WO2006001856A2 - Projectile et systeme pour assurer une reconnaissance air-sol - Google Patents

Projectile et systeme pour assurer une reconnaissance air-sol Download PDF

Info

Publication number
WO2006001856A2
WO2006001856A2 PCT/US2005/008569 US2005008569W WO2006001856A2 WO 2006001856 A2 WO2006001856 A2 WO 2006001856A2 US 2005008569 W US2005008569 W US 2005008569W WO 2006001856 A2 WO2006001856 A2 WO 2006001856A2
Authority
WO
WIPO (PCT)
Prior art keywords
reconnaissance
projectile
aerial
separable section
surface area
Prior art date
Application number
PCT/US2005/008569
Other languages
English (en)
Other versions
WO2006001856A3 (fr
Inventor
Charles M. Stancil
Original Assignee
Georgia Tech Research Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Georgia Tech Research Corporation filed Critical Georgia Tech Research Corporation
Priority to US10/592,881 priority Critical patent/US20080276821A1/en
Priority to EP05788132A priority patent/EP1761431A4/fr
Publication of WO2006001856A2 publication Critical patent/WO2006001856A2/fr
Publication of WO2006001856A3 publication Critical patent/WO2006001856A3/fr
Priority to IL178135A priority patent/IL178135A0/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • F42B12/365—Projectiles transmitting information to a remote location using optical or electronic means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/02—Aiming or laying means using an independent line of sight

