[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

EP0223949A1 - Method for detection, tracking and defence of flying objects - Google Patents

Method for detection, tracking and defence of flying objects Download PDF

Info

Publication number
EP0223949A1
EP0223949A1 EP86112713A EP86112713A EP0223949A1 EP 0223949 A1 EP0223949 A1 EP 0223949A1 EP 86112713 A EP86112713 A EP 86112713A EP 86112713 A EP86112713 A EP 86112713A EP 0223949 A1 EP0223949 A1 EP 0223949A1
Authority
EP
European Patent Office
Prior art keywords
target
sensor
target data
tracking
transformed
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
EP86112713A
Other languages
German (de)
French (fr)
Other versions
EP0223949B1 (en
Inventor
Winfried Dr. Ing. Büttner
Edgar Thiele
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.)
Siemens AG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Priority to AT86112713T priority Critical patent/ATE44610T1/en
Publication of EP0223949A1 publication Critical patent/EP0223949A1/en
Application granted granted Critical
Publication of EP0223949B1 publication Critical patent/EP0223949B1/en
Expired legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G5/00Elevating or traversing control systems for guns
    • F41G5/14Elevating or traversing control systems for guns for vehicle-borne guns
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G3/00Aiming or laying means
    • F41G3/02Aiming or laying means using an independent line of sight

Definitions

  • the invention relates to a method for the detection, tracking and defense of flying objects using a central common search sensor for a number of mobile weapon systems, each with a follow sensor and its own vehicle navigation system.
  • the invention is based on the object of specifying a location determination of a mobile weapon system which can be carried out with reasonable effort in the battlefield in a method of the type mentioned at the outset, which enables the target data relating to the location to be calculated with sufficient accuracy.
  • this object is achieved in that, with the location data of the weapon system ascertained by the vehicle navigation system, a transformation of the target data assigned by the search sensor to a weapon system is carried out, and that with the transformed target data, the follow-up sensor is controlled to the target, and that after activation with the target data determined by the follow-up sensor are compared with the assigned transformed target data and the difference values are stored as correction values for the target display on the display device of the follow-up sensor and for evaluation in the case of further target assignments to the weapon system.
  • the probability of activation is significantly improved by using this method, since the errors that are unavoidable when determining the location due to the slip of the drive of the vehicle relative to the ground can lead to a considerable deterioration in the data quality.
  • the air situation in the battlefield is continuously determined at a central point with a monitoring sensor (search radar) SR. Flying objects appearing in airspace are detected by the surveillance sensor and their target data after identification via a coordinating point KS is transmitted to one of several weapon systems WS1 to WSn stationed in the battlefield, each with a secondary radar FR.
  • a transformation of the assigned target data to the location of the weapon system is required, which requires knowledge of the location coordinates.
  • the values of the vehicle navigation system FNA are used for a first transformation with approximated data F of the monitoring sensor SR.
  • the errors that cannot be avoided with this transformation are due to inaccuracies in the measurement of the route by means of the vehicle navigation system FNA, which result from the slippage of the drive. These errors have a detrimental effect on the data accuracy and thus on the probability of activation of the weapon system. Repeatedly initiating the location determination by the vehicle navigation system FNA can only partially correct these errors be lifted.
  • a follow sensor FR located on the vehicle of the weapon system with the transformed data is applied to the assigned target.
  • the target data determined by the follow sensor FR with very high accuracy are compared with the data of the assigned target, which are still supplied by the central point.
  • the difference between the assigned target data and the target data determined by the subsequent sensor FR is stored and taken into account as a correction value in all further target assignments and target data transformations.
  • the target tracking system shown in FIG. 2 shows a block diagram of the device for the electronic data processing and data evaluation of a mobile weapon system for the defense against enemy flying objects.
  • RR is a radar searching radar, which assigns the target coordinates of a located target object Z to one of several mobile weapon systems WS.
  • the in-vehicle device consists of a following sensor FR, a vehicle navigation system FNA and a data preparation DA with a display device PPI.
  • the target data assigned by the central station is transformed to the location coordinates of the location of the weapon system WS determined by the travel time navigation system FNA and is displayed as the target object on the screen of the display device PPI.
  • the sequence sensor FR is now switched on by the operating personnel to the displayed target by means of a roller ball or control stick.
  • the following sensor FR delivers very precise during the tracking of the target object Z.
  • Target data which are compared in a comparator K with the transformed assigned target data.
  • the determined difference value ⁇ is stored in a memory SP and is taken into account as a correction value for the display on the PPI for all further target assignments by a central point (search radar) RR, especially after a change in the location of the weapon system WS.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Geophysics And Detection Of Objects (AREA)
  • Burglar Alarm Systems (AREA)

