EP2573500B1 - Unité d'entraînement de corps volant - Google Patents

Unité d'entraînement de corps volant Download PDF

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Publication number
EP2573500B1
EP2573500B1 EP12006229.4A EP12006229A EP2573500B1 EP 2573500 B1 EP2573500 B1 EP 2573500B1 EP 12006229 A EP12006229 A EP 12006229A EP 2573500 B1 EP2573500 B1 EP 2573500B1
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EP
European Patent Office
Prior art keywords
missile
training
error
computer
weapon
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.)
Active
Application number
EP12006229.4A
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German (de)
English (en)
Other versions
EP2573500A1 (fr
EP2573500B8 (fr
Inventor
Michael Grabmeier
Oliver Menn
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.)
MBDA Deutschland GmbH
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MBDA Deutschland GmbH
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Publication date
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Publication of EP2573500A1 publication Critical patent/EP2573500A1/fr
Publication of EP2573500B1 publication Critical patent/EP2573500B1/fr
Application granted granted Critical
Publication of EP2573500B8 publication Critical patent/EP2573500B8/fr
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B35/00—Testing or checking of ammunition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/001—Devices or systems for testing or checking
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/006—Guided missiles training or simulation devices

Definitions

  • the present invention relates to a missile training unit according to claim 1.
  • the invention relates to a missile training unit with a training missile forming unmanned missile and connectable to the missile configuration device for the training missile, the training missile has at least one fault memory.
  • the invention relates to such a missile training unit with a weapon control computer having a carrier aircraft, to which the training missile can be coupled.
  • Missile training units are needed and used to train the operation, handling and maintenance of a missile by the personnel involved in the mission of the missile.
  • Such training In order to be effective, such training must be oriented as closely as possible to the respective real deployment situation.
  • the ideal training from the point of view of learning efficiency would of course be the training on a sharp missile, which corresponds to 100% to a mission missile.
  • this type of training is prohibited for safety reasons. It is therefore necessary to use special training missiles for training purposes, which have hitherto often been adapted to specific training tasks.
  • such an adaptation of the missile to training tasks inevitably entails that such a missile clearly differs from a "real" missile.
  • the EP 2 253 537 A2 and their priority-giving DE 10 2009 022 007 B4 show and describe an unmanned missile intended for operational use.
  • This missile is equipped with an on-board computer running operational software stored in a program memory of the missile.
  • a test software for checking the functionality of the missile and / or its components may be stored.
  • This software is also designed to run on the on-board computer of the missile.
  • the missile can be connected to an external service device, which is responsible for checking Has required test hardware and which is controllable by running on the onboard computer of the missile test software.
  • training software for simulating errors in the missile, which is configured to run on the onboard computer of the missile and which should make it possible to train maintenance personnel on each provided with the test software unmanned missiles.
  • Object of the present invention is therefore to provide a generic missile training unit, with the different training tasks in conjunction with unmanned missiles can be trained as realistic as possible.
  • This missile training unit is provided with a training missile forming unmanned missile and connectable to the missile configuration device for the training missile, the training missile has at least one fault memory.
  • the missile training unit according to the invention is characterized in that the configuration device is designed such that simulated fault data and / or simulated fault images can be inserted into the at least one fault memory.
  • a particularly preferred development is characterized in that the training missile has a data memory and that the configuration device is designed so that a training mission software can be loaded into the data memory with it.
  • the use of training mission software makes it possible, for example, to train the effects of erroneous mission planning and the detection and correction of mission planning errors.
  • the training mission software preferably contains a check program which, when starting the training mission software, checks on the basis of the hardware present in the missile whether the missile is a training missile. This will prevent inadvertent loading of training mission software into a rogue mission vehicle, potentially triggering safety-related actions.
  • the training missile is a series-produced missile which has been disarmed in accordance with the abovementioned hardware features.
  • a likewise particularly advantageous variant of the missile training unit according to the invention additionally comprises a training aircraft having a weapon control computer to which the training missile can be coupled.