Definitions

  • a projectile for providing air to surface reconnaissance with a camera or other type of sensor that conveys the images or other data by a radio transmitter to a radio receiver that may be connected to a viewing screen at a remote location is provided.
  • a small infantry unit also needs up-to the minute information about the deployment of enemy units close to them.
  • a reconnaissance system is needed for a small infantry unit to view what is over the next hill or on top of or behind the next building. This reconnaissance capability needs to be controlled by the small infantry unit so that it can have a reconnaissance view immediately prior to a planned advance of the unit. All infantry units also need the capability of determining any enemy buildup that cannot be viewed from the ground level.
  • This invention provides real time reconnaissance information to small infantry units such as the squad.
  • Aerial reconnaissance pictures are provided by a camera or other sensors, such as radio frequency detectors, chemical or biological detectors, that are housed and conveyed in a projectile, such as a mortar round, deployed in the air over the battlefield.
  • the reconnaissance equipment is housed in a separable section of the projectile and separated at a control point in the air over the battlefield.
  • a parachute is provided to slow the descent of the separable section to allow the camera to take a number of pictures of the battlefield, or any other sensor to collect data, during its descent.
  • the reconnaissance equipment consists of a camera, or other type of sensor, for sensing images of the surface area or contaminates such as nuclear, chemical and biological agents.
  • a radio transmitter is connected to the sensor or camera for fransmitting images or digital data at a selected radio frequency.
  • An antenna is connected to the radio transmitter and a power source, such as a battery, is included for powering the sensor and the transmitter and any other equipment.
  • a timer can be included for timing the separation of the separable section from the rest of the projectile.
  • a remote radio receiver may be connected to a viewing screen for viewing the images or displaying data transmitted to it.
  • a number of different reconnaissance projectiles maybe used as a vehicle for the reconnaissance equipment disclosed in this invention. Among these are mortar rounds launched by an explosive propellant or gas, artillery shells, rockets and bombs. [0007] Using a mortar round as an example, the separable section can be separated by a number of different means. A simple means is to provide an explosive charge to separate the separable section. An ignition delay element can be set to detonate the charge at a specified time from the launch of the projectile. This time can be preset in manufacture or preferably set just prior to launch.
  • the descent of the reconnaissance equipment is slowed to permit a camera to take a number of photographs or other sensors collected data before reaching the surface of the earth.
  • This descent can be regulated by a parachute, which is preferably vented to control the descent and prevent the spinning of the parachute and the reconnaissance equipment.
  • the parachute and the reconnaissance equipment are housed in the separable section.
  • a drogue such as a simple aluminum plate, can be used to facilitate the parachute being deployed and filled with air.
  • a camera can be set to commence taking pictures as soon as the separable unit is separated from the rest of the projectile or it can be delayed for a few seconds.
  • the camera is preferably a CMOS on a chip. It can be either a still picture camera or a video.
  • a wide angle lens is preferably provided.
  • the image recorded by the digital camera is delivered via electronic data link to the ground as a digital stream which is processed by the receiver unit for display. Analog to digital conversion take place in the reconnaissance equipment. Once received, the scenes can then be transmitted in digital format to a receiver as normal jpeg images.
  • a power source such as a small battery, is provided to supply all the electrical power requirements for the reconnaissance equipment.
  • a miniature inertia measuring unit can be provided as a part of the reconnaissance equipment. This unit will measure the body acceleration and attitude of the separable section.
  • a microprocessor can be provided to process this information for conveying back to the remote radio receiver.
  • the reconnaissance equipment provided by this invention is capable of being placed in a regular mortar illumination round in which flare material is normally contained.
  • This aerial reconnaissance projectile can be a conventional mortar round, artillery round, or rocket.
  • a parachute or other means, such as braking fins on the reconnaissance equipment can be used to slow and control its descent over the surface to be viewed.
  • the remote radio receiver is capable of receiving radio transmissions from the radio transmitter in the reconnaissance equipment.
  • the radio receiver is usually located where, in the case of a mortar, it has a line of sight to the reconnaissance equipment during its descent.
  • This radio receiver is connected to a viewing screen, such as in a personal computer. A specially adapted hand held viewing device that has a screen can be used.
  • the trajectory model of the projectile can be stored in the personal computer or hand held video device so that the position of the view is displayed on the screen with appropriate scaling applied.
  • An on-board inertia measuring unit (IMU) can be used to improve the position estimation in respect to the view displayed on the screen.
  • the reconnaissance projectile of this invention can be used on battlefields with poor visibility conditions, such as darkness. It can be used in conjunction with an illumination mortar which can launch an illumination round over the battlefield scene to be viewed so the battlefield scene is illuminated by either visible light or IR light while the reconnaissance projectile is over the battlefield scene.
  • a reconnaissance projectile can carry other types of sensors such as a radio receiver for detecting radio frequency transmissions from the ground, and chemical, biological or nuclear sensors. This information can be processed by a microprocessor in the reconnaissance section and transmitted to a receiver on the ground for processing.
  • FIG. 1 is a perspective view of the reconnaissance equipment attached to a parachute over a scene with obstructions to visibility and radio receiver connected to a personal computer for receiving and displaying images from the reconnaissance equipment.
  • FIG. 2 is perspective view of a mortar projectile.
  • FIG. 3 is a perspective view of the mortar projectile of FIG. 2 showing its components.
  • FIG. 4 is a cross-sectional view of the reconnaissance section housed in the mortar projectile of FIG. 3.
  • FIG. 5 is a graph that shows the nominal traj ectory of a 40mm recon round with different degrees of elevation of the mortar tube.
  • FIG. 1 A perspective view of the method of this invention by which the reconnaissance equipment is used to view a scene that is obstructed from view is illustrated in FIG. 1.
  • the perspective view 10 is a view of a batttlefield scene.
  • a mortar round has just been launched from the rocket tube 38 over the battlefield scene.
  • the mortar round has been separated into a nose section 12 and a tail section 14 by a small explosion within the rocket round that cuts the pins (not shown) that hold the nose section 12 and the tail section 14 together.
  • the reconnaissance section 16 has been pulled from the rocket round and is slowly descending over the scene to be viewed 24. This descent is slowed by a parachute 18.
  • the reconnaissance section 16 has a camera 20 for viewing the battlefield scene 24 and transmitting the view by radio back to a radio receiver and computer 34 on the ground which is connected to a viewing screen 36 which can be viewed by the soldier 32.
  • the soldier 32 needs to be on a line of sight 40 with the reconnaissance section 16 in order to receive the radio waves from the transmitter in the reconnaissance section 16. While the soldier's view of the battlefield scene 24 is obstructed by hill 30, he is on a line of sight 40 with the reconnaissance section 16. [0019] Once the soldier 32 has a view of the battlefield scene 24 transmitted to him, he can accurately direct the firing of high explosive mortar round onto the battlefield scene 24.
  • the reconnaissance projectile can be used for target acquisition and fire control.
  • the mortar can fire either a reconnaissance round or a high explosive round.
  • the mortar can be operated by the soldier 32 that operates the computer and radio receiver 34 or by another soldier who operates a nearby mortar.
  • the soldier 32 can give directions to the soldier operating the nearby mortar over a radio or by voice over a telephone line. It is normally preferable that the mortar be located near the soldier 32 operating the computer and radio receiver 34, but it should be realized that they could be separated by some distance. It is obvious that the mortar needs to be located close to the battlefield scene 24 in order to fire reconnaissance rounds and armed rounds if necessary.
  • the reconnaissance information can be conveyed to an artillery battery or aircraft for firing on the battlefield scene 24 if desired.
