[go: up one dir, main page]

WO2014060189A1 - Système interarmes et procédé de commande dudit système - Google Patents

Système interarmes et procédé de commande dudit système Download PDF

Info

Publication number
WO2014060189A1
WO2014060189A1 PCT/EP2013/069690 EP2013069690W WO2014060189A1 WO 2014060189 A1 WO2014060189 A1 WO 2014060189A1 EP 2013069690 W EP2013069690 W EP 2013069690W WO 2014060189 A1 WO2014060189 A1 WO 2014060189A1
Authority
WO
WIPO (PCT)
Prior art keywords
composite
active
control
observation
data
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.)
Ceased
Application number
PCT/EP2013/069690
Other languages
German (de)
English (en)
Inventor
Philipp GLÖSMANN
Boris Trouvain
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.)
Airbus DS Airborne Solutions GmbH
Original Assignee
Airbus DS Airborne Solutions GmbH
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 Airbus DS Airborne Solutions GmbH filed Critical Airbus DS Airborne Solutions GmbH
Priority to EP13773650.0A priority Critical patent/EP2906899A1/fr
Publication of WO2014060189A1 publication Critical patent/WO2014060189A1/fr
Priority to IL238035A priority patent/IL238035A0/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G3/00Aiming or laying means
    • F41G3/04Aiming or laying means for dispersing fire from a battery ; for controlling spread of shots; for coordinating fire from spaced weapons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30Command link guidance systems
    • F41G7/301Details
    • F41G7/303Sighting or tracking devices especially provided for simultaneous observation of the target and of the missile
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G9/00Systems for controlling missiles or projectiles, not provided for elsewhere
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0011Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
    • G05D1/0038Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement by providing the operator with simple or augmented images from one or more cameras located onboard the vehicle, e.g. tele-operation

