparation (10) pour nacelle (11), notamment pour une nacelle de désignation laser, comprenant : - une caisse (14) transportable, - une bulle (18) fixée sur la caisse (14), la bulle (18) ayant un état replié et un état déployé, la bulle (18) comportant une ouverture (46) d'introduction d'une partie d'une nacelle (11) et au moins deux protubérances formant tube (50) de passage des mains d'un opérateur, chaque tube (50) débouchant dans la bulle (18), - un dispositif d'approvisionnement en gaz (22) propre à faire passer la bulle (18) de l'état replié à l'état déployé, - la caisse (14) et la bulle (18) délimitant un espace intérieur étanche aux contaminants extérieurs à la fois dans l'état replié et dans l'état déployé.

Aircraft payload apparatus and method

Multi-function optical system and assembly

An optical system or assembly is formed of a plurality of optical sources ( 10, 12, 14 ) and components of different laser-based equipment systems. The sources and/or components may be combined and/or eliminated to reduce complexity, cost and/or overall weight of the system by consolidating multiple laser sources into a reduced number of sources, and by multiplexing ( 19 ) different wavelength signals over common carriers. A laser engagement system ( 12, 14 ) and an infrared aim light ( 10 ) (or infrared illuminator) are powered by a single laser source which is adopted for use with conventional equipment by lengthening the duration of the coded pulses emitted by the transmitter. The transmitter may be triggered in response to the heat and/or pressure generated by the blank upon firing. A visible bore light may be eliminated by connecting infrared and/or visible aim light ( 10 ) directly to a rifle barrel. The laser engagement system and the infrared aim light (or infrared illuminator) are provided in a common housing assembly ( 410 ).

Remote control device for a target designator from an attack module, attack module and designator implementing such device

The invention relates to a remote control device from an attack module flying over a target, module of the projectile or sub-projectile, missile or attack drone type, for a target designator positioned on a terrain of operations, comprising means to emit a remote control signal that are arranged in the attack module and at least one receiver means for the remote control signal that are integral with the designator and are associated with means to activate the start-up of the designator, wherein the emitter means incorporate at least one light source oriented so as to illuminate the terrain and in that the receiver means incorporate a detector for the radiation emitted by the light source or sources.

Device and system for representing hits by shots and/or rockets and method for same

The present invention relates to a device (10) for representing hits by shots and/or rockets, a corresponding system for same and an associated method. Disclosed is a device (10) which is capable of flight and provides means (12) for optical and/or acoustic representation of hits. The device (10) and the means (12) can be remotely controlled and can be controlled from a control centre (30). For the purpose of control, the control centre (30) can locate objects capable of being located via positioning satellites (50) and control the device (10) according to the location.

Laser focusing through turbulent medium

Methods and systems for performing target-in-the-loop, real-time laser beam phase aberration compensation through a turbulent atmosphere are disclosed. The methods and systems can distinguish between phase aberration contributions from atmospheric turbulence-induced phase aberration and target-induced phase aberration caused by target surface roughness. Selected components of incoming light can be used to define a reversed wavefront and a reverse direction of propagation such that a laser beam returned to a target tends to be concentrated upon a desired region of a target. In this manner, applications such as laser target designation, tracking, pointing, active imaging, and directed energy systems are better facilitated.

Enhanced vision systems and methods

An enhanced vision system includes a first optic subsystem and a transparent photodetector subsystem disposed within a common housing. The first optic subsystem may include passive devices such as simple or compound lenses, active devices such as low-light enhancing image intensifiers, or a combination of passive and active devices. The transparent photodetector subsystem receives the visible image exiting the first optic subsystem and converts a portion of the electromagnetic energy in the visible image to a signal communicated to image analysis circuitry. On a real-time or near real-time basis, the image analysis circuitry detects and identifies structures, objects, and/or individuals in the visible image. The image analysis circuitry provides an output that includes information regarding the structure, objects, and individuals to the system user contemporaneous with the system user viewing the visible image.