Abstract

1. Method for the detection and tracking of and defence against flying objects, using a central common surveillance sensor for a number of mobile weapon systems which are directed against the flying objects and have one tracking sensor, a separate vehicle navigation systems and a display device each, characterized in that the targeted data allocated to a weapons system (WS1 ... WSn) by the surveillance sensor (SR, RR) are transformed to the position coordinates, determined by the vehicle navigation system (FNA), of the location of deployment of the weapons system and are represented as target on the display device (PPl), that the transformed target data are used for locking the tracking sensor (FR) to the target (Z) and that the target data determined by means of the tracking sensor after the locking are compared with the previously allocated transformed target data and the difference values (DELTA) are stored as correction values for the representation of the target on the display device (PPl) and for the analysis during further target allocations to the weapons system (WS1 ... WSn).

Description

Die Erfindung bezieht sich auf ein Verfahren zur Erfassung, Verfolgung und Abwehr von Flugobjekten unter Verwendung eines zentralen gemeinsamen Rundsuchsensors für eine Anzahl mobiler Waffensysteme mit je einem Folgesensor und einer eigenen Fahrzeugnavigationsanlage.The invention relates to a method for the detection, tracking and defense of flying objects using a central common search sensor for a number of mobile weapon systems, each with a follow sensor and its own vehicle navigation system.

Es ist bekannt, im Gefechtsfeld mit mehreren an verschiedenen Standorten fest aufgestellten Waffen­systemen und eine zentrale Stelle mit einem Rundsuch­sensor vorzusehen, der das gesamte Gefechtsfeld überwacht. Werden feindliche Objekte geortet, dann werden Zieldaten dieser Objekte den Waffensystemen einzeln zugewiesen. Die voneinander abweichend Position von Rundsuchsensor und Waffensystem erfordert eine Zieldatentransformation, die auf den Standort des Waffensystems bezogen ist. Da die Ortskoordinaten fest installierter Waffensysteme im allgemeinen bekannt sind, haben die transformierten Zieldaten eine ausreichende Genauigkeit für eine Zielverfolgung bzw. für Abwehrmaßnahmen.It is known to provide in the battlefield with several weapon systems permanently installed at different locations and a central location with a round search sensor which monitors the entire battlefield. If enemy objects are located, the target data of these objects are individually assigned to the weapon systems. The different position of the circular search sensor and weapon system requires a target data transformation that is related to the location of the weapon system. Since the location coordinates of permanently installed weapon systems are generally known, the transformed target data have sufficient accuracy for target tracking or for countermeasures.

Im Gefechtsfeld nicht ortsfest stationierte Waffensysteme erfordern für die Bestimmung der Standort­koordinaten unter Umständen einen erheblichen Aufwand. Als Standort eines mobilen Waffensystems kann nur in seltenen Fällen ein trigonometrisch vermessener Punkt im Gefechtsfeld, der die Vorraussetzung für eine genaue Transformation der vom Rundsuchsensor zugewiesenen Zieldaten auf den Standort ermöglichen würde, gewählt werden.Weapon systems that are not stationed stationary in the battlefield may require considerable effort to determine the location coordinates. As a location of a mobile weapon system, a trigonometric point in the battlefield can only be used in rare cases, which is the prerequisite for an exact transformation of those assigned by the search sensor Target data on the location would allow to be chosen.

