EP0800052B1 - Système de reconnaissance - Google Patents

Système de reconnaissance Download PDF

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Publication number
EP0800052B1
EP0800052B1 EP97104932A EP97104932A EP0800052B1 EP 0800052 B1 EP0800052 B1 EP 0800052B1 EP 97104932 A EP97104932 A EP 97104932A EP 97104932 A EP97104932 A EP 97104932A EP 0800052 B1 EP0800052 B1 EP 0800052B1
Authority
EP
European Patent Office
Prior art keywords
reconnaissance
buoyancy
reconnaissance device
facility
paraglider
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP97104932A
Other languages
German (de)
English (en)
Other versions
EP0800052A2 (fr
EP0800052A3 (fr
Inventor
Ulrich Dr. Schleicher
Joseph H. Prof. Dr. Spurk
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Diehl Stiftung and Co KG
Original Assignee
Diehl Stiftung and Co KG
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 Diehl Stiftung and Co KG filed Critical Diehl Stiftung and Co KG
Publication of EP0800052A2 publication Critical patent/EP0800052A2/fr
Publication of EP0800052A3 publication Critical patent/EP0800052A3/fr
Application granted granted Critical
Publication of EP0800052B1 publication Critical patent/EP0800052B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/56—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding of parachute or paraglider type

Definitions

  • the invention relates to a reconnaissance device according to the preamble of claim 1.
  • Reconnaissance facilities are known as so-called Known drones. These drones are small remote-controlled aircraft. These aircraft require a corresponding production effort. Also are such aircraft are relatively easy to combat. For example, such drones in DE-Z "Armada International "5/95, page 70.
  • EP 0 466 499 A1 is an artillery projectile with a target seeker Submunition known.
  • An ejection unit causes the ejection of the Submunition, with a swirl device and a brake screen for the Stabilization of the submunition ensures.
  • a long-term education is due to the relatively short fall time.
  • the invention has for its object a Reconnaissance facility of the type mentioned at the beginning create that is simple, that in a simple way and with simple means to a corresponding one Observation height is reasonable, which is a relative long-term clarification in the order of up to 10 minutes allowed, and which is quasi insensitive to control.
  • the reconnaissance device is with the help a carrier or artillery projectile in the target area spent and there at a suitable height by means of a Timer or the like from the artillery storey pushed out.
  • the Swirl device the speed and with the help of Brake parachute the airspeed of the Reconnaissance facility slowed down.
  • the buoyancy device activated the buoyancy device.
  • the buoyancy device is suitable for the Reconnaissance facility up to 10 minutes in size to hold over a target or along a desired one To move trajectory over the target area.
  • the reconnaissance device thus forms a optimal replacement of a so-called advanced Observer. It is advantageously possible the coordinates of corresponding targets with the help of a fixed coordinate system to measure. To this The coordinates and orientation of the Reconnaissance facility using a GPS receiver, with Using a gravity sensor, using a Height measurement sensor or the like can be determined. With the sensor unit of the invention Reconnaissance information, for example in the form of TV pictures, can be on-line or be evaluated via video.
  • the reconnaissance device according to the invention has the advantages of a reliable, reliable mode of operation, simple handling and simple logistics.
  • the reconnaissance device according to the invention can advantageously be designed to be compatible with imported weapon and fire control systems without any problems.
  • the electronic assemblies used in the reconnaissance device according to the invention for the sensor unit, for the transmitter for data transmission to a fire control center, for the receiver for receiving steering data, the GPS receiver, the computer for image evaluation of the sensor unit, etc. are commercially available and need only be slightly modified if necessary, there is the further advantage of a correspondingly inexpensive feasibility of the reconnaissance device according to the invention.
  • the mechanical components of the reconnaissance device according to the invention such as the steering device and in particular the buoyancy device, which is advantageously designed as a paraglider.
  • the buoyancy body can also be designed as a kite, for example.
  • a kite for example, has an area of the order of 1 m 2 and a paraglider, for example, has a buoyancy area of the order of 2.5 m 2 if such a buoyant body is to be used to transport a payload mass of approximately 10 kg with a correspondingly low sinking speed.
  • a kite and a paraglider of the area dimensions mentioned can be stowed easily in a corresponding artillery storey.
  • a float in the form of a paraglider has the advantages of a smaller packing volume and a simpler construction.
  • a kite has the advantages of better aerodynamics, it flies longer and faster.
  • Common to a paraglider and a kite as a buoyancy body of the reconnaissance device according to the invention is the advantage of low technical complexity.
  • This security against shelling is particularly due to this ensures that the projected area of the Buoyancy device is relatively small, both for the Training the buoyancy device as a paraglider or Kite or hot air balloon, or because small Holes in the preferably made of a textile material existing buoyancy device does not crash the same bring about and / or the reconnaissance facility fighting projectiles with a detonator through the Do not respond to the buoyancy device and / or the Missile fighting projectiles with Timers cannot be used because of the respective exact target distance is not detectable.
  • Figure 1 shows an artillery projectile 10 with a housing 12, to the front of which is connected a projectile casing 14 and completed on the back by a floor 16 is.
  • a projectile casing 14 At the top of the shell 14 is an igniter 18th and inside the shell 14 is an ejection unit 20 arranged with an exhaust hood 22.
  • a reconnaissance facility 24 is located in artillery storey 10 arranged, which is connected to a buoyancy device 26 is.
  • the buoyancy device 26 is, for example, as Kite or preferably designed as a paraglider.
  • Figure 1 is the buoyancy device 26 schematically in indicated their space-saving folded state of rest.
  • FIG. 2 shows the buoyancy device 26 in her from the artillery storey (see Figure 1) released active state with the at the Buoyancy device 26 hanging by means of suspension lines 28 Reconnaissance facility 24.
  • the reconnaissance device 24 has a Sensor unit 30 for detecting and locating Aim a transmitter 32 for data transmission to a Fire control center (not shown), a computer 34 for Image evaluation of the sensor unit 30 and one Steering device 36, which for controlled steering of the Buoyancy device 26 is provided in its active state is.
  • the computer 34 is equipped with a for data compression Data compression device 38 is formed.
  • the Steering device 36 is connected to a receiver 40, the one for receiving steering data for the steering device 36 is provided.
  • a GPS receiver 42 is provided to determine the device-fixed Coordination system.
  • a drive device 44 serves for an extension of the observation period by at least partially Compensation of the flow resistance and consequently one Reduction of the sink rate and through compensation a possible cross wind and therefore a lower one To accomplish drift.
  • This drive device 44 can, for example, a slowly burning rocket or have a series connection of such rockets.
  • the Floor 16 separated and a floor brake cloth opened, to brake the floor 10.
  • the Ejection unit 20 from artillery storey 10 pulled out and using a brake screen and a Swirl device, not shown in the drawing are slowed down to a certain flight speed and untwisted.
  • the buoyancy device 26 from the space-saving resting position in the active state set up, support tube shell elements 48 (see FIG. 1) separated and discarded become.
  • FIG. 2 illustrates that on the buoyancy device 26 in Reconnaissance facility hanging from a paraglider 24.
  • the paraglider has an upper sail 48 and Bottom sail 50, which laterally ends in stabilizers 52, and divided into individual cells 56 by cell walls 54 are.
  • Each cell 56 has an upstream side Compensation opening 58 formed.
  • the fishing lines 28 are grouped into two groups, the are each provided with a rope lock 60.
  • the Reconnaissance device 24 is with the two Catch line locks 60 connected by means of risers 62.