  • This invention allows a single weapon, such as a mortar, rocket launcher, or rocket propelled grenade to conduct both reconnaissance and to fire an armed projectile on the target.
  • the mortar can be a conventional mortar or it can be a mortar where the mortar round is launched by a gas propellant.
  • the mortar tube 38 would be basically the same in both cases.
  • a perspective view of a mortar projectile is illustrated in FIG. 2. Bags of explosives can be placed between the fins 22 of the mortar projectile 42 for launching from a mortar. The fuse 44 can be set by turning to time an explosion in the nose 12 of the round for cutting shear pins holding the nose section 12 and tail section 14 together.
  • the reconnaissance section 16 is housed in the nose section 12 of the mortar round 42.
  • a parachute 18 is attached to the reconnaissance section 16 by lines 68 as shown in FIG. 1.
  • a pusher plate 46 is placed in front of the reconnaissance section 16 so that the small explosion in the nose section 12 will push the reconnaissance section 16 and parachute 18 from the nose section as shown in FIGs. 3 and 4.
  • a drogue 70 which may be a small aluminum plate, may be attached to the parachute 18 to aid in the parachute being properly deployed.
  • the parachute 18 may have a vent in the top or vents on all four sides of the parachute near the bottom of the canopy to stabilize its descent.
  • the reconnaissance section 16 has a lens assembly 50 through which images of the scene 24 being viewed are projected onto the imaging board 52.
  • This lens assembly 50 can be a single lens, such as a 4 mm f/2 lens. This lens would provide a 75° by 60° field of view which would cover 306 by 230 meter area from an altitude of 200 meters. Other types of lens can be used depending upon the reconnaissance situation.
  • the imaging board 52 is basically a CCD array. The size of this array could be 312 pixels in the horizontal direction and 287 pixels in the vertical direction with each pixel measuring 19.6 by 16 microns.
  • the camera system used can be a basic black and white still-frame.
  • a video camera arrangement can be used by the addition of a Charge Couple Device (CCD), a timing crystal and voltage regulator and a chip to supply a standard video, such as RS-170 standard video. Filters such as an infra red cut filter 66 can be used over the lens in the same way that they are used with normal cameras.
  • CCD Charge Couple Device
  • Filters such as an infra red cut filter 66 can be used over the lens in the same way that they are used with normal cameras.
  • the imaging board 52 is shown connected to a sensor board 54 which in turn is connected to a transmitter board 56 which is connected to an antenna 48.
  • the image recorded by the imaging board 52 is delivered to the sensor board 54 as an analog signal. This signal is digitized and stored in a frame buffer. Eight-bit digitization is sufficient for many applications.
  • the digital signal is delivered to the transmitter board 56 for transmission to the antenna 48 for broadcast.
  • the antenna 48 is a small omni-directional antenna.
  • the antenna may be designed to transmit on a lower UHF or a high VHF (in the range of 200 to 400 MHz). These bandwidths may offer the best combination of foliage penetration and multi-path tolerance which can be compatible with using a small antenna and low transmitter power.
  • the antenna could be a metallic slot, a shot monopole, or a short dipole.
  • the antenna could possible be integrated into the parachute itself.
  • the entire operation of the reconnaissance equipment can be controlled by a small processor housed in the reconnaissance section 16.
  • Small batteries 58 can be used to furnish the power for the reconnaissance section 16.
  • the batteries 58 can be held in place by a battery holder 64.
  • the reconnaissance section 16 may be encapsulated with an encapsulant 62.
  • the reconnaissance section 16 has a parachute attachment plate 60 to which the parachute lines 68 are attached.
  • the mortar or rocket In operation on the battlefield, the mortar or rocket is launched through a mortar tube 38 over the scene 24 to be viewed. The mortar or rocket round will be launched according to the normal trajectory for that particular weapon. The trajectory for a 40mm round is illustrated in FIG. 5.
  • the reconnaissance section 16 can be the same weight as the explosives or flare material it replaces so the weight of the mortar round is the same and the trajectory is the same. In this way the trajectory of the reconnaissance mortar round need not be recomputed.
  • the fuse 44 Prior to launching the fuse 44 is turned and set to denote the explosive in the nose section 12 at the right altitude. As illustrated in FIG.5 the time is set at 5 seconds. That time will be different depending on the trajectory and attitude of the mortar.
  • the reconnaissance section 16 of this invention can be used with other mortar sizes, such as 60 and 81mm. It could also be used with bombs and certain shoulder fired rockets and artillery. [0029] As illustrated in FIG. 1 the explosion separates the nose section 12 from the tail section 14. It also pushes the reconnaissance section 16 out of the nose section 12 by pushing the pusher plate 46. The drogue 70 pulls out the parachute 18 and ensures that it is properly deployed.
  • the reconnaissance section 16 can be designed so that the images are transmitted from the time the reconnaissance section 16 is separated from the nose section 12.
  • a processor can be used in the reconnaissance section 16 to control the operation of the camera 20 and transmitter board 56. If the height of the trajectory of the projectile is 100 meters the parachute can be designed so that the descent takes approximately 45 seconds.
  • the images are transmitted from the reconnaissance unit 16 to a computer and radio receiver 34 operated by a soldier 32 on the ground.
  • the computer and receiver 34 are connected to a viewing screen 36.
  • the computer and radio receiver 34 receives a GPS signal for displaying on the viewing screen 36. This will enable the scene 24 being viewed to be properly positioned in the landscape. This positioning can be based upon the trajectory projection as illustrated in FIG.
  • a miniature inertia measuring unit can be installed in the reconnaissance section 16 to compensate for errors in the dead-reckoning computation so that the scene 24 is properly displayed in relation to the geographical setting.
  • IMU inertia measuring unit
  • FIG. 1 While a computer is shown in FIG. 1, it should be realized that a small hand held viewing device could be used to display the imagery and indicate its origination.
  • the trajectory model of the projectile could be stored in the hand held viewing device so that the position can be estimated through dead-reckoning.
  • the trajectory of a projectile, such as a 40mm round is based upon a set of ballistic equations which starts with the elevation of the launching tube.
  • the muzzle velocity is a known quantity for various sizes of projectiles.
  • feed back from an EVIU would improve the position estimation whether a computer or hand held viewing device is used.
  • specialized software can be installed on the computer or hand held viewing device to facilitate the viewing and positioning of the battlefield scene being surveyed.
  • this system it is also possible for this system to be employed on a vehicle with the projectile being launched from the vehicle and having a receiver for a GPS system in the vehicle.
  • a transmitter may be located with the computer and radio receiver 34 to convey the information of the scene viewed to some other location for firing of artillery or air strikes. This could also be done by wire.
  • the reconnaissance equipment of this invention can be used to conduct aerial reconnaissance surveillance of a ground surface under conditions of poor visibility, such as at night time. This can be accomplished by first launching an illumination shell on a trajectory course over the surface to be viewed. A reconnaissance shell containing the reconnaissance equipment is then launched over the surface area to be viewed so that it arrive and can take pictures during the period of illumination provided by the illumination shell. Both the illumination shell and the reconnaissance shell can be launched from the same mortar or from different mortars.
  • the reconnaissance section 16 can carry a variety of other sensors either in addition to or in lieu of the camera 20.
  • the reconnaissance section may carry a chemical sensor to detect the presence of poison gas on the battlefield. This information can be conveyed from the sensor to the processor in the reconnaissance section for transmission back to the computer and radio receiver 34. This data could also be displayed on the viewing screen 36 or simply transmitted as a radio signal which the soldier 32 could hear.
  • a sensor could be installed in the reconnaissance section 16 to test for the presence of various biological agents which also could be conveyed to a processor in the reconnaissance section for transmission back to the computer and radio receiver 34.
  • a Geiger counter, or other type of radiation detector could also be included in the reconnaissance section 16 for transmission back through the computer and radio receiver 34 on the ground.
  • a radio receiver could be included in the reconnaissance section 16 to determine radio transmissions in the battlefield scene for transmission back to the computer and receiver 34.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