Der Erfindung liegt die Aufgabe zugrunde, bei einem Verfahren der eingangs genannten Art eine mit vertret­barem Aufwand im Gefechtsfeld durchführbare Standort­bestimmung eines mobilen Waffensystems anzugeben, die eine Berechnung der auf den Standort bezogenen Ziel­daten mit ausreichender Genauigkeit ermöglicht. Gemäß der Erfindung wird diese Aufgabe dadurch gelöst, daß mit den von der Fahrzeugnavigationsanlage ermittelten Standortdaten des Waffensystems eine Transformation der vom Rundsuchsensor einem Waffensystem zugewiesenen Zieldaten durchgeführt wird und daß mit den transformier­ten Zieldaten der Folgesensor an das Ziel gesteuert wird und daß die nach dem Aufschalten mit dem Folgesensor ermittelten Zieldaten mit den zugewiesenen transformierten Zieldaten verglichen und die Differenz­werte als Korrekturwerte für die Zieldarstellung auf dem Sichtgerät des Folgesensors und für die Auswertung bei weiteren Zielzuweisungen an das Waffensystem abgespei­chert werden.The invention is based on the object of specifying a location determination of a mobile weapon system which can be carried out with reasonable effort in the battlefield in a method of the type mentioned at the outset, which enables the target data relating to the location to be calculated with sufficient accuracy. According to the invention, this object is achieved in that, with the location data of the weapon system ascertained by the vehicle navigation system, a transformation of the target data assigned by the search sensor to a weapon system is carried out, and that with the transformed target data, the follow-up sensor is controlled to the target, and that after activation with the target data determined by the follow-up sensor are compared with the assigned transformed target data and the difference values are stored as correction values for the target display on the display device of the follow-up sensor and for evaluation in the case of further target assignments to the weapon system.

Die Aufschaltwahrscheinlichkeit wird durch Anwendung dieses Verfahrens wesentlich verbessert, da die bei der Standortbestimmung durch den Schlupf des Antriebes des Fahrzeuges gegenüber dem Erdboden unvermeidbaren Fehler zu einer unter Umständen erheblichen Verschlechterung der Datengüte führen können.The probability of activation is significantly improved by using this method, since the errors that are unavoidable when determining the location due to the slip of the drive of the vehicle relative to the ground can lead to a considerable deterioration in the data quality.

In der ersten Phase der Korrektur der Zieldaten durch Transformation auf den aktuellen Standort des Waffen­systems wird unter Verwendung der von der Fahrzeug­navigationsanlage ermittelten mehr oder weniger fehler­behafteten Standortkoordinaten mittels manueller Nachsteuerung des Folgesensors des Waffensystems eine Aufschaltung herbeigeführt und so die genauen Zielkoordinaten durch den Folgesensor ermittelt.In the first phase of the correction of the target data by transformation to the current location of the weapon system, using the location coordinates determined by the vehicle navigation system, a more or less erroneous location coordinate by means of manual readjustment of the follow-up sensor of the weapon system Activation brought about and so the exact target coordinates determined by the following sensor.

Die Erfindung und weitere Einzelheiten der Erfindung werden anhand der Figuren 1 und 2 beispielhaft erläutert.The invention and further details of the invention are explained by way of example with reference to FIGS. 1 and 2.

Es zeigen

  • Fig. 1 ein Feuerleitsystem mit einem zentralen Ortungs­gerät und mehreren mobilen Waffensystemen mit je inem Folgesensor,
  • Fig. 2 ein Blockschaltbild der Zieldatenverarbeitung in einem Waffensystem.
Show it
  • 1 shows a fire control system with a central location device and several mobile weapon systems, each with a follow sensor,
  • Fig. 2 is a block diagram of target data processing in a weapon system.

In einer zentralen Stelle wird mit einem Überwachungs­sensor (Suchradar) SR ständig die Luftlage im Gefechts­feld ermittelt. Im Luftraum auftauchende Flugobjekte werden vom Überwachungssensor erfaßt und deren Zieldaten nach Identifizierung über eine koordinierende Stelle KS einem von mehreren im Gefechtsfeld stationierten Waffen­systemen WS1 bis WSn mit je einem Folgeradar FR über­mittelt. Für alle weiteren Vorgänge ist eine Transforma­tion der zugewiesenen Zieldaten auf den Standort des Waffensystems erforderlich, welche die Kenntnis der Standortkoordinaten voraussetzt. Für eine erste Trans­formation mit angenäherten Daten F des Überwachungssen­sors SR werden die Werte der Fahrzeugnavigationsanlage FNA verwendet. Die Fehler, die bei dieser Transformation nicht zu vermeiden sind, gehen auf Ungenauigkeiten der Messung der Fahrstrecke mittels der Fahrzeugnavigations­anlage FNA zurück, die durch den Schlupf des Antriebes entstehen. Diese Fehler wirken sich nachteilig auf die Datengenauigkeit und damit auf die Aufschaltwahrschein­lichkeit des Waffensystems aus. Durch wiederholtes In­niziieren der Standortbestimmung durch die Fahrzeugnavi­gationsanlage FNA können diese Fehler nur teilweise be­ hoben werden.The air situation in the battlefield is continuously determined at a central point with a monitoring sensor (search radar) SR. Flying objects appearing in airspace are detected by the surveillance sensor and their target data after identification via a coordinating point KS is transmitted to one of several weapon systems WS1 to WSn stationed in the battlefield, each with a secondary radar FR. For all further processes, a transformation of the assigned target data to the location of the weapon system is required, which requires knowledge of the location coordinates. The values of the vehicle navigation system FNA are used for a first transformation with approximated data F of the monitoring sensor SR. The errors that cannot be avoided with this transformation are due to inaccuracies in the measurement of the route by means of the vehicle navigation system FNA, which result from the slippage of the drive. These errors have a detrimental effect on the data accuracy and thus on the probability of activation of the weapon system. Repeatedly initiating the location determination by the vehicle navigation system FNA can only partially correct these errors be lifted.