Definitions

  • the present invention relates to a weapons composite system and a method for controlling a weapons composite system.
  • Observation systems can be stationary or mobile, such as drones or KZOs (small aircraft targeting). They include an observer, such as an unmanned aerial vehicle (UAV), and an observer control station that controls the observer. The observer may also perform the function of a target commander marking a target, for example by means of a laser designator.
  • Effective systems are systems that have a military effect on a target. Examples of active systems are loiterable ammunition and end-phase-guided ammunition, but also armed manned or unmanned aerial vehicles.
  • An action system includes a caster and an activity control station that controls the caster.
  • Both the observing and acting systems have the ability to transmit data to, for example, their condition (self-position, self-location, sensor data, sub-data, and the like), as well as, where appropriate, target location data with systemic latency to a suitable receiving device a corresponding system can be monitored.
  • Both the observational and the acting systems have a direct (for example radio) or indirect (for example by means of a laser designator) ability to influence with a given latency on their actions (such as in particular their navigation), so to lead.
  • a last possible time for the termination of the use of an active system should be delayed as far as possible.
  • the interference with the effect taking into account the latest situation information with the aim of avoiding collateral damage is in the foreground.
  • the basis of the present invention is to create an instance that has both the decision-relevant information of the participating observation and active systems with minimal latency and also the instruction of an active system with minimum latency is feasible. This gives the operator the maximum decision time to manage the operation of an agent so that the likelihood of collateral damage can be reduced to the technically possible minimum.
  • the present invention comprises a weapon composite system comprising at least one observation system with an observation system control station, at least one active system with an active system control station and a compound control system connected to the control stations of the observation and active systems.
  • the compound control system comprises a computing unit and a display device, which are adapted to receive data from the Display control stations of the observation and action systems and display at least one input field for instructions to the control center of an active system.
  • a compound system interface computer data from both an observation system and an active system can be simultaneously detected and evaluated by an operator.
  • the operator thus has access to target information, such as electro-optical and / or infrared real-time images, sensor target information such as radar or acoustic intensity diagrams, position, behavior, signature or environment, of all systems involved.
  • the composite control system is preferably set up to display a subset of the data that can be provided by the control stations of the observation and active systems on the display device. This corresponds to a filtering of the available data. Thus, not all available data is displayed, but in particular only the decision-relevant data, which simplifies the detection of the situation by the operator.
  • the filtering of the data occurs in the data providing system prior to transmission to the compound control system, upon receipt in the compound control system or as a combination thereof.
  • the compound control system is adapted to display input fields for a subset of the instructions executable by an active system control station on the display device. Thus, a reduced amount of instructions can be transmitted to the active system control station via the compound control system.
  • the subset of the data and / or the instructions is determined on the basis of criteria stored in a database.
  • the database includes a plurality of criteria records, wherein an appropriate criteria record is retrieved from the database and used to filter the data and / or available instructions.
  • the subset of the data and / or instructions is determined on the basis of at least one of the type of an observation system, the type of an active system or the deployment scenario of the weapon composite system.
  • a rule can be specified for the determination of the subset of the data and / or instructions.
  • the abovementioned parameters are used to search for an associated criterion data record in the database.
  • the compound control system has an interface for establishing a data connection to a guidance system, wherein the composite control system is adapted to display data from the guidance system on the display device.
  • the guidance system which may be, for example, a fire control system, commands the use of the weapons composite system and, for example, gives clearance for the use of an active system.
  • the compound control system indicates in particular on its display device whether the release has been issued or the application is to be terminated.
  • an observation system has a work station container housing its control station and an active system has a work station container housing its control station.
  • a workstation container which can also be mobile, contains at least one workstation for an operator of the corresponding observation or active system.
  • the Verbundkontrolisystem two arithmetic units and two display devices, wherein in each of the two workstation an arithmetic unit and a display device are housed.
  • the composite system interface computer is thus divided into two workplaces, which are arranged in the respective workstation containers of the observation and active systems involved.
  • the compound control system is configured to display on the display device at least one input field for instructions to the control station of an observation system.
  • an observation system can be at least partially controlled by the compound control system.
  • input fields for a subset of the instructions executable by the observation system are displayed on the display device. The determination of the subset takes place in an advantageous manner as described above for the instructions for the active system.
  • the compound control system is set up to display on the display device the latest possible time for canceling the use of an active system.
  • the latest possible time is calculated from at least one of the latency of the communication of the compound control system with the knitter, the properties of the knitter and the application scenario of the knitter.
  • the compound control system is adapted to display a Eingefeid an order to cancel the use of an active system. This allows an operator of the compound control system to directly command the use of the active system.
  • the Verbundkontrolisystem is set up to display on the display device a map with the positions of the knitter, the observer and any goals and / or the situation situation.
  • the compound control system when the compound control system is set up to perform a function, this means that the arithmetic unit of the compound control system is set up to perform the function or is arranged to instruct the performance of the function.
  • the present invention further relates to a method for controlling a weapon composite system comprising at least one observation system with an observation system control station, at least one active system with an active system control station and a compound control system connected to the control stations of the observation and active systems, wherein the composite control system comprises a computing unit and a Display device, wherein on the display device data from the control stations of the observation and active systems and at least one input field for instructions to the control station of an active system are displayed.
  • a subset of the data that can be provided by the monitoring stations of the monitoring and active systems is displayed on the display device.
