ES2019756A6 - Sistema de guia de misiles por radar y fibra optica. - Google Patents

Sistema de guia de misiles por radar y fibra optica.

Info

Publication number
ES2019756A6
ES2019756A6 ES8904260A ES8904260A ES2019756A6 ES 2019756 A6 ES2019756 A6 ES 2019756A6 ES 8904260 A ES8904260 A ES 8904260A ES 8904260 A ES8904260 A ES 8904260A ES 2019756 A6 ES2019756 A6 ES 2019756A6
Authority
ES
Spain
Prior art keywords
radar
fiber optic
receiver
launcher
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 - Fee Related
Application number
ES8904260A
Other languages
English (en)
Inventor
Kenneth J Friedenthal
La Chapelle Michael De
Hui-Pin Hsu
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.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
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 Hughes Aircraft Co filed Critical Hughes Aircraft Co
Publication of ES2019756A6 publication Critical patent/ES2019756A6/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

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
    • F41G7/22—Homing guidance systems
    • F41G7/226—Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles
    • F41G7/2266—Systems comparing signals received from a base station and reflected from the target
    • 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
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2286—Homing guidance systems characterised by the type of waves using radio waves
    • 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
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • 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

Abstract

SISTEMA DE GUIA DE MISILES POR RADAR Y FIBRA OPTICA (10) QUE INCLUYE UN RECEPTOR DE RADAR (12) DISPUESTO EN UN MISIL PARA RECIBIR REFLEXIONES DE RADAR Y PROPORCIONAR EN RESPUESTA A ESTAS REFLEXIONES UNA PRIMERA SEÑAL OPTICA. UN RECEPTOR OPTICO (14) ESTA MONTADO EN UN DISPOSITIVO DE LANZAMIENTO PARA RECIBIR LA PRIMERA SEÑAL OPTICA Y PARA PROPORCIONAR EN RESPUESTA A ESTA SEÑAL UNA SERIE DE SEÑALES ELECTRICAS. UN ENLACE DE FIBRA OPTICA (32) ESTA CONECTADO ENTRE EL MISIL Y EL DISPOSITIVO DE LANZAMIENTO PARA COMUNICAR LA PRIMERA SEÑAL OPTICA DESDE EL RECEPTOR DE RADAR (12) AL RECEPTOR OPTICO (14).
ES8904260A 1988-12-19 1989-12-18 Sistema de guia de misiles por radar y fibra optica. Expired - Fee Related ES2019756A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/286,436 US5035375A (en) 1988-12-19 1988-12-19 Fiber optic radar guided missile system

Publications (1)

Publication Number Publication Date
ES2019756A6 true ES2019756A6 (es) 1991-07-01

Family

ID=23098602

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8904260A Expired - Fee Related ES2019756A6 (es) 1988-12-19 1989-12-18 Sistema de guia de misiles por radar y fibra optica.

Country Status (11)

Country Link
US (1) US5035375A (es)
EP (1) EP0401327B1 (es)
JP (1) JP2529472B2 (es)
KR (1) KR940011259B1 (es)
AU (1) AU619365B2 (es)
CA (1) CA2002987C (es)
DE (1) DE68916790T2 (es)
ES (1) ES2019756A6 (es)
IL (1) IL92878A (es)
NO (1) NO180697C (es)
WO (1) WO1990007093A1 (es)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2049270A1 (en) * 1990-11-01 1992-05-02 Robert W. Petty Integrated fiber optic missile test system
US5296860A (en) * 1991-11-04 1994-03-22 Li Ming Chiang Optical fiber based bistatic radar
US5310134A (en) * 1992-03-16 1994-05-10 Hughes Aircraft Company Tethered vehicle positioning system
US5186414A (en) * 1992-04-20 1993-02-16 The United States Of America As Represented By The Secretary Of The Navy Hybrid data link
US5396357A (en) * 1994-01-25 1995-03-07 Honeywell Inc. Fault tolerant optical cross-channel data link
US6064332A (en) * 1994-04-26 2000-05-16 The United States Of America As Represented By The Secretary Of The Air Force Proportional Guidance (PROGUIDE) and Augmented Proportional Guidance (Augmented PROGUIDE)
US5458041A (en) * 1994-08-02 1995-10-17 Northrop Grumman Corporation Air defense destruction missile weapon system
USH1980H1 (en) 1996-11-29 2001-08-07 The United States Of America As Represented By The Secretary Of The Air Force Adaptive matched augmented proportional navigation
US5944281A (en) * 1998-03-09 1999-08-31 The United States Of America As Represented By The Secretary Of The Army Dual band millimeter-infrared fiber optics guidance data link
US6345784B1 (en) * 1999-11-26 2002-02-12 Tadiran Spectralink Ltd System and method for munition impact assessment
US6474592B1 (en) * 2001-05-25 2002-11-05 Tadiran Spectralink Ltd. System and method for munition impact assessment
US20050023409A1 (en) * 2003-07-28 2005-02-03 Moshe Shnaps System and method for munition impact assessment
US7882983B2 (en) 2003-08-14 2011-02-08 3M Innovative Properties Company Capsule for two-component materials
US7158072B1 (en) * 2006-09-08 2007-01-02 Rockwell Collins, Inc. Ethernet connection of airborne radar over fiber optic cable
US7956733B1 (en) 2008-09-23 2011-06-07 The United States Of America As Represented By The Secretary Of The Navy Optical fiber sensor for quantitative monitoring of deflection from high-speed launcher operation conditions