Um trotzdem mit den fehlerhaften Standortdaten der Fahrzeugnavigationsanlage FNA zu genauen Zieldaten zu kommen, wird ein am Fahrzeug des Waffensystems befind­licher Folgesensor FR mit den transformierten Daten auf das zugewiesene Ziel aufgeschaltet. Die vom Folgesensor FR mit sehr hoher Genauigkeit ermittelten Zieldaten wer­den mit den weiterhin von der zentralen Stelle geliefer­ten Daten des zugewiesenen Zieles verglichen. Die Dif­ferenz zwischen zugewiesenen Zieldaten und vom Folge­sensor FR ermittelten Zieldaten wird abgespeichert und bei allen weiteren Zielzuweisungen und Zieldatentrans­formationen als Korrekturwert berücksichtigt.In order nevertheless to arrive at exact target data with the incorrect location data of the vehicle navigation system FNA, a follow sensor FR located on the vehicle of the weapon system with the transformed data is applied to the assigned target. The target data determined by the follow sensor FR with very high accuracy are compared with the data of the assigned target, which are still supplied by the central point. The difference between the assigned target data and the target data determined by the subsequent sensor FR is stored and taken into account as a correction value in all further target assignments and target data transformations.

Das in Fig. 2 dargestellte Zielverfolgungssystem zeigt Blockschaltbild der Einrichtung für die elektronische Datenverarbeitung und Datenauswertung eines mobilen Waffensystems zur Abwehr von feindlichen Flugobjekten. Mit RR ist ein rundsuchendes Radar bezeichnet, das die Zielkoordinaten eines georteten Zielobjektes Z einem von mehreren mobilen Waffensystemen WS zuweist. Die fahr­zeugeigene Einrichtung besteht aus einem Folgesensor FR, einer Fahrzeugnavigationsanlage FNA und einer Datenauf­bereitung DA mit einer Anzeigeeinrichtung PPI.The target tracking system shown in FIG. 2 shows a block diagram of the device for the electronic data processing and data evaluation of a mobile weapon system for the defense against enemy flying objects. With RR is a radar searching radar, which assigns the target coordinates of a located target object Z to one of several mobile weapon systems WS. The in-vehicle device consists of a following sensor FR, a vehicle navigation system FNA and a data preparation DA with a display device PPI.

In einem Rechner MP werden die von der Zentralstation zugewiesenen Zieldaten auf die durch die Fahrzeitnavi­gationsanlage FNA ermittelten Ortskoordinaten des Stand­ortes des Waffensystems WS transformiert und als Zielob­jekt auf dem Bildschirm der Anzeigeeinrichtung PPI dar­gestellt. Der Folgesensor FR wird nun mittels Rollkugel oder Steuerknüppel vom Bedienungspersonal auf das darge­stellte Ziel aufgeschaltet. Der Folgesensor FR liefert während der Verfolgung des Zielobjektes Z sehr genaue Zieldaten, die in einem Komparator K mit den transfor­mierten zugewiesenen Zieldaten verglichen werden. Der ermittelte Differenzwert Δ wird in einem Speicher SP abgelegt und bei allen weiteren Zielzuweisungen durch eine zentrale Stelle (Rundsuchradar) RR vor allem nach einer Standortänderung des Waffensystems WS als Korrek­turwert für die Darstellung auf dem PPI berücksichtigt.In a computer MP, the target data assigned by the central station is transformed to the location coordinates of the location of the weapon system WS determined by the travel time navigation system FNA and is displayed as the target object on the screen of the display device PPI. The sequence sensor FR is now switched on by the operating personnel to the displayed target by means of a roller ball or control stick. The following sensor FR delivers very precise during the tracking of the target object Z. Target data, which are compared in a comparator K with the transformed assigned target data. The determined difference value Δ is stored in a memory SP and is taken into account as a correction value for the display on the PPI for all further target assignments by a central point (search radar) RR, especially after a change in the location of the weapon system WS.

