EP0915314B1 - 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
EP0915314B1
EP0915314B1 EP98402413A EP98402413A EP0915314B1 EP 0915314 B1 EP0915314 B1 EP 0915314B1 EP 98402413 A EP98402413 A EP 98402413A EP 98402413 A EP98402413 A EP 98402413A EP 0915314 B1 EP0915314 B1 EP 0915314B1
Authority
EP
European Patent Office
Prior art keywords
aircraft
guide
missile
images
screen
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.)
Expired - Lifetime
Application number
EP98402413A
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English (en)
French (fr)
Other versions
EP0915314A1 (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
Aerospatiale Matra
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 Aerospatiale Matra filed Critical Aerospatiale Matra
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 reach by the flying object, for example the center of a target.
  • a device of the known art is disclosed by EP-A-0 337 254.
  • 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, including 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 object 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 means of a radio link, such as the 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)

Claims (6)

  1. Vorrichtung zur Lenkung eines fliegenden Geräts (M), insbesondere eines Flugkörpers, die Folgendes umfasst:
    einen Bildsensor (2), der Bilder (I) von der vor dem genannten fliegenden Gerät (M) liegenden Umgebung erzeugt;
    Mittel zur Datenübertragung;
    einen Lenkstand (3), der die vom genannten Bildsensor (2) erzeugten Bilder (I) über die genannten Datenübertragungsmittel erhält und sie auf einem Bildschirm zeigt, wobei der genannte Lenkstand (3) außerdem einen Berührungsbildschirm (ET) umfasst; und
    Rechenmittel (4), die mit dem genannten Lenkstand (3) verbunden sind und Lenkbefehle des fliegenden Geräts (M) ermitteln, wobei die genannten Lenkbefehle zu Lenkorganen (6A, 6B) übertragen werden, die am genannten fliegenden Gerät (M) befestigt sind,
    dadurch gekennzeichnet, dass es sich bei dem genannten Bildschirm, der die Bilder (I) zeigt, und dem genannten Berührungsbildschirm (ET) um ein und denselben Bildschirm handelt, der gleichzeitig:
    die vom genannten Bildsensor (2) erzeugten Bilder (I) anzeigt; und
    es einem Bediener gestattet, durch einen Punktkontakt des Berührungsbildschirms (ET) einen Lenkpunkt (P) auszuwählen, zu dem er das genannte fliegende Gerät (M) lenken möchte;
    sowie dadurch, dass
    die genannten Rechenmittel (4) fortlaufend Lenkbefehle ermitteln, die es ermöglichen, den Flugkörper (M) so zu bewegen, dass ein Zielkreuz (R) des Berührungsbildschirms (ET) auf den gewählten Punkt (P) gebracht wird.
  2. Vorrichtung gemäß Anspruch 1,
    dadurch gekennzeichnet, dass der genannte Berührungsbildschirm (ET) ein Flachbildschirm ist.
  3. Vorrichtung gemäß Anspruch 1 oder 2,
    dadurch gekennzeichnet, dass der genannte Punktkontakt direkt durch einen Finger (D) des Bedieners hergestellt wird.
  4. Vorrichtung gemäß Anspruch 1 oder 2,
    dadurch gekennzeichnet, dass der genannte Punktkontakt durch einen Lichtstift hergestellt wird.
  5. Vorrichtung gemäß einem der Ansprüche 1 bis 4,
    dadurch gekennzeichnet, dass die Datenübertragung zwischen dem fliegenden Gerät (M) und dem auf dem Boden befindlichen Lenkstand (3) mit einer Funkverbindung (L1) erfolgt.
  6. Vorrichtung gemäß einem der Ansprüche 1 bis 5,
    dadurch gekennzeichnet, dass die Datenübertragung zwischen dem fliegenden Gerät (M) und dem auf dem Boden befindlichen Lenkstand (3) mit einer Lichtwellenleiterverbindung (L2) erfolgt.
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 EP0915314A1 (de) 1999-05-12
EP0915314B1 true 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)

Families Citing this family (10)

* 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
FR2837955B1 (fr) * 2002-03-29 2006-03-03 Giat Ind Sa Systeme de traitement des informations sur un champ de bataille
DE10238019A1 (de) * 2002-08-20 2004-03-11 Diehl Munitionssysteme Gmbh & Co. Kg Verfahren und Vorrichtung zur Echtzeit-Geländeaufklärung
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
ES2773740T3 (es) * 2010-01-29 2020-07-14 Saab Ab Un sistema y procedimiento para rastrear y guiar múltiples objetos
DE102014019199A1 (de) 2014-12-19 2016-06-23 Diehl Bgt Defence Gmbh & Co. Kg Maschinenwaffe
WO2020114595A1 (en) * 2018-12-05 2020-06-11 Telefonaktiebolaget Lm Ericsson (Publ) Object targeting

Family Cites Families (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
US4860968A (en) * 1988-04-15 1989-08-29 The Boeing Company Communication link between moving bodies
DE3928244C1 (de) * 1989-08-26 1990-10-25 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
CA2049270A1 (en) * 1990-11-01 1992-05-02 Robert W. Petty Integrated fiber optic missile test system
FR2721458B1 (fr) * 1994-06-15 1996-09-13 Aerospatiale Système d'observation par aéronef télépilote.
US5605307A (en) * 1995-06-07 1997-02-25 Hughes Aircraft Compay Missile system incorporating a targeting aid for man-in-the-loop missile controller

Also Published As

Publication number Publication date
US6142410A (en) 2000-11-07
FR2769699A1 (fr) 1999-04-16
EP0915314A1 (de) 1999-05-12
IL126396A (en) 2001-10-31
IL126396A0 (en) 1999-05-09
DE69812537T2 (de) 2004-02-12
FR2769699B1 (fr) 1999-12-10
DE69812537D1 (de) 2003-04-30

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