ES2012816A6 - Lanzador de misiles controlados por hilo y dirigidos opticamente con circuito electronico mejorado - Google Patents

Lanzador de misiles controlados por hilo y dirigidos opticamente con circuito electronico mejorado

Info

Publication number
ES2012816A6
ES2012816A6 ES8700639A ES8700639A ES2012816A6 ES 2012816 A6 ES2012816 A6 ES 2012816A6 ES 8700639 A ES8700639 A ES 8700639A ES 8700639 A ES8700639 A ES 8700639A ES 2012816 A6 ES2012816 A6 ES 2012816A6
Authority
ES
Spain
Prior art keywords
launcher
wire
missile
optically guided
improved electronic
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
ES8700639A
Other languages
English (en)
Inventor
Emil Goldfeld
Yuri Takserman
Shlomo Harush
Shmuel Weiler
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.)
Israel Military Industries Ltd
State of Israel
Original Assignee
Israel Military Industries Ltd
State of Israel
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 Israel Military Industries Ltd, State of Israel filed Critical Israel Military Industries Ltd
Publication of ES2012816A6 publication Critical patent/ES2012816A6/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F41G7/30—Command link guidance systems
    • F41G7/32—Command link guidance systems for wire-guided missiles

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

LANZADOR DE MISILES CONTROLADOS POR HILO Y DIRIGIDOS OPTICAMENTE, CON CIRCUITO ELECTRONICO MEJORADO. LANZADOR DE MISILES CONTROLADOS POR HILO Y DIRIGIDOS OPTICAMENTE Y LANZADOS CON TUBO. EN EL CIRCUITO ELECTRONICO QUE FORMA PARTE DEL SERVOMECANISMO DE REALIMENTACION SE DISPONE DE CANALES DE INCLINACION Y DESVIACION CON INCREMENTOS VARIABLES DE TIEMPO QUE TIENEN FUNCIONES DE TRANSFERENCIA DISTINTAS. OPCIONALMENTE EXISTEN, ADEMAS, POR LO MENOS DOS GENERADORES DE SEÑALES DIFERENTES PARA EL AJUSTE DE LA GRAVEDAD CON MEDIOS AUTOMATICOS PARA SELECCIONAR ENTRE AMBOS EL QUE CORRESPONDE A LAS CARACTERISTICAS FISICAS DEL MISIL.
ES8700639A 1986-05-12 1987-03-09 Lanzador de misiles controlados por hilo y dirigidos opticamente con circuito electronico mejorado Expired - Lifetime ES2012816A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IL78757A IL78757A0 (en) 1986-05-12 1986-05-12 Launcher for an optically guided,wire-controlled missile with improved electronic circuitry

Publications (1)

Publication Number Publication Date
ES2012816A6 true ES2012816A6 (es) 1990-04-16

Family

ID=11056765

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8700639A Expired - Lifetime ES2012816A6 (es) 1986-05-12 1987-03-09 Lanzador de misiles controlados por hilo y dirigidos opticamente con circuito electronico mejorado

Country Status (8)

Country Link
US (1) US4705237A (es)
EP (1) EP0253919A3 (es)
DK (1) DK90787A (es)
ES (1) ES2012816A6 (es)
GR (1) GR870293B (es)
IL (1) IL78757A0 (es)
NO (1) NO870726L (es)
PT (1) PT84451B (es)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5035375A (en) * 1988-12-19 1991-07-30 Hughes Aircraft Company Fiber optic radar guided missile system
US5123610A (en) * 1989-07-21 1992-06-23 Hughes Aircraft Company Retrofit digital electronics unit for a tube-launched missile
US5082199A (en) * 1989-07-21 1992-01-21 Hughes Aircraft Company Digital electronics assembly for a tube-launched missile
US5118050A (en) * 1989-12-07 1992-06-02 Hughes Aircraft Company Launcher control system
US5080300A (en) * 1989-12-07 