EP2642241A1 - Überwachungssystem zum Überwachen einer Waffe, insbesondere eines Lenkflugkörpers - Google Patents

Überwachungssystem zum Überwachen einer Waffe, insbesondere eines Lenkflugkörpers Download PDF

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Publication number
EP2642241A1
EP2642241A1 EP13290058.0A EP13290058A EP2642241A1 EP 2642241 A1 EP2642241 A1 EP 2642241A1 EP 13290058 A EP13290058 A EP 13290058A EP 2642241 A1 EP2642241 A1 EP 2642241A1
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EP
European Patent Office
Prior art keywords
measuring
data
operator
weapon system
power supply
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.)
Granted
Application number
EP13290058.0A
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English (en)
French (fr)
Other versions
EP2642241B1 (de
Inventor
Pascal Massé
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 France SAS
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MBDA France SAS
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Publication of EP2642241A1 publication Critical patent/EP2642241A1/de
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Publication of EP2642241B1 publication Critical patent/EP2642241B1/de
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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
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket

Definitions

  • the present invention relates to a device for monitoring a weapon system.
  • the present invention applies more particularly to a weapon system such as a missile, whatever the type.
  • a weapon system such as a missile, whatever the type.
  • a missile is usually stored and transported in a container.
  • This monitoring device is more particularly intended to monitor the environment of the weapon system over a long period including for example storage periods and / or periods of transport and movement, to inform an operator of a risk deterioration of the weapon (missile), in particular with a view to managing a plurality of weapons or for maintenance and logistics purposes.
  • data logger devices of the "datalogger” type, which can monitor the environment of a device. These customary devices measure data, and they date and record the raw data measured. These conventional devices, however, have disadvantages. In particular, they need a large memory capacity, since they record all the data, and a large amount of energy to operate. In addition, they have a large volume, and they are not militarized to come out that they can not be used in the envisaged applications relating to a weapon system.
  • the present invention aims to overcome these disadvantages. It relates to a device for monitoring a system weapon, which can be implemented in the aforementioned military applications.
  • the measurements and the treatments carried out allow a continuous and relatively global monitoring of the environment, being able to provide an operator with information concerning this monitoring and in particular a summary information of the state of the weapon system, and this at any time.
  • the monitoring device is designed for a militarized use (with particular conditions to respect concerning the temperature (-40 ° C to + 85 ° C), the humidity (0 to 100%), the vibrations, ). Preferably, it is fixed on or in a container provided with one or more missiles.
  • said housing is also provided with a location for at least one optional electronic card, which gives it an internal expansion capacity.
  • said monitoring device comprises an activation tab which is accessible from outside the housing and which can be removed by an operator, as well as associated means which make it possible, when the activation tab is removed, to supply all the electrical elements of the device using at least one internal battery, to activate the implementation of the functions of said device.
  • This activation is irreversible until the internal battery is empty (duration which can possibly be prolonged by means of an external power supply), in order to limit the intervention capacity of an unauthorized operator, to increase the level. trusted when managing collateral and data processing (in case of power failure, the date is reset to a common reference date).
  • said power supply means comprise an internal battery, as well as means for producing an external power supply.
  • the present invention therefore provides a monitoring device having a significant autonomy (from 5 to 10 years minimum), which is compatible with military environment conditions and use of a missile, while offering a reduced cost and implementation. easy and open to extensions.
  • the present invention also relates to a weapon system, provided in particular with a missile, which comprises a monitoring device such as that mentioned above.
  • the housing of said device is attached to a missile container.
  • the shape of said housing is adapted to the shape of said missile container, which allows a varied use including mounting on existing containers already.
  • the device 1 according to the invention and schematically represented on the figure 1 is intended to monitor the environment of a weapon system (not shown), in particular a container equipped with a missile, over a long period including for example storage periods and / or periods of transport, to be able to inform a operator of a risk of deterioration of the weapon, in particular with a view to managing a plurality of weapons or for maintenance purposes.
  • a weapon system not shown
  • a container equipped with a missile over a long period including for example storage periods and / or periods of transport
  • said device 1 is autonomous and comprises, in addition, data processing means 6 which process, in real time, the data measured by said measurement means 2 and transmit at least the results of these processing to said means registration 3 for their registration.
  • said measuring means 2 comprise elements 7, 8 and 9 (specified below) for measuring parameters representative of the mechanical environment and elements 10 and 11 (also specified below) for measuring representative parameters. of the climatic environment of said device 1 and therefore of the weapon system with which it is associated.
  • said rendering means 4 allow restitution, at any time (particularly on request), recorded data and in particular the results of the treatments.
  • the measurements and the treatments carried out allow a continuous and relatively global monitoring of the environment, by making it possible to provide an operator with information concerning this surveillance and in particular a synthetic information of the state of the weapon system, and this at any time.
  • the monitoring device 1 is designed for a militarized use (with particular conditions to respect concerning the temperature (-40 ° C to + 85 ° C), the humidity (0 to 100%), the vibrations ).
  • it is attached to or in a missile container (s).
  • the shape of said housing 13 is adapted to the shape of said missile container (s), which allows a varied use including mounting it on already existing containers, the mechanical locations available on such containers can be very different , fit and size.