La présente invention a trait à un projectile de reconnaissance aérienne, tel qu'un mortier, lancé pour la visualisation d'une scène de champ de bataille. Une section de reconnaissance est libérée du projectile et retransmet des images de la scène de champ de bataille prises par une caméra et transmises par radio vers une position au sol pour la visualisation sur un écran vidéo. La section de reconnaissance peut comporter une unité de mesure inertielle en vue de déterminer sa position sur la scène de champ de bataille. Le projectile contenant l'équipement de reconnaissance peut être un obus de mortier classique ou un projectile de type fusée. Le projectile de reconnaissance aérienne est capable de transporter des capteurs pour la détection d'activité chimique, biologique ou nucléaire sur l'étendue de la surface parcourue ou pour une interception de signaux radiofréquence en provenance du sol et le transport de cette information par radio vers une position au sol avec un récepteur radio.
PCT/US2005/008569 2004-03-15 2005-03-15 Projectile et systeme pour assurer une reconnaissance air-sol WO2006001856A2 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US10/592,881 US20080276821A1 (en) 2004-03-15 2005-03-15 Projectile and System for Providing Air-to-Surface Reconnaissance
EP05788132A EP1761431A4 (fr) 2004-03-15 2005-03-15 Projectile et systeme pour assurer une reconnaissance air-sol
IL178135A IL178135A0 (en) 2004-03-15 2006-09-17 A projectile and system for providing air-to-surface reconnaissance

