EP0915314A1 - Vorrichtung zur Lenkung eines fliegenden Gerätes, insbesondere eines Flugkörpers - Google Patents

Vorrichtung zur Lenkung eines fliegenden Gerätes, insbesondere eines Flugkörpers Download PDF

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Publication number
EP0915314A1
EP0915314A1 EP98402413A EP98402413A EP0915314A1 EP 0915314 A1 EP0915314 A1 EP 0915314A1 EP 98402413 A EP98402413 A EP 98402413A EP 98402413 A EP98402413 A EP 98402413A EP 0915314 A1 EP0915314 A1 EP 0915314A1
Authority
EP
European Patent Office
Prior art keywords
guidance
images
missile
touch screen
flying object
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
EP98402413A
Other languages
English (en)
French (fr)
Other versions
EP0915314B1 (de
Inventor
Frédéric Naccache
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.)
Aerospatiale Matra
Original Assignee
Airbus Group SAS
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 Group SAS filed Critical Airbus Group SAS
Publication of EP0915314A1 publication Critical patent/EP0915314A1/de
Application granted granted Critical
Publication of EP0915314B1 publication Critical patent/EP0915314B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30—Command link guidance systems
    • F41G7/32—Command link guidance systems for wire-guided missiles

Definitions

  • the present invention relates to a device for guidance of a flying object, in particular a missile.
  • said guide station includes a desk with a screen for viewing the generated images by said image sensor and a handle for controlling moving a pointing reticle on said screen.
  • the operator brings said aiming reticle to the selected point on said image, i.e. at the point to be reached by the flying object, for example the center of a target.
  • the pointing is accompanied generally of more or less damped oscillations around of the selected position, which of course leads a relatively long aiming time (about one second in the best of cases) and random precision.
  • the object of the present invention is to remedy these disadvantages. It relates to a guiding device a flying object, notably a missile, which allows a operator to carry out the guidance extremely quickly and precise.
  • the device for guidance of the aforementioned type is remarkable in that said guidance station includes a touch screen, on which the images generated by said sensor are viewed of images, the selection of said guide points being made by a specific contact of the touch screen to points considered, preferably either by means of a finger operator, either using an optical pen.
  • the transmission between the flying machine and the guidance station located on the ground is carried out by means of a hertzian connection and / or a fiber optic link.
  • Said guide device 1 is intended to guide a flying object, for example an M missile, on a target, in this case a C tank.
  • said guidance station 3 includes a flat ET touch screen, on which are viewed the I images generated by the image sensor 2, and the selection of a point P is carried out by a contact one-off touch screen AND, either directly by a finger D of the operator, of which a hand Ma is represented partially in broken lines, i.e. using an optical pen, not shown.
  • the calculation means 4 determine, continuously, guidance orders that move the missile M so as to bring a reticle R located in the center of the touch screen AND, at said selected point P and thus to guide missile M on target C.
  • the transmission of data between the missile M and the ground can be achieved either by means a fiber optic link, such as the L2 link, either by radio link, such as link L1.
  • said data transmission can be performed, either by separate means for both directions of transmission either by unique means double direction of transmission, which simplifies said device 1.
  • the image sensor 2 is mounted on the missile M.
  • said sensor of images 2 can also be arranged on the ground, for example at a shooting station not shown including also said guide station.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP98402413A 1997-10-10 1998-10-01 Vorrichtung zur Lenkung eines fliegenden Gerätes, insbesondere eines Flugkörpers Expired - Lifetime EP0915314B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9712667A FR2769699B1 (fr) 1997-10-10 1997-10-10 Dispositif de guidage d'un engin volant, notamment un missile
FR9712667 1997-10-10

Publications (2)

Publication Number Publication Date
EP0915314A1 true EP0915314A1 (de) 1999-05-12
EP0915314B1 EP0915314B1 (de) 2003-03-26

Family

ID=9512068

Family Applications (1)

Application Number Title Priority Date Filing Date
EP98402413A Expired - Lifetime EP0915314B1 (de) 1997-10-10 1998-10-01 Vorrichtung zur Lenkung eines fliegenden Gerätes, insbesondere eines Flugkörpers

Country Status (5)