Claims (8)

  1. Dispositif de reconnaissance comportant une unité à capteurs pour détecter et localiser des objectifs, qui peut être transporté dans un projectile d'artillerie et largué de celui-ci, en même temps qu'un dispositif déployable retardant la chute et qui est pourvu d'un parachute de freinage et d'un dispositif anti-giratoire, caractérisé en ce que le dispositif retardant la chute est un dispositif de sustentation (26) qui, pour le déplacement ciblé et pour accroítre la durée de séjour au-dessus de la région d'intervention de l'unité de reconnaissance (24), comporte un dispositif de guidage (36) et un dispositif de propulsion (44).
  2. Dispositif de reconnaissance selon la revendication 1, caractérisé en ce que le dispositif de sustentation (26) est conformé en parachute planant.
  3. Dispositif de reconnaissance selon la revendication 1, caractérisé en ce que le dispositif de sustentation (26) est conformé en cerf-volant.
  4. Dispositif de reconnaissance selon la revendication 1, caractérisé en ce qu'un émetteur (32) est prévu pour la transmission des données à un poste de conduite de tir.
  5. Dispositif de reconnaissance selon l'une des revendications 1 à 4, caractérisé en ce que le dispositif de sustentation (26) comporte un récepteur (40) pour recevoir des données de guidage destinées au dispositif de guidage (36) du dispositif de sustentation (26).
  6. Dispositif de reconnaissance selon l'une des revendications 1 à 5, caractérisé en ce qu'il est prévu un récepteur GPS (42).
  7. Dispositif de reconnaissance selon l'une des revendications 1 à 6, caractérisé en ce qu'un ordinateur (34) est prévu pour l'interprétation des images de l'unité à capteurs (30).
  8. Dispositif de reconnaissance selon la revendication 7, caractérisé en ce que l'ordinateur (34) comporte un dispositif de compression de données (38).
EP97104932A 1996-04-04 1997-03-22 Système de reconnaissance Expired - Lifetime EP0800052B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19613492A DE19613492C2 (de) 1996-04-04 1996-04-04 Aufklärungseinrichtung
DE19613492 1996-04-04