Visualization device for near-IR laser designator

A tracking system (10) is for use in a weapons system (W). The tracking system is used to assist a gunner (G) in designating and tracking a target which the gunner can fire upon using a weapon under his control. A laser (12) operating at a wavelength beyond the visible band (i.e., 70.7 um) projects a laser beam (B) at the target which illuminates a portion of the target struck by the beam. The laser is boresighted with the weapon and moves with it as the gunner tracks the target. A curved window is interposed between the laser and the target. The window (16) passes a portion of the incident laser beam on it for the laser beam to strike the target. The window also reflects a portion of the laser beam. The amount of the laser beam passing through the window is substantially greater than the portion reflected. The reflected portion of the laser beam reflects at an angle (θ) with respect to the incident beam. A sensing element (26) upon which the reflected portion of the beam impinges emits a visible spot of light. The sensing element is at, or near, the focal point of the window. A visible, virtual image of the target, which is at, or near, infinity, is now created. This visible image is observable by the gunner. The gunner maintains the laser beam on the target by moving his weapon as the target moves. Movement of the laser beam produces a corresponding movement of the virtual image.

Passive boresighting system

A boresighting system including an optically pumped target member for correlating the boresight between a plurality of components such as a laser rangefinder/designator (LRF/D), a thermal imager such as a Forward Looking Infrared (FLIR) device, and a video system. The laser rangefinder is used as a reference with which to align the thermal imager and the video system. The target member and a visible source generator of the boresighting system provide multispectral capability without using any driving electronics. Both the target member and the visible source generator are located at the geometric focus of collimating optics used with the system, and, since, by definition, the geometric focus is equivalent to infinity, a point souce of radiation by the optically pumped target and the visible light generated by the visible source generator will appear to be extended sources from infinity.

Engaging targets with passive projectiles

Far field target designators

A target designation system is created by use of a dual-beam illumination bsystem of coherent light. One beam is shifted a discrete frequency level from the other beam. The beams diverge from the source until they overlap on the desired target. The difference in frequency when the beams overlap creates an interference pattern composed of moving fringes which scan across the target. Various receiver systems can be used to identify the scanning fringes and mark the target. In addition, without the use of a receiver subsystem, the illuminations subsystem can still be used as a ranging device which can be tuned to identify range to an object by adjustment of the beams until a maximum intensity moving fringe pattern is observed.

PORTABLE AND AUTONOMOUS LASER TRANSMITTER

LA PRESENTE INVENTION CONCERNE UN EMETTEUR LASER PORTABLE ET AUTONOME COMPRENANT UNE SOURCE EMETTRICE D'UN RAYON LASER, UN REDUCTEUR DE DIVERGENCE DE FAISCEAU, UNE VISEE OPTIQUE, ET UNE ALIMENTATION PORTABLE A COMMUTATIONS TEMPORAIRES. CE DISPOSITIF COMPORTE ESSENTIELLEMENT UN BATI INTERMEDIAIRE 2 DE FORME CYLINDRIQUE CONTENANT DANS UN LOGEMENT ALLONGE 15 UN EMETTEUR LASER 3, PROLONGE PAR UN REDUCTEUR DE DIVERGENCE DE FAISCEAU I. UNE VISEE OPTIQUE PAR LUNETTE 5 EST FIXEE SUR LE BATI 2 PAR UNE FIXATION REGLABLE 4. L'ENSEMBLE DE CES ELEMENTS EST FIXE MECANIQUEMENT SUR LA CROSSE 7. UNE ALIMENTATION PAR CABLAGE ELECTRIQUE 6.14 20 EST ASSUREE EN PROVENANCE D'UN SAC 9 COMPRENANT UN ACCUMULATEUR ELECTRIQUE 10, UNE ALIMENTATION ELECTRIQUE 11, UN AMPLIFICATEUR DE COURANT 12. LE CALAGE EST ASSURE PAR DE LA MOUSSE SYNTHETIQUE 16. UN INTERRUPTEUR 8 EST MONTE SUR LA CROSSE, LES FILS ETANT CONNECTES DE FACON DEMONTABLE PAR DES CONNEXIONS 13 23. APPLICATIONS AUX TELECOMMANDES, ILLUMINATIONS ET EBLOUISSEMENTS DIVERS. THE PRESENT INVENTION RELATES TO A PORTABLE AND AUTONOMOUS LASER TRANSMITTER INCLUDING A LASER BAY EMISSION SOURCE, A BEAM DIVERGENCE REDUCER, AN OPTICAL SIGHT, AND A TEMPORARY SWITCHING PORTABLE POWER SUPPLY. THIS DEVICE ESSENTIALLY INCLUDES AN INTERMEDIATE RACK 2 OF CYLINDRICAL SHAPE CONTAINING, IN AN EXTENDED HOUSING 15, A LASER EMITTER 3, EXTENDED BY A BEAM DIVERGENCE REDUCER I. AN OPTICAL SIGHT BY BEZEL 5 IS FIXED ON THE RACK 2 BY AN ADJUSTABLE FIXING 4. ALL OF THESE ELEMENTS IS MECHANICALLY FIXED ON THE CROSSETE 7. A POWER SUPPLY BY ELECTRIC WIRING 6.14 20 IS PROVIDED FROM A BAG 9 INCLUDING AN ELECTRIC ACCUMULATOR 10, AN ELECTRIC POWER SUPPLY 11, A CURRENT AMPLIFIER 12. THE CALCULATION IS PROVIDED. PROVIDED BY SYNTHETIC FOAM 16. A SWITCH 8 IS MOUNTED ON THE CROSSBODY, THE WIRES BEING REMOVABLE CONNECTIONS BY CONNECTIONS 13 23. APPLICATIONS TO REMOTE CONTROLS, LIGHTS AND VARIOUS GLOWING.