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US55317704P 2004-03-15 2004-03-15
US60/553,177 2004-03-15

Publications (2)

Publication Number Publication Date
WO2006001856A2 true WO2006001856A2 (fr) 2006-01-05
WO2006001856A3 WO2006001856A3 (fr) 2006-08-24

Family

ID=35782213

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/008569 WO2006001856A2 (fr) 2004-03-15 2005-03-15 Projectile et systeme pour assurer une reconnaissance air-sol

Country Status (4)

Country Link
US (1) US20080276821A1 (fr)
EP (1) EP1761431A4 (fr)
IL (1) IL178135A0 (fr)
WO (1) WO2006001856A2 (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011144497A1 (fr) * 2010-05-17 2011-11-24 Aries Ingeniería Y Sistemas S.A. Dispositif de reconnaissance aérienne télécommandé
US8263919B2 (en) 2008-08-27 2012-09-11 Raytheon Company Unmanned surveillance vehicle
RU2669690C1 (ru) * 2017-08-29 2018-10-12 Акционерное общество "Научно-производственное предприятие "Дельта" Способ коррекции стрельбы из артиллерийских орудий
RU2715466C1 (ru) * 2019-05-17 2020-02-28 Федеральное государственное бюджетное военное образовательное учреждение высшего образования "Черноморское высшее военно-морское ордена Красной Звезды училище имени П.С. Нахимова" Министерства обороны Российской Федерации Способ пристрелки цели с использованием специального реактивного снаряда
WO2021034424A2 (fr) 2019-07-12 2021-02-25 Leonardo Electronics Us Inc. Procédé et système pour l'obscurcissement et la suppression d'actifs de guerre électronique de défenses ennemies
RU215774U1 (ru) * 2022-06-29 2022-12-26 Федеральное государственное казенное военное образовательное учреждение высшего образования "ВОЕННАЯ АКАДЕМИЯ МАТЕРИАЛЬНО-ТЕХНИЧЕСКОГО ОБЕСПЕЧЕНИЯ имени генерала армии А.В. Хрулева" Министерства обороны Российской Федерации БОЕПРИПАС С СОВМЕЩЕНИЕМ РЕЖИМОВ ОБНАРУЖЕНИЯ И ПОРАЖЕНИЯ ЦЕЛИ К 82-мм МИНОМЁТУ