Publications (3)

Publication Number Publication Date
EP0800052A2 EP0800052A2 (fr) 1997-10-08
EP0800052A3 EP0800052A3 (fr) 1998-10-28
EP0800052B1 true EP0800052B1 (fr) 2002-09-18

Family

ID=7790463

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97104932A Expired - Lifetime EP0800052B1 (fr) 1996-04-04 1997-03-22 Système de reconnaissance

Country Status (2)

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EP (1) EP0800052B1 (fr)
DE (2) DE19613492C2 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3995776A1 (fr) 2020-11-10 2022-05-11 Diehl Defence GmbH & Co. KG Dispositif actionneur permettant de combattre une cible au moyen des impulsions électromagnétiques, système de dispositif actionneur, dispositif porteur et procédé de fonctionnement d'un dispositif actionneur

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7109598B2 (en) * 2001-11-07 2006-09-19 Bryan William Roberts Precisely controlled flying electric generators III
DE10238019A1 (de) * 2002-08-20 2004-03-11 Diehl Munitionssysteme Gmbh & Co. Kg Verfahren und Vorrichtung zur Echtzeit-Geländeaufklärung
DE10238717A1 (de) 2002-08-23 2004-03-04 Diehl Munitionssysteme Gmbh & Co. Kg Aufklärungseinrichtung
DE10251118A1 (de) 2002-11-02 2004-05-19 Diehl Munitionssysteme Gmbh & Co. Kg Aufklärungseinrichtung
DE202004010194U1 (de) * 2004-06-30 2005-11-24 Diehl Bgt Defence Gmbh & Co. Kg Gefechtskopf für Artilleriemunition
DE102005043078B4 (de) * 2005-09-10 2007-06-14 Diehl Bgt Defence Gmbh & Co. Kg Suchzündermunition
US8263919B2 (en) * 2008-08-27 2012-09-11 Raytheon Company Unmanned surveillance vehicle
DE102008050377B4 (de) * 2008-10-02 2013-11-07 Mbda Deutschland Gmbh Vorrichtung zur Vergrößerung des Aufklärungsradius' einer Basis
GB2498185B (en) 2012-01-03 2016-04-27 Bae Systems Plc Surveillance system
GB2586820B (en) * 2019-09-04 2023-12-20 Bae Systems Plc A munition and munition assembly

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE64209C (fr) *
DE3516673A1 (de) * 1985-05-09 1986-11-13 Diehl GmbH & Co, 8500 Nürnberg Endphasen-korrigierbare suchzuender-munition und verfahren zum bekaempfen gepanzerter zielobjekte
DE3618777A1 (de) * 1986-06-04 1987-12-10 Messerschmitt Boelkow Blohm Detonationsmelder
FR2656082A1 (fr) * 1989-12-15 1991-06-21 Thomson Brandt Armements Systeme deployable pour l'emport et la sustentation d'une munition.
GB9015445D0 (en) * 1990-07-13 1991-02-20 Royal Ordnance Plc Projectile surveillance apparatus
DE4104800C2 (de) * 1991-02-16 1998-07-02 Diehl Stiftung & Co Einrichtung zur Echtzeit-Geländeaufklärung
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3995776A1 (fr) 2020-11-10 2022-05-11 Diehl Defence GmbH & Co. KG Dispositif actionneur permettant de combattre une cible au moyen des impulsions électromagnétiques, système de dispositif actionneur, dispositif porteur et procédé de fonctionnement d'un dispositif actionneur
DE102020006889A1 (de) 2020-11-10 2022-05-12 Diehl Defence Gmbh & Co. Kg Wirkvorrichtung zum Bekämpfen eines Ziels mittels elektromagnetischer Impulse, Wirkvorrichtungssystem, Trägereinrichtung und Verfahren zum Betreiben einer Wirkvorrichtung

Also Published As

Publication number Publication date
DE19613492A1 (de) 1997-10-09
DE59708224D1 (de) 2002-10-24
DE19613492C2 (de) 2001-10-04
EP0800052A2 (fr) 1997-10-08
EP0800052A3 (fr) 1998-10-28

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