BezugszeichenlisteReference symbol list

  • SR, RR = SuchradarSR, RR = search radar
  • KS = Koordinierende StelleKS = coordinating body
  • WS1,2...n = WaffensystemeWS1.2 ... n = weapon systems
  • FNA = FahrzeugnavigationsanlageFNA = car navigation system
  • Z = ZielobjektZ = target object
  • FR = FolgesensorFR = follow sensor
  • DA = DatenaufbereitungDA = data preparation
  • PPI = AnzeigeeinrichtungPPI = display device
  • Mp = RechnerMp = calculator
  • K = KomparatorK = comparator
  • Sp = SpeicherSp = memory
  • Δ = DifferenzwertΔ = difference value

Claims (1)

Verfahren zur Erfassung, Verfolgung und Abwehr von Flug­objekten unter Verwendung eines zentralen gemeinsamen Rundsuchsensors für eine Anzahl mobiler Waffensysteme mit je einem Folgesensor und einer eigenen Fahrzeugnavi­gationsanlage,
dadurch gekennzeichnet, daß mit den von der Fahrzeugnavigationsanlage (FNA) ermittelten Standortdaten des Waffensystems (WS1...WSn) eine Trans­formation der vom Rundsuchsensor (SR,RR) einem Waffen­system (WS1...WSn) zugewiesenen Zieldaten durchgeführt wird und daß mit den transformierten Zieldaten der Fol­gesensor (FR) an das Ziel (Z) gesteuert wird und daß die nach dem Aufschalten mit dem Folgesensor ermittelten Zieldaten mit den zugewiesenen transformierten Zieldaten verglichen und die Differenzwerte (Δ) als Korrekturwerte für die Zieldarstellung auf dem Sichtgerät (ppI) des Folgesensors (FR) und für die Auswertung bei weiteren Zielzuweisungen an das Waffensystem (WS1...WSn) abge­speichert werden.
Procedure for the detection, tracking and defense of flying objects using a central common search sensor for a number of mobile weapon systems, each with a follow-up sensor and its own vehicle navigation system,
characterized in that the location data of the weapon system (WS1 ... WSn) determined by the vehicle navigation system (FNA) is used to transform the target data assigned by the search sensor (SR, RR) to a weapon system (WS1 ... WSn) and that transformed target data of the following sensor (FR) is controlled to the target (Z) and that the target data determined after activation with the following sensor is compared with the assigned transformed target data and the difference values (Δ) as correction values for the target display on the display device (ppI) Follow sensor (FR) and for evaluation with further target assignments to the weapon system (WS1 ... WSn).
EP86112713A 1985-09-17 1986-09-15 Method for detection, tracking and defence of flying objects Expired EP0223949B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT86112713T ATE44610T1 (en) 1985-09-17 1986-09-15 PROCEDURES FOR DETECTING, TRACKING AND COUNTERING AIRCRAFT OBJECTS.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3533042 1985-09-17
DE3533042 1985-09-17

Publications (2)

Publication Number Publication Date
EP0223949A1 true EP0223949A1 (en) 1987-06-03
EP0223949B1 EP0223949B1 (en) 1989-07-12

Family

ID=6281113

Family Applications (1)

Application Number Title Priority Date Filing Date
EP86112713A Expired EP0223949B1 (en) 1985-09-17 1986-09-15 Method for detection, tracking and defence of flying objects

Country Status (3)

Country Link
EP (1) EP0223949B1 (en)
AT (1) ATE44610T1 (en)
DE (1) DE3664377D1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0884604A1 (en) * 1997-06-12 1998-12-16 Diehl Stiftung & Co. Warning sensor, especially for a target tracking device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4093153A (en) * 1965-11-18 1978-06-06 The United States Of America As Represented By The Secretary Of The Army Ground-controlled guided-missile system
DE3131089A1 (en) * 1981-08-06 1983-03-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Reconnaissance and fire-control system