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3041011A (en) * 1951-03-12 1962-06-26 Rand Corp Method and apparatus for vernier map matching and flight control therewith
US3001186A (en) * 1951-08-17 1961-09-19 Otto J Baltzer Missile guidance system
US3182930A (en) * 1956-10-10 1965-05-11 Jr Joseph P Randolph Missile in flight indicator
US3729150A (en) * 1961-04-19 1973-04-24 Us Navy Missile guidance system
DE977989C (es) * 1964-06-19 1974-12-12
US4653032A (en) * 1969-10-10 1987-03-24 Schwarz Hans D Arrangement for the determination of the direction and/or distance of objects by means of water-borne sound waves
US3743215A (en) * 1971-08-25 1973-07-03 Us Army Switching system and method for missile guidance control in a tvm system
US3943357A (en) * 1973-08-31 1976-03-09 William Howard Culver Remote controlled vehicle systems
US3938148A (en) * 1974-07-10 1976-02-10 The United States Of America As Represented By The Secretary Of The Navy Automatic frequency control system
US4185796A (en) * 1976-12-13 1980-01-29 The United States Of America As Represented By The Secretary Of The Army Fiber optic missile guidance and control
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
IL78757A0 (en) * 1986-05-12 1986-08-31 Israel State Launcher for an optically guided,wire-controlled missile with improved electronic circuitry
US4907763A (en) * 1987-03-31 1990-03-13 The Boeing Company Optical fiber guided tube-launched projectile system
US4967980A (en) * 1987-03-31 1990-11-06 The Boeing Company Optical fiber guided tube-launched projectile system
US4796833A (en) * 1987-03-31 1989-01-10 The Boeing Company Optical fiber guided tube-launched projectile system
US4770370A (en) * 1987-03-31 1988-09-13 The Boeing Company Optical fiber guided tube-launched projectile system
US4860968A (en) * 1988-04-15 1989-08-29 The Boeing Company Communication link between moving bodies
US4974793A (en) * 1989-12-15 1990-12-04 The Boeing Company Tapered chamber dispensing of optical fiber

Also Published As

Publication number Publication date
JPH03502834A (ja) 1991-06-27
IL92878A (en) 1992-07-15
KR940011259B1 (ko) 1994-12-03
CA2002987A1 (en) 1990-06-19
JP2529472B2 (ja) 1996-08-28
EP0401327A1 (en) 1990-12-12
US5035375A (en) 1991-07-30
IL92878A0 (en) 1990-09-17
EP0401327B1 (en) 1994-07-13
WO1990007093A1 (en) 1990-06-28
KR910700441A (ko) 1991-03-15
DE68916790D1 (de) 1994-08-18
NO903501D0 (no) 1990-08-09
CA2002987C (en) 1994-04-05
NO180697C (no) 1997-05-28
AU4629689A (en) 1990-07-10
NO180697B (no) 1997-02-17
AU619365B2 (en) 1992-01-23
DE68916790T2 (de) 1994-10-27
NO903501L (no) 1990-08-09

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Legal Events

Date Code Title Description
SA6 Expiration date (snapshot 920101)

Free format text: 2009-12-18

FD1A Patent lapsed

Effective date: 20010301