  • This missile training unit is characterized in that the training missile coupled in the state coupled to the carrier aircraft, an identification signal to the weapon control computer of the carrier aircraft, which identifies the missile as a training missile, and that the weapon control computer is designed so that a drop of the training missile prevented even then if an operational release signal (emergency emergency signal: emergency jettison) is generated during the execution of a training flight.
  • an operational release signal emergency emergency signal: emergency jettison
  • Fig. 1 is shown schematically a simplest version of a missile training unit according to the invention.
  • the dashed line symbolizes an unmanned training missile 1, which is provided on its upper side with a Umbilical Strecker 10 for electrical connection to a carrier aircraft and further comprising a Test and Load Panel (TLP) 11 with a TLP connector 12, to which in the application example shown a configuration device 2 for the training missile 1 is connected for data exchange.
  • TLP Test and Load Panel
  • the training missile 1 is equipped with a central weapon computer 14 (Central Weapon Computer CWC) and with a power supply unit 16 (PS1).
  • the power supply unit 16 is supplied via the umbilical plug 10 and / or the TLP plug 12 with electrical energy from the outside and in turn supplies the central weapon computer 14 with electrical energy.
  • the central weapon computer 14 is connected to both the umbilical connector 10 and the TLP connector 12 by data lines.
  • the central weapon computer 14 is associated with a fault memory 13.
  • simulated error data and simulated error images can be imported into the error memory 13 and stored there.
  • the in Fig. 1 is represented symbolically and the alternative to the configuration device 2 is connected to the TLP connector, carried out for training purposes tests or operating operations, the missile will respond as if the simulated and stored in the error memory 13 errors actually exist, so that the operator team their skills in terms can train on detecting and fixing simulated errors.
  • the configuration device 2 may also be provided in the service and test device 3.
  • the missile training unit shown by way of example is based on a so-called ground trainer of a missile (Ground Trainer Missile GTM or Fuel Training Missile FTM), which is usually provided without the power supply (PS1) and without the central weapons computer (CWC) to the ground personnel with respect to the purely mechanical Handling a missile to train.
  • GTM Ground Trainer Missile GTM or Fuel Training Missile FTM
  • PS1 power supply
  • CWC central weapons computer
  • the training missile 1 for the missile training unit such a ground training device GTM with the central weapon computer 14 and the power supply unit 16 and the corresponding wiring for making the electrical connections between these two units with each other and between them and the Umbilical connector 10 and the TLP connector 12 equipped.
  • the central weapon computer 14 is recorded with adapted software, the training mission software as a complete interaction of this training missile 1 via Umbilical interface 10 with a carrier aircraft and the TLP interface 12 with the configuration device and provided for ground operation external service - and Aircraft Weapon Readiness Set (AWRS) allowed, as for example from the DE 10 2009 040 304 A1 known is.
  • the training mission software uses operational mission software software objects such that the training missile at the umbilical interface 10 and at the TLP interface 12 behaves essentially like an operational serial missile.
  • this exemplary training missile It is advantageous in this exemplary training missile that existing and only training the handling of a missile ground training devices GTM can be upgraded to low acquisition and low follow-up costs by series parts from the production of operational missile to the intelligent training missile 1.
  • intelligent training missile 1 Captive Air Trainer Missile CATM
  • this intelligent training missile 1 not only the handling of the missile on the ground trainable, but it can also perform operating and test procedures on the missile, including troubleshooting, the import of mission plans and the handling be trained with the external service and testing device AWRS.
  • a simulated error message can be programmed into the memory 13 of the central weapon computer 14 by means of the configuration device via the TLP connector.
  • a faulty module and the time of the occurrence of the error and the appearance of the error are recorded in the memory 13 of the central weapon computer 14.
  • These data are then interpreted by the training mission software when training is performed, and corresponding error signals are output to the carrier aircraft via the umbilical interface 10 during training or to the service and testing device AWRS via the TLP interface 12.
  • the training staff can then Train the handling of this error and its detection on the basis of the corresponding output, for example a display in the cockpit of the carrier aircraft or an indicator on the screen of the service and test device.
  • a separate fault memory may be provided in addition to the memory 13, in which simulated fault patterns can be recorded and assigned to the central weapon computer, in which possibly during the Training flights occurring real flaws are detected in the missile. In this way, it is possible to distinguish between simulated errors and possibly occurring real errors, so that a quick and easy repair of a defective training missile after performing a training mission is possible.

