ES8404504A1 - Conjunto guiador semiactivo para un cuerpo volante dirigible buscador del objetivo - Google Patents

Conjunto guiador semiactivo para un cuerpo volante dirigible buscador del objetivo

Info

Publication number
ES8404504A1
ES8404504A1 ES524887A ES524887A ES8404504A1 ES 8404504 A1 ES8404504 A1 ES 8404504A1 ES 524887 A ES524887 A ES 524887A ES 524887 A ES524887 A ES 524887A ES 8404504 A1 ES8404504 A1 ES 8404504A1
Authority
ES
Spain
Prior art keywords
target
semi
illuminating
guidance system
guided missile
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
Application number
ES524887A
Other languages
English (en)
Other versions
ES524887A0 (es
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.)
Licentia Patent Verwaltungs GmbH
Original Assignee
Licentia Patent Verwaltungs 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 Licentia Patent Verwaltungs GmbH filed Critical Licentia Patent Verwaltungs GmbH
Publication of ES8404504A1 publication Critical patent/ES8404504A1/es
Publication of ES524887A0 publication Critical patent/ES524887A0/es
Granted legal-status Critical Current

Links

Classifications

    • 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
    • F41G7/22Homing guidance systems
    • F41G7/226Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles
    • 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
    • F41G7/22Homing guidance systems
    • F41G7/2273Homing guidance systems characterised by the type of waves
    • F41G7/2286Homing guidance systems characterised by the type of waves using radio waves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Sampling And Sample Adjustment (AREA)
  • Measuring Pulse, Heart Rate, Blood Pressure Or Blood Flow (AREA)

Abstract

CARACTERIZADO PORQUE COMPRENDE INSTALACIONES DE LOCALIZACION DE BLANCO Y POR LO MENOS UNA INSTALACION ILUMINADORA DE OBJETIVO CON DIAGRAMA DE DIRECCION OSCILABLE; PORQUE LA INSTALACION ILUMINADORA SOLO ESTA CONSTITUIDA COMO INSTALACION DE EMISION; PORQUE LAS INSTALACIONES DE LOCALIZACION DE OBJETIVO CONTIENEN UNA INSTALACION DE RADAR DE BUSCA CIRCULAR Y UNA INSTALACION DE PERSECUCION DE OBJETIVO CON DIAGRAMA EN FORMA DE LAPIZ; Y PORQUE LA FASE INICIAL DE LA ILUMINACION SE EJECUTA POR LA INSTALACION DE PERSECUCION DEL OBJETIVO.
ES524887A 1982-08-14 1983-08-11 Conjunto guiador semiactivo para un cuerpo volante dirigible buscador del objetivo Granted ES524887A0 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19823230267 DE3230267A1 (de) 1982-08-14 1982-08-14 Halbaktives leitsystem fuer einen zielsuchenden, lenkbaren flugkoerper

Publications (2)

Publication Number Publication Date
ES8404504A1 true ES8404504A1 (es) 1984-05-01
ES524887A0 ES524887A0 (es) 1984-05-01

Family

ID=6170862

Family Applications (1)

Application Number Title Priority Date Filing Date
ES524887A Granted ES524887A0 (es) 1982-08-14 1983-08-11 Conjunto guiador semiactivo para un cuerpo volante dirigible buscador del objetivo

Country Status (7)

Country Link
US (1) US4558836A (es)
EP (1) EP0100979B1 (es)
DE (2) DE3230267A1 (es)
DK (1) DK159860C (es)
ES (1) ES524887A0 (es)
GR (1) GR77566B (es)
NO (1) NO156389C (es)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6145784A (en) * 1997-08-27 2000-11-14 Trw Inc. Shared aperture dichroic active tracker with background subtraction
DE102004029343B4 (de) * 2004-06-17 2009-04-30 Diehl Bgt Defence Gmbh & Co. Kg Zielführungsvorrichtung für ein Fluggerät
FR2885213B1 (fr) * 2005-05-02 2010-11-05 Giat Ind Sa Procede de commande d'une munition ou sous-munition, systeme d'attaque, munition et designateur mettant en oeuvre un tel procede
US7767945B2 (en) 2005-11-23 2010-08-03 Raytheon Company Absolute time encoded semi-active laser designation
US7575191B2 (en) * 2006-01-27 2009-08-18 Lockheed Martin Corporation Binary optics SAL seeker (BOSS)
US8390802B2 (en) * 2009-05-13 2013-03-05 Bae Systems Information And Electronic Systems Intergration Inc. Distributed array semi-active laser designator sensor
US8344302B1 (en) * 2010-06-07 2013-01-01 Raytheon Company Optically-coupled communication interface for a laser-guided projectile
FR3050814B1 (fr) * 2016-04-29 2019-06-07 Airbus Helicopters Procede et dispositif d'aide a la visee pour le guidage laser d'un projectile

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3001186A (en) * 1951-08-17 1961-09-19 Otto J Baltzer Missile guidance system
US3116039A (en) * 1956-02-29 1963-12-31 Goldberg Michael Method of and system for guiding a missile
GB1064150A (en) * 1963-01-07 1967-04-05 British Aircraft Corp Ltd Improvements relating to target acquisition systems
GB1021867A (en) * 1963-10-28 1966-03-09 English Electric Aviat Ltd Improvements relating to visual identification of aircraft
DE1249124B (de) * 1965-03-26 1967-08-31 Albiswerk Zurich A G Zurich (Schweiz) Verfahren und Einrichtung zum Lenken eines ersten bewegten Korpers m Bezug auf einen zweiten bewegten Korper
FR1454451A (fr) * 1965-08-04 1966-02-11 Comp Generale Electricite Dispositif de pointage combiné radar-laser
DE2162983A1 (de) * 1971-12-18 1973-06-20 Fusban Ulrich Mit zielsucheinrichtung ausgestattetes lenkflugkoerpersystem
US3799676A (en) * 1972-05-26 1974-03-26 Us Air Force Optical tracking system
GB1406707A (en) * 1972-07-03 1975-09-17 British Aircraft Corp Ltd Object recognition
US4143835A (en) * 1972-09-12 1979-03-13 The United States Of America As Represented By The Secretary Of The Army Missile system using laser illuminator
US3974383A (en) * 1975-02-03 1976-08-10 Hughes Aircraft Company Missile tracking and guidance system
US4406429A (en) * 1978-04-13 1983-09-27 Texas Instruments Incorporated Missile detecting and tracking unit
DE2922592C2 (de) * 1979-06-02 1981-11-26 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zur Abwehr von Flugkörpern
DE2947492C2 (de) * 1979-11-24 1983-04-28 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt Lenkverfahren für Flugkörper

Also Published As

Publication number Publication date
DE3377155D1 (en) 1988-07-28
DK355783A (da) 1984-02-15
NO156389C (no) 1987-09-09
EP0100979B1 (de) 1988-06-22
DK355783D0 (da) 1983-08-04
GR77566B (es) 1984-09-24
US4558836A (en) 1985-12-17
NO832910L (no) 1984-02-15
EP0100979A1 (de) 1984-02-22
DE3230267A1 (de) 1984-02-16
ES524887A0 (es) 1984-05-01
NO156389B (no) 1987-06-01
DK159860C (da) 1991-05-13
DK159860B (da) 1990-12-17

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19970401