  • the subset of the data is determined, for example, based on criteria stored in a database.
  • the subset of the data is determined on the basis of at least one of the type of an observation system, the type of an active system or the deployment scenario of the weapon composite system.
  • the latest possible time for canceling the use of an active system is displayed on the display device.
  • Figure 1 is a schematic representation of an inventive
  • Figure 2 is an exemplary screen display on a
  • FIG. 1 schematically shows the structure of a weapons composite system 1 which contains a composite control system 2, an observation system 3 and an active system 4.
  • the composite control system 2 and thus the weapon composite system 1 is connected to a guide system 5.
  • the weapon composite system 1 is used in a scenario to enlighten and combat at least one target, so to perform an operation.
  • the observation system 3 consists of an observer 32, for example an unmanned mounting drone, and an observation system control station 31, between which a wireless, bi-directional data connection exists.
  • the observation system control station 31 controls the observer 32. This sends sensor data and telemetry data to the observation system control station 31.
  • the observation system serves to capture information about the target, that is, to clarify the goal.
  • the active system 4 consists of a kneader 42, for example loiter-capable or end-phase-controlled ammunition, and an active-system control station 41, between which there is a wireless, bidirectional data connection.
  • the control system control station 41 controls the kneader 42, which is also referred to as active agent, in particular with regard to the navigation and the triggering of the effect.
  • the knitter 42 sends sensor data and telemetry data to the active system control station 41.
  • the action system serves to combat the target.
  • the observer 32 and the creater 42 are also referred to as unmanned aerial vehicles (UAVs).
  • the Verbundkontroilsystem consists of a computing unit 21, which is connected to a display device 22, such as a monitor or a projector, and three interfaces 23, 24 and 25.
  • the interfaces 23 to 25 may be separate interfaces or a common interface.
  • the composite control system 2 is connected to the control station 31 of the observation system 3.
  • the composite control system 2 is connected to the control station 41 of the active system 4.
  • the composite control system 2 is connected to the guide system 5, for example a fire control system.
  • the guide system 5 is part of the weapon composite system 1.
  • the composite control system 2 transmits data on the situation of the scenario to the guidance system 5 and receives commands and information from the guidance system 5, ie is guided by the guidance system 5.
  • the arithmetic unit 21 includes, among other things, a processor, a graphics adapter, an input device, a main memory and a mass memory.
  • the processor processes and outputs data, such as through interfaces 23 through 25 or the graphics adapter.
  • the graphics adapter calculates an image for display on the display device 22.
  • the input device for example a mouse, a keyboard or a touch-sensitive surface of the display device 22, serves for the input of data.
  • the main memory contains the program code to be processed by the processor and stores the data to be processed and processed.
  • the mass storage is used to store larger amounts of data and the program code permanently
  • the arithmetic unit 21 receives and transmits data via the interfaces 23 to 25, processes the received data and displays the processed data on the display device 22. Since the control stations 31 and 41 of the observation system 3 and the active system 4 have a plurality of data, however, not all of which are relevant to the operator of the compound control system 2, only a subset of the available data is displayed on the display device 22. The filtering of the available data on the subset of the data takes place either in the compound control system 2 or in the respective control station 31 or 41, in that the compound control system 2 only selectively retrieves data from the respective control station 31 or 41 or notifies the respective control station 31 or 41 which Subset of the data are in particular regularly transferred to the compound control system.
  • the subset of data is defined by filter criteria, which in turn depend on one or more parameters. Examples of these parameters are the type of observation system 3, the type of the active system 4, the type of target and the scenario.
  • filter criteria are the type of observation system 3, the type of the active system 4, the type of target and the scenario.
  • a database with filter criteria records deposited which is searched on the basis of the parameters for a suitable record with filter criteria.
  • a record also includes a scheme for arranging the subset of the data on the display device 22.
  • the operator of the compound control system may enter or change the filter criteria via the input device.
  • the observer 32 and the creater 42 are interconnected via a bidirectional wireless data link. This connection can also be made via a relay.
  • sensor data of the observer 32 are shown, for example, an infrared or electro-optical video image, which is preferably enriched with further information, for example on the target.
  • sensor data of the warper 42 are displayed, for example an infrared or electro-optical video image, which is preferably enriched with further information, for example about the destination.
  • field F02 data on the status and / or the mission of the observer 32, such as the position, the direction of flight, the airspeed and the fuel remaining amount, are displayed.
  • data about the status and / or the mission of the warper 42 such as the position, the flight direction, the airspeed and the fuel remaining amount, are displayed.
  • the remaining time is displayed in the field F06, during which the use of the warper 42 can be canceled.
  • Field F03 displays a table or list of the status of one or more destinations, for example, for n destinations.
  • the status of the target is, for example, the speed, the direction of movement or the Condition of the target.
  • field F07 a table or list is displayed with the status of one or more active agents, for example for m effectors.
  • Field F04 is divided into three subfields, each representing release by one of three instances.
  • the field F09 is an input field through which the operator of the compound control system 2 can command or cancel the attack by the operator 42. Depending on the status of the warper 42, the field is deposited in different colors. If the attack is possible, but not yet commanded, the field F09 is deposited with a first color, for example green. An actuation of the field F09 in this state initiates the attack, ie the use of the razor 42. If the attack is ordered, but can still be canceled, the field F09 with a second color, such as red, deposited. Actuation of the field F09 in this state aborts the attack by the caster 42. If the attack is ordered and can no longer be aborted, the field F09 is deposited with a third color, for example black. Actuating field F09 in this state has no effect.
  • the composite control system 2 on the display device 22 is preferably a selection field, via which the type of termination of the attack can be selected.
  • the available types of demolition are shown, for example, return of the razor 42, self-destruction of the razor 42, rerouting of the razor 42 to an uncritical target area or intercepting flight.
  • the operator of the compound control system 2 has all decision essentials information and data with the smallest possible latency, since data of both an observation system and an active system are displayed on the same display device. Since the operator can also influence the action system, for example commanding or canceling the attack, guidance also takes place with the lowest possible latency. Thus, the time until which an operation can be effectively canceled, as far as possible delayed.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