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9448040B2 (en) * 2010-03-22 2016-09-20 Omnitek Partners Llc Remotely guided gun-fired and mortar rounds
IL210370A (en) 2010-12-30 2015-08-31 Israel Aerospace Ind Ltd missile
US8848046B1 (en) * 2011-08-25 2014-09-30 The United States Of America As Represented By The Secretary Of The Army Kinetic energy absorber and method for gun-launched projectile
GB2498185B (en) 2012-01-03 2016-04-27 Bae Systems Plc Surveillance system
DE102012218746A1 (de) * 2012-10-15 2014-04-17 Cassidian Airborne Solutions Gmbh Waffenverbundsystem und Verfahren zur Steuerung desselben
US9513371B2 (en) * 2013-02-28 2016-12-06 Identified Technologies Corporation Ground survey and obstacle detection system
US9234728B2 (en) * 2013-11-08 2016-01-12 Lonestar Inventions, L.P. Rocket or artillery launched smart reconnaissance pod
WO2016069723A1 (fr) 2014-10-29 2016-05-06 Identified Technologies Corporation Structure et processus de fabrication d'un véhicule aérien sans pilote
US10651899B2 (en) 2016-05-26 2020-05-12 Qualcomm Incorporated System and method for beam switching and reporting
US10541741B2 (en) * 2016-05-26 2020-01-21 Qualcomm Incorporated System and method for beam switching and reporting
US10498406B2 (en) 2016-05-26 2019-12-03 Qualcomm Incorporated System and method for beam switching and reporting
US10181891B2 (en) 2016-05-26 2019-01-15 Qualcomm Incorporated System and method for beam switching and reporting
US10917158B2 (en) 2016-05-26 2021-02-09 Qualcomm Incorporated System and method for beam switching and reporting
US10742307B2 (en) * 2017-06-08 2020-08-11 Set Point Solutions, LLC Displaceable signal relay node package
CN112857224B (zh) * 2021-01-20 2022-08-30 中北大学 一种ccd线阵相机交汇连发弹丸坐标快速处理方法

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0447080A1 (fr) 1990-03-10 1991-09-18 United Kingdom Atomic Energy Authority Dispositif de reconnaissance

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2000853A6 (es) * 1986-08-08 1988-03-16 Esperanza & Cie Sa Proyectil portador para mortero
GB9015445D0 (en) * 1990-07-13 1991-02-20 Royal Ordnance Plc Projectile surveillance apparatus
US5467681A (en) * 1994-07-21 1995-11-21 The United States Of America As Represented By The Secretary Of The Army Cannon launched reconnaissance vehicle
FR2759775B1 (fr) * 1997-02-17 1999-03-05 Giat Ind Sa Munition emportant une charge utile et dispositif de collecte et transmission d'informations mettant en oeuvre une telle munition
US6392213B1 (en) * 2000-10-12 2002-05-21 The Charles Stark Draper Laboratory, Inc. Flyer assembly

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0447080A1 (fr) 1990-03-10 1991-09-18 United Kingdom Atomic Energy Authority Dispositif de reconnaissance