Low power laser sensing

Method and apparatus for efficiently targeting multiple re-entry vehicles with multiple kill vehicles

A method and apparatus is provided for increasing the effectiveness of destroying selected objects in a target cloud by prioritizing the objects detected in a large aperture IR detector aboard a carrier vehicle and sequentially illuminating the detected targets with coded laser radiation, followed by the launching of multiple miniature kill vehicles from the carrier vehicle, with each kill vehicle assigned to a differently-coded object in the target cloud due to the reflection back of the coded returns, thus to permit directing of individual miniature kill vehicles to a specific object in the target cloud prior to a handoff to an IR heat seeker in the miniature kill vehicle, actuated to guide the kill vehicle for a final kill.

Imaging systems and methods

An imaging method includes receiving electromagnetic radiation at a focal plane array of a handheld device. The electromagnetic radiation is processed within the handheld device, and visible images are displayed on the handheld device. The displayed visible images are indicative of a scene, and include a designator and a designator identifier when a high frequency laser pulse is in the scene. The designator and designator identifier represent the high frequency pulsed electromagnetic radiation received by the focal plane array when a high frequency pulse is present in the scene.

System for target designation and/or illumination and for air reconnaissance

L'invention concerne un système (100) de désignation et/ou d'illumination d'une cible dans une scène, qui est destiné à être fixé à un aéronef et comprend au moins une voie optique (1) équipée d'un détecteur (2) matriciel formant une image de la scène, chaque image correspondant à un champ instantané centré autour d'une ligne de visée LV, et équipée d'un dispositif de déviation de la LV à une vitesse déterminée Vd permettant d'effectuer un balayage pour assurer la fonction de désignation et d'illumination de cible. Il comporte un dispositif additionnel (3) de déviation de la LV à une vitesse Vr permettant d'effectuer un contre balayage, pour assurer en outre une fonction de reconnaissance aérienne.

Device and system for representing hits by shots and/or rockets and method for same

The present invention relates to a device (10) for representing hits by shots and/or rockets, a corresponding system for same and an associated method. Disclosed is a device (10) which is capable of flight and provides means (12) for optical and/or acoustic representation of hits. The device (10) and the means (12) can be remotely controlled and can be controlled from a control centre (30). For the purpose of control, the control centre (30) can locate objects capable of being located via positioning satellites (50) and control the device (10) according to the location.