L'invention concerne un système interarmes (1) comprenant au moins un système d'observation (3) comportant un poste de contrôle (31) du système d'observation, au moins un système actif (4) comportant un poste de contrôle (41) du système actif, et un système de contrôle interarmes (2) qui est relié aux postes de contrôle (31, 41) du système d'observation (3) et du système actif (4), le système de contrôle interarmes (2) présentant une unité de calcul (21) et un dispositif d'affichage (22) configurés pour afficher les données des postes de contrôle (31, 41) du système d'observation (3) et du système actif (4), et au moins une zone de saisie (F09) pour l'affichage des instructions au poste de contrôle (41) d'un système actif (4).
PCT/EP2013/069690 2012-10-15 2013-09-23 Système interarmes et procédé de commande dudit système Ceased WO2014060189A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP13773650.0A EP2906899A1 (fr) 2012-10-15 2013-09-23 Système interarmes et procédé de commande dudit système
IL238035A IL238035A0 (en) 2012-10-15 2015-03-30 A composite weapon system and a method for controlling it

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102012218746.4 2012-10-15
DE102012218746.4A DE102012218746A1 (de) 2012-10-15 2012-10-15 Waffenverbundsystem und Verfahren zur Steuerung desselben

Publications (1)

Publication Number Publication Date
WO2014060189A1 true WO2014060189A1 (fr) 2014-04-24

Family

ID=49304905

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2013/069690 Ceased WO2014060189A1 (fr) 2012-10-15 2013-09-23 Système interarmes et procédé de commande dudit système

Country Status (4)

Country Link
EP (1) EP2906899A1 (fr)
DE (1) DE102012218746A1 (fr)
IL (1) IL238035A0 (fr)
WO (1) WO2014060189A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014007456B3 (de) * 2014-05-21 2015-01-22 Mbda Deutschland Gmbh Modulares Lenkflugkörpersystem

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080052621A1 (en) * 2006-08-22 2008-02-28 University Of Florida Research Foundation, Inc. System and methods for providing integrated situational awareness
US20090326735A1 (en) * 2008-06-27 2009-12-31 Raytheon Company Apparatus and method for controlling an unmanned vehicle