  • said monitoring device 1 further comprises an activation tab 17 which is accessible from outside the casing 13 (FIG. figure 2 ) and which can be removed by an operator, as well as associated means 18 which allow, when the activation tab 17 is removed, to supply all the electrical elements of the device 1 (as illustrated by a double arrow 21 on the figure 1 ) using an internal battery 19 or an external power supply 20 if present, which initiates the implementation of the various functions of the device 1.
  • an activation tab 17 which is accessible from outside the casing 13 (FIG. figure 2 ) and which can be removed by an operator, as well as associated means 18 which allow, when the activation tab 17 is removed, to supply all the electrical elements of the device 1 (as illustrated by a double arrow 21 on the figure 1 ) using an internal battery 19 or an external power supply 20 if present, which initiates the implementation of the various functions of the device 1.
  • This activation is irreversible until the end of the internal battery 19 ( duration which can possibly be prolonged by means of an external power supply 20), in order to limit the capacity of intervention of an unauthorized operator, to increase the level of confidence during the management of the guarantees and the data processing ( in the event of power failure, the date is reset to a common reference date).
  • This tab 17 is preferably red in the manner of weapons security flags.
  • the present invention therefore provides a monitoring device 1 which is autonomous (internal battery, external power supply) and which, in real time, records and processes the parameters of the environment to which it is subjected to restore them at any time. It has the ability to calculate, process, compare, date, save and retrieve data.
  • This monitoring device 1 has a range of 5 to 10 years minimum which is compatible with military environment conditions and use of a missile, while offering a reduced cost and easy implementation and open to extensions . In addition, it has a very small volume and a low cost and allows the addition of additional external means (communications, remote sensor systems, ...), as indicated below.
  • Set A aims to manage all the principles and methods of measurement, calculation, comparison, processing, evaluation, monitoring, dating, formatting, and backup of the data generated by the integrated sensors.
  • the means 6 comprise two microcontrollers 6A and 6B, one of which is provided for the management of the functions of the device 1, and the other for the management of the external communications. These microcontrollers 6A and 6B are very low consumption. It is conceivable to use a single microcontroller if it has enough computing power to handle both monitoring and communications.
  • RTC real time counters 22
  • the dating function is performed by a very low temperature compensated oscillator and a real time counter (RTC) 23 initialized at the factory and powered by the battery 19.
  • RTC real time counter
  • the internal RTC counters 22 are initialized, following the extraction of the activation tab 17, by reading the common RTC counter 23. Before the extraction of the activation tab 17, the microcontrollers 6A and 6B are not powered. . The date and time are available in the common metric RTC 23 of high precision and very low consumption, which uses the internal battery 19 from the factory. The RTC counters 22 of the microcontrollers 6A and 6B are, after activation, synchronized regularly on this common RTC counter 23.
  • FRAM memory consumes little, is nonvolatile, and allows access to infinity without a complex access protocol, but it is limited in memory size. It is used for repeated access to the same addresses, such as programming parameters, identifiers, and user information. As it is non-volatile, it ensures to keep all data in case of power loss.
  • FLASH memory consumes a lot more power, is nonvolatile, and offers more memory capacity, but it requires a slower and much more complex page registration process.
  • Set B aims to manage external means of communication. These means comprise at least one USB link, and a communication bus to external optional modules.
  • this set B comprises a backup memory 25, external modules 26 and an optional internal card 27.
  • the optional internal card 27 is envisaged to add one or more low-power wireless communication means or geolocation.
  • This optional internal card 27 can also be used for additional internal sensors with a measure of salinity, brightness, radio frequency level, sound level, chemical composition.
  • An appropriate location is provided in the housing 13 for this optional internal card 27.
  • the external modules 26 are optional modules to add as needed. These modules 26 are either complementary sensor or detection systems, or short or long-range communication modules. These modules can communicate with each other for the purpose of transmitting and obtaining data.
  • the memory space is shared via configuration parameters accessible to the operator.
  • a function 28 serves to separate an I 2 C link from the external modules and to adapt the level of the communication lines of the I 2 C bus to the voltage level of this link.
  • Plugins use their own power and may want to master the level high of this communication voltage. The device allows this link only if needed.
  • the high voltage level of the communication lines can be equal to or independent of the power level of the device.
  • a ground station 29 must accept wired USB communications. It allows you to configure device 1 (parameters, identifiers), to record the material tracking data by the operator, to download all or part of the recorded data, to carry out tests and / or calibrations at the factory level or end user level.
  • the ground station 29 supplies the device via the USB line 30 during the time of connection.
  • the USB power supply replaces the internal battery 19 and the external power supply 20.
  • Set C aims to manage power modes.
  • the device 1 thus has an internal battery 19, and it can also be powered by an external power supply 20 (battery (s) or other usual power supply means) or by a USB link 30.
  • an external power supply 20 battery (s) or other usual power supply means
  • a USB link 30 a USB link
  • the battery (non-rechargeable) 19 is, for example, LiSOCl2 type and supports the temperature range (-60 ° C to + 90 ° C), shock, vibration, and altitude considered. It has a great energy capacity.
  • the device 1 is powered by PC.
  • the internal battery 19 and the external power supply 20 are no longer requested as long as the USB link is present.
  • the device 1 is delivered programmed (date, time, parameters), and only its basic functions (date, time) are active.
  • the final operator is responsible for activating the operational phase of the device by activating the general power supply by extracting the activation tab 17. From this moment, all the functions have access to the main power supply which is at least distributed by the internal battery 19 or the external power supply 20 if present.
  • part D non-leakproof area 15 of the figure 1 to be able to perform their functions
  • the climatic sensors pressure and humidity
  • the temperature sensor 10 is also placed in this zone.
  • a second internal temperature sensor (not shown) is present in the sealed zone 14 for purposes of self-test and degraded mode operation if the main sensor were to be used. declared out of service, temperature being the minimum factor that must be measured.
  • HMI hypervisorid zone