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8263919B2 (en) 2008-08-27 2012-09-11 Raytheon Company Unmanned surveillance vehicle
WO2011144497A1 (fr) * 2010-05-17 2011-11-24 Aries Ingeniería Y Sistemas S.A. Dispositif de reconnaissance aérienne télécommandé
RU2669690C1 (ru) * 2017-08-29 2018-10-12 Акционерное общество "Научно-производственное предприятие "Дельта" Способ коррекции стрельбы из артиллерийских орудий
RU2715466C1 (ru) * 2019-05-17 2020-02-28 Федеральное государственное бюджетное военное образовательное учреждение высшего образования "Черноморское высшее военно-морское ордена Красной Звезды училище имени П.С. Нахимова" Министерства обороны Российской Федерации Способ пристрелки цели с использованием специального реактивного снаряда
WO2021034424A2 (fr) 2019-07-12 2021-02-25 Leonardo Electronics Us Inc. Procédé et système pour l'obscurcissement et la suppression d'actifs de guerre électronique de défenses ennemies
EP3833927A4 (fr) * 2019-07-12 2022-06-08 Leonardo Electronics US Inc. Procédé et système pour l'obscurcissement et la suppression d'actifs de guerre électronique de défenses ennemies
US11802940B2 (en) 2019-07-12 2023-10-31 Leonardo Electronics Us Inc Method and system for electronic warfare obscuration and suppression of enemy defenses
RU215774U1 (ru) * 2022-06-29 2022-12-26 Федеральное государственное казенное военное образовательное учреждение высшего образования "ВОЕННАЯ АКАДЕМИЯ МАТЕРИАЛЬНО-ТЕХНИЧЕСКОГО ОБЕСПЕЧЕНИЯ имени генерала армии А.В. Хрулева" Министерства обороны Российской Федерации БОЕПРИПАС С СОВМЕЩЕНИЕМ РЕЖИМОВ ОБНАРУЖЕНИЯ И ПОРАЖЕНИЯ ЦЕЛИ К 82-мм МИНОМЁТУ
RU216613U1 (ru) * 2022-08-03 2023-02-15 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военная академия материально-технического обеспечения имени генерала армии А.В. Хрулёва" Министерства обороны Российской Федерации Артиллерийский снаряд для аэровидеоразведки

Also Published As

Publication number Publication date
EP1761431A2 (fr) 2007-03-14
US20080276821A1 (en) 2008-11-13
EP1761431A4 (fr) 2010-09-22
WO2006001856A3 (fr) 2006-08-24
IL178135A0 (en) 2006-12-31

Similar Documents

Publication Publication Date Title
US20080276821A1 (en) Projectile and System for Providing Air-to-Surface Reconnaissance
US20220163304A1 (en) Remotely Controllable Aeronautical Ordnance
EP2871438B1 (fr) Pod de reconnaissance intelligente lancé de pièces d'artillerie ou de roquette
JP2878639B2 (ja) 全局面の爆弾被害評価システム
US8263919B2 (en) Unmanned surveillance vehicle
US6933965B2 (en) Panoramic aerial imaging device
EP1573266B1 (fr) Système de reconnaissance individuel lancé par fusil
AU2023202815A1 (en) Drone-assisted systems and methods of calculating a ballistic solution for a projectile
US20040196367A1 (en) Method and apparatus for performing reconnaissance, intelligence-gathering, and surveillance over a zone
EP1794535B1 (fr) Systeme et procede de destruction d'objets volants
US20190072962A1 (en) Drone for collecting and providing image material for bomb damage assessment and air-to-ground armament system having same
EP0447080A1 (fr) Dispositif de reconnaissance
US20040066451A1 (en) Airborne delivered video surveillance system
RU2395782C1 (ru) Способ скоростной воздушной разведки
US20220139077A1 (en) Stitched image
JP5412379B2 (ja) 投射型飛翔体
WO2011144497A1 (fr) Dispositif de reconnaissance aérienne télécommandé
Hansen et al. ARGUS: real-time UAV imaging system
PL223962B1 (pl) Sposób rozpoznania terenu za pomocą pocisku

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A2

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BW BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE EG ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NA NI NO NZ OM PG PH PL PT RO RU SC SD SE SG SK SL SM SY TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW

AL Designated countries for regional patents

Kind code of ref document: A2

Designated state(s): GM KE LS MW MZ NA SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LT LU MC NL PL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

NENP Non-entry into the national phase

Ref country code: DE

WWW Wipo information: withdrawn in national office

Country of ref document: DE

WWE Wipo information: entry into national phase

Ref document number: 178135

Country of ref document: IL

WWE Wipo information: entry into national phase

Ref document number: 2005788132

Country of ref document: EP

121 Ep: the epo has been informed by wipo that ep was designated in this application
WWP Wipo information: published in national office

Ref document number: 2005788132

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 10592881

Country of ref document: US