Country Link
US (1) US6142410A (de)
EP (1) EP0915314B1 (de)
DE (1) DE69812537T2 (de)
FR (1) FR2769699B1 (de)
IL (1) IL126396A (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2837955A1 (fr) * 2002-03-29 2003-10-03 Giat Ind Sa Systeme de traitement des informations sur un champ de bataille
EP1391681A1 (de) * 2002-08-20 2004-02-25 Diehl Munitionssysteme GmbH & Co. KG Verfahren und Vorrichtung zur Echtzeit-Geländeaufklärung

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6924838B1 (en) * 2000-07-31 2005-08-02 Charlton Nieves Grenade cam
US20050062730A1 (en) * 2003-09-19 2005-03-24 Henryk Birecki Ergonomic pointing device
US6978717B1 (en) * 2004-08-16 2005-12-27 The United States Of America As Represented By The Secretary Of The Army Infrared camera deployed by grenade launcher
FR2875613B1 (fr) * 2004-09-23 2007-03-16 Giat Ind Sa Interface homme machine d'un systeme de traitement de menaces
US7968831B2 (en) * 2007-06-12 2011-06-28 The Boeing Company Systems and methods for optimizing the aimpoint for a missile
BR112012018778B1 (pt) * 2010-01-29 2020-12-01 Saab Ab sistema de orientação e método de guiar para rastrear e guiar pelo menos dois objetos
DE102014019199A1 (de) 2014-12-19 2016-06-23 Diehl Bgt Defence Gmbh & Co. Kg Maschinenwaffe
MX2021006494A (es) * 2018-12-05 2021-07-06 Ericsson Telefon Ab L M Apuntamiento a objetos.

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2433760A1 (de) * 1974-07-13 1976-01-29 Deutsche Forsch Luft Raumfahrt Ferngesteuertes bewegliches objekt
US4611771A (en) * 1985-04-18 1986-09-16 United States Of America As Represented By The Secretary Of The Army Fiber optic track/reaim system
EP0337254A2 (de) * 1988-04-15 1989-10-18 The Boeing Company Nachrichtenverbindung zwischen Fahrzeugen
DE3928244C1 (de) * 1989-08-26 1990-10-25 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
EP0483841A1 (de) * 1990-11-01 1992-05-06 Hughes Aircraft Company Integrierte optische Faserflugkörperprüfvorrichtung
EP0687626A1 (de) * 1994-06-15 1995-12-20 AEROSPATIALE Société Nationale Industrielle Beobachtungsystem mit einem ferngelenkten Flugzeug ausgerüstet
US5605307A (en) * 1995-06-07 1997-02-25 Hughes Aircraft Compay Missile system incorporating a targeting aid for man-in-the-loop missile controller

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2433760A1 (de) * 1974-07-13 1976-01-29 Deutsche Forsch Luft Raumfahrt Ferngesteuertes bewegliches objekt
US4611771A (en) * 1985-04-18 1986-09-16 United States Of America As Represented By The Secretary Of The Army Fiber optic track/reaim system
EP0337254A2 (de) * 1988-04-15 1989-10-18 The Boeing Company Nachrichtenverbindung zwischen Fahrzeugen
DE3928244C1 (de) * 1989-08-26 1990-10-25 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
EP0483841A1 (de) * 1990-11-01 1992-05-06 Hughes Aircraft Company Integrierte optische Faserflugkörperprüfvorrichtung
EP0687626A1 (de) * 1994-06-15 1995-12-20 AEROSPATIALE Société Nationale Industrielle Beobachtungsystem mit einem ferngelenkten Flugzeug ausgerüstet
US5605307A (en) * 1995-06-07 1997-02-25 Hughes Aircraft Compay Missile system incorporating a targeting aid for man-in-the-loop missile controller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2837955A1 (fr) * 2002-03-29 2003-10-03 Giat Ind Sa Systeme de traitement des informations sur un champ de bataille
WO2003083400A1 (fr) * 2002-03-29 2003-10-09 Giat Industries Systeme de traitement des informations sur un champ de bataille
EP1391681A1 (de) * 2002-08-20 2004-02-25 Diehl Munitionssysteme GmbH & Co. KG Verfahren und Vorrichtung zur Echtzeit-Geländeaufklärung

Also Published As

Publication number Publication date
IL126396A (en) 2001-10-31
FR2769699B1 (fr) 1999-12-10
FR2769699A1 (fr) 1999-04-16
DE69812537T2 (de) 2004-02-12
IL126396A0 (en) 1999-05-09
DE69812537D1 (de) 2003-04-30
US6142410A (en) 2000-11-07
EP0915314B1 (de) 2003-03-26

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