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
  • Radar Systems Or Details Thereof (AREA)
EP13290058.0A 2012-03-22 2013-03-14 Überwachungssystem zum Überwachen einer Waffe, insbesondere eines Lenkflugkörpers Active EP2642241B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1200866A FR2988469B1 (fr) 2012-03-22 2012-03-22 Dispositif de surveillance d'un systeme d'arme, en particulier de type missile

Publications (2)

Publication Number Publication Date
EP2642241A1 true EP2642241A1 (de) 2013-09-25
EP2642241B1 EP2642241B1 (de) 2019-06-05

Family

ID=46852049

Family Applications (1)

Application Number Title Priority Date Filing Date
EP13290058.0A Active EP2642241B1 (de) 2012-03-22 2013-03-14 Überwachungssystem zum Überwachen einer Waffe, insbesondere eines Lenkflugkörpers

Country Status (6)

Country Link
EP (1) EP2642241B1 (de)
ES (1) ES2743724T3 (de)
FR (1) FR2988469B1 (de)
IL (1) IL234611B (de)
IN (1) IN2014DN08001A (de)
WO (1) WO2013140050A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2589221C1 (ru) * 2015-04-21 2016-07-10 Открытое акционерное общество "Акционерная Компания "Туламашзавод" Способ климатических испытаний выключателей с пружинным приводом и стенд для его осуществления

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0305285A1 (de) * 1987-08-28 1989-03-01 Thomson-Brandt Armements Armiergerät mit Sicherheitsvorrichtung für ein von einem Träger abgeworfenes Projektil
US20030058130A1 (en) * 2001-09-26 2003-03-27 Leslie Kramer Remote monitoring of munition assets
US20070067138A1 (en) * 2005-09-21 2007-03-22 Rabin Daniel A Self-contained, non-intrusive data acquisition in ammunition
EP1992904A2 (de) * 2007-05-15 2008-11-19 LFK-Lenkflugkörpersysteme GmbH Verfahren zur Zustandsüberwachung einer intelligenten Waffe und intelligente Waffe

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4576172A (en) * 1982-05-26 1986-03-18 Bentall Richard Hugh Cameron Switched electrical apparatus for medical use
CN102895735B (zh) * 2004-12-27 2015-12-16 皇家飞利浦电子股份有限公司 预置自动外部除纤颤器以便使用的方法
TWM358504U (en) * 2008-12-16 2009-06-01 Microelectronics Tech Inc Shielding apparatus for transceiver

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0305285A1 (de) * 1987-08-28 1989-03-01 Thomson-Brandt Armements Armiergerät mit Sicherheitsvorrichtung für ein von einem Träger abgeworfenes Projektil
US20030058130A1 (en) * 2001-09-26 2003-03-27 Leslie Kramer Remote monitoring of munition assets
US20070067138A1 (en) * 2005-09-21 2007-03-22 Rabin Daniel A Self-contained, non-intrusive data acquisition in ammunition
EP1992904A2 (de) * 2007-05-15 2008-11-19 LFK-Lenkflugkörpersysteme GmbH Verfahren zur Zustandsüberwachung einer intelligenten Waffe und intelligente Waffe

Also Published As

Publication number Publication date
FR2988469A1 (fr) 2013-09-27
IN2014DN08001A (de) 2015-05-01
WO2013140050A8 (fr) 2014-10-30
FR2988469B1 (fr) 2015-01-02
ES2743724T3 (es) 2020-02-20
WO2013140050A1 (fr) 2013-09-26
EP2642241B1 (de) 2019-06-05
IL234611B (en) 2018-11-29

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