Landscapes

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

Claims (6)

  1. Unité d'exercice de missile, comportant :
    un missile sans pilote formant un missile d'exercice (1) présentant un ordinateur central d'armes (14) comportant une mémoire de données, une mémoire d'erreurs (13) associée à l'ordinateur central d'armes (14), et une interface d'unité d'essai et de programmation, l'interface TLP (12), reliée par le biais de lignes de données à l'ordinateur central d'armes (14) ; et
    un moyen de configuration (2) raccordable à l'interface TLP (12) pour le missile d'exercice (1), qui est configuré de telle sorte que des données d'erreurs simulées et/ou images d'erreurs simulées avec celui-ci peuvent être enregistrées dans l'au moins une mémoire d'erreurs (13) et un logiciel de mission d'exercice dans la mémoire de données ;
    dans lequel le logiciel de mission d'exercice est configuré de manière à interpréter les données d'erreurs simulées et/ou images d'erreurs simulées enregistrées dans la mémoire d'erreurs (13) et à ordonner à l'ordinateur central d'armes (14) d'émettre un signal d'erreur correspondant vers l'interface TLP (12).
  2. Unité d'exercice de missile selon la revendication 1, caractérisée en ce que
    le logiciel de mission d'exercice comprend un programme de vérification qui vérifie, au démarrage du logiciel de mission d'exercice, à l'aide du matériel prévu dans le missile, si le missile est un missile d'exercice.
  3. Unité d'exercice de missile selon la revendication 1 ou 2, caractérisée en ce que
    le missile d'exercice (1) se distingue d'un missile de série armé au moins par les caractéristiques matérielles suivantes :
    - tous les composants pyrotechniques d'un missile de série sont désactivés ou non présents ;
    - le moyen de démarrage du réacteur du missile de série est désactivé ou non présent ; et
    - l'alimentation autonome en courant du missile de série est désactivée ou non présente.
  4. Unité d'exercice de missile selon la revendication 3, caractérisée en ce que
    le missile d'exercice est un missile de série qui est désarmé conformément aux caractéristiques matérielles selon la revendication 3.
  5. Unité d'exercice de missile selon une des revendications précédentes, dans laquelle le missile présente en outre un connecteur ombilical (10) pour la liaison électrique avec un avion porteur, le connecteur ombilical (10) étant relié à l'ordinateur central d'armes (14) par le biais de lignes de données.
  6. Système, comportant :
    une unité d'exercice de missile selon une des revendications précédentes ; et
    un avion porteur présentant un ordinateur de commande d'armes auquel le missile d'exercice peut être accouplé ; caractérisé en ce que
    le missile d'exercice transmet, dans l'état accouplé à l'avion porteur, un signal d'identification à l'ordinateur de commande d'armes de l'avion porteur qui identifie le missile en tant que missile d'exercice, et
    en ce que l'ordinateur de commande d'armes est configuré de telle sorte qu'un lancement du missile d'exercice est également empêché lorsque, lors de la mise en oeuvre d'un vol d'exercice, un signal de lancement opérationnel est généré.
EP12006229.4A 2011-09-23 2012-09-04 Unité d'entraînement de corps volant Active EP2573500B8 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE201110114225 DE102011114225B3 (de) 2011-09-23 2011-09-23 Flugkörper-Trainingseinheit

Publications (3)

Publication Number Publication Date
EP2573500A1 EP2573500A1 (fr) 2013-03-27
EP2573500B1 true EP2573500B1 (fr) 2018-11-07
EP2573500B8 EP2573500B8 (fr) 2019-01-09

Family

ID=46144965

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12006229.4A Active EP2573500B8 (fr) 2011-09-23 2012-09-04 Unité d'entraînement de corps volant

Country Status (3)

Country Link
EP (1) EP2573500B8 (fr)
DE (1) DE102011114225B3 (fr)
ES (1) ES2705753T3 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011115963B3 (de) 2011-10-13 2012-10-25 Lfk-Lenkflugkörpersysteme Gmbh Unbemannter Trainings- und Testflugkörper
DE102012012044A1 (de) 2012-06-19 2013-12-19 Eads Deutschland Gmbh Simulieren eines komplexen Systems
DE102015002563B3 (de) * 2015-02-27 2016-02-11 Mbda Deutschland Gmbh Flugkörper-Startvorrichtung
DE102015006799B4 (de) * 2015-05-27 2022-11-17 Mbda Deutschland Gmbh Testeinrichtung für eine Flugkörper-Startvorrichtung
DE102015012971A1 (de) * 2015-10-07 2017-04-13 Mbda Deutschland Gmbh Einsatzcomputersystem
CN111504142B (zh) * 2019-12-15 2022-08-19 湖北航天飞行器研究所 一种通用导弹模拟器及模拟方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5624264A (en) * 1995-09-29 1997-04-29 The United States Of America As Represented By The Secretary Of The Navy Missile launch simulator
DE102004042990B4 (de) * 2004-09-06 2008-11-20 Michael Grabmeier Verfahren und Vorrichtung zum Test eines operationellen Marschflugkörpers in verschiedenen Prüfzenarien mittels Betriebsart Wartung
DE102008054264B4 (de) * 2008-10-31 2012-09-13 Lfk-Lenkflugkörpersysteme Gmbh Multifunktionale Service- und Testeinrichtung für unbemannte Flugkörper
DE102009022007B4 (de) * 2009-05-19 2011-09-22 Lfk-Lenkflugkörpersysteme Gmbh Unbemannter Flugkörper
DE102009040304B4 (de) * 2009-09-05 2012-10-04 Lfk-Lenkflugkörpersysteme Gmbh Vorrichtung zur Steuerung von Funktionstests und/oder Serviceprozeduren für von Luftfahrzeugen absetzbare unbemannte Flugkörper

Non-Patent Citations (1)

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Title
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Also Published As

Publication number Publication date
ES2705753T3 (es) 2019-03-26
DE102011114225B3 (de) 2012-06-14
EP2573500A1 (fr) 2013-03-27
EP2573500B8 (fr) 2019-01-09

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