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3778007A (en) * 1972-05-08 1973-12-11 Us Navy Rod television-guided drone to perform reconnaissance and ordnance delivery
US4267562A (en) * 1977-10-18 1981-05-12 The United States Of America As Represented By The Secretary Of The Army Method of autonomous target acquisition
DE19828644C2 (de) * 1998-06-26 2001-12-06 Lfk Gmbh Verfahren zum ferngesteuerten Bekämpfen bodennaher und/oder bodengebundener Ziele
EP1761431A4 (fr) * 2004-03-15 2010-09-22 Georgia Tech Res Inst Projectile et systeme pour assurer une reconnaissance air-sol
WO2007089243A2 (fr) * 2005-02-07 2007-08-09 Bae Systems Information And Electronic Systems Integration Inc. Procédé et système de commande de munition à guidage optique
US7767945B2 (en) * 2005-11-23 2010-08-03 Raytheon Company Absolute time encoded semi-active laser designation
KR102282901B1 (ko) * 2009-02-02 2021-07-29 에어로바이론먼트, 인크. 멀티모드 무인 항공기
US8648285B2 (en) * 2010-03-22 2014-02-11 Omnitek Partners Llc Remotely guided gun-fired and mortar rounds

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080052621A1 (en) * 2006-08-22 2008-02-28 University Of Florida Research Foundation, Inc. System and methods for providing integrated situational awareness
US20090326735A1 (en) * 2008-06-27 2009-12-31 Raytheon Company Apparatus and method for controlling an unmanned vehicle

Also Published As

Publication number Publication date
EP2906899A1 (fr) 2015-08-19
DE102012218746A1 (de) 2014-04-17
IL238035A0 (en) 2015-05-31

Similar Documents

Publication Publication Date Title
DE60113552T2 (de) Intuitives fahrzeug und maschinensteuerung
DE102012101654B3 (de) Militärisches Fahrzeug
EP3605256B1 (fr) Système et procédé de surveillance de l'état d'un aéronef sans pilote
Mouloua et al. Workload, situation awareness, and teaming issues for UAV/UCAV operations
DE102018200011A1 (de) Testsystem und Verfahren zum Testen einer Steuerung eines zumindest teilweise autonom fahrenden Fahrzeugs in einer virtuellen Umgebung
EP3725472A1 (fr) Procédé de détermination d'une trajectoire d'un robot
DE102019212842B4 (de) Steuerung eines Kraftfahrzeugs unter Verwendung einer unbemannten Flugvorrichtung
DE102015122090A1 (de) Fahrzeugfernsteuerung und -Betrieb
EP2293008A2 (fr) Dispositif de commande de tests fonctionnels et/ou de procédures de service pour aéronefs sans conducteur pouvant être déposés par des avions
DE102018105045A1 (de) Luftlageinformations- und Verkehrsmanagementsystem für unbemannte und bemannte Luftfahrzeuge
WO2020048718A1 (fr) Concept de surveillance et de planification d'un mouvement d'un moyen de transport
EP3499175B1 (fr) Procédé de commande d'un système de défense contre les véhicules aériens sans pilote
EP2511894B1 (fr) Procédé de surveillance d'un espace aérien autour d'un aéronef
EP2906899A1 (fr) Système interarmes et procédé de commande dudit système
EP1821246A2 (fr) Commande d'une plate-forme autonome
EP1014028A1 (fr) Système de guidage, de navigation et de commande pour missile
DE19716025B4 (de) Plattform mit abschießbaren, zielverfolgenden Flugkörpern, insbesondere Kampfflugzeug
EP2581699B1 (fr) Corps volant de test et de formation sans conducteur
DE102022124047A1 (de) Verfahren zur Steuerung von Ausweichmanövern im Luftraum
EP4172765A1 (fr) Répartition de charge et attribution de ressources dans un aéronef
DE102023118284B4 (de) Verfahren zum Steuern eines Schwarms aus Flugobjekten und System hierzu
WO2024042062A1 (fr) Procédé de commande d'un aéronef sans pilote
EP4495854A1 (fr) Procédé de fonctionnement d'une pluralité de drones répartis géographiquement
DE102023208378A1 (de) Verfahren zum Betreiben eines mobilen Arbeitsgeräts
DE102023136871A1 (de) Verfahren und System zum Steuern eines Schwarms aus Flugobjekten

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 13773650

Country of ref document: EP

Kind code of ref document: A1

WWE Wipo information: entry into national phase

Ref document number: 2013773650

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 238035

Country of ref document: IL