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4093153A (en) * 1965-11-18 1978-06-06 The United States Of America As Represented By The Secretary Of The Army Ground-controlled guided-missile system
DE3131089A1 (en) * 1981-08-06 1983-03-03 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Reconnaissance and fire-control system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Bofors, Air Defence Weapons-Bofi AA-System * gesamt * *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0884604A1 (en) * 1997-06-12 1998-12-16 Diehl Stiftung & Co. Warning sensor, especially for a target tracking device
US6137436A (en) * 1997-06-12 2000-10-24 Diehl Stiftung & Co. Alarm sensor, in particular for a target tracking apparatus

Also Published As

Publication number Publication date
DE3664377D1 (en) 1989-08-17
ATE44610T1 (en) 1989-07-15
EP0223949B1 (en) 1989-07-12

Similar Documents

Publication Publication Date Title
DE10143561B4 (en) Method and system for locating emitters
DE69318023T2 (en) TARGET AND ALIGNMENT SYSTEM FOR A GROUND ARMOR DEVICE
DE69218143T2 (en) Autonomous precision weapon firing using a synthetic aperture radar
DE69006709T2 (en) System for determining the position on board an aircraft and its applications.
DE3937427A1 (en) IMAGE PROCESSING DEVICE
EP0429952A2 (en) Automatic landing system
EP0232762B1 (en) Method for acoustically determining the trajectory of projectiles and for the determination of the shortest distance projectile/target
DE69426585T2 (en) Sensor system
EP3620819B1 (en) Coordinated detection of objects in an airspace
DE3442598C2 (en) Guidance system for missiles
DE102018220782A1 (en) Localization of a vehicle based on dynamic objects
EP0223949B1 (en) Method for detection, tracking and defence of flying objects
DE3626030A1 (en) METHOD AND DEVICE FOR DISCOVERING A PRESENT VISUAL INTERRUPTION BETWEEN A PLANE AND A TARGET, ESPECIALLY IN A LASER FIRE CONTROL SYSTEM
DE3131089C2 (en) Reconnaissance and fire control system
Eggemeier et al. Application of automatic/controlled processing theory to training tactical command and control skills: II. Evaluation of a task analytic methodology
DE2018799A1 (en) Arrangement for the location and tracking of air targets. Note United Flugtechnische Werke-Fokker GmbH, 2800 Bremen
DE102016223526A1 (en) Method and device for determining a first highly accurate position of a vehicle
EP2897102A1 (en) Method for determining positional data of a target object in a reference system and method for guiding an aircraft, preferably in the form of a missile
DE69310695T2 (en) Procedure for the control aid of a low-flying missile
DE102018211240A1 (en) Method for classifying an object's relevance
EP0745828A1 (en) Method for determining roll of a spinning flying object
DE3225474C2 (en) Method of target recognition
DE3222255C2 (en)
DE3537730C2 (en)
DE102020204034A1 (en) Method and device for calibrating at least one radar sensor

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH DE FR GB IT LI LU NL SE

17P Request for examination filed

Effective date: 19870626

17Q First examination report despatched

Effective date: 19881221

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH DE FR GB IT LI LU NL SE

REF Corresponds to:

Ref document number: 44610

Country of ref document: AT

Date of ref document: 19890715

Kind code of ref document: T

REF Corresponds to:

Ref document number: 3664377

Country of ref document: DE

Date of ref document: 19890817

ITF It: translation for a ep patent filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19890930

ET Fr: translation filed
GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: LU

Payment date: 19900807

Year of fee payment: 5

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: AT

Payment date: 19900830

Year of fee payment: 5

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 19900913

Year of fee payment: 5

ITTA It: last paid annual fee
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Effective date: 19910915

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Effective date: 19910916

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 19920820

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 19920915

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 19920917

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 19920930

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 19921124

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 19921215

Year of fee payment: 7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Effective date: 19930915

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Effective date: 19930930

Ref country code: CH

Effective date: 19930930

Ref country code: BE

Effective date: 19930930

BERE Be: lapsed

Owner name: SIEMENS A.G. BERLIN UND MUNCHEN

Effective date: 19930930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Effective date: 19940401

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 19930915

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19940531

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Effective date: 19940601

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

EUG Se: european patent has lapsed

Ref document number: 86112713.2

Effective date: 19920408

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

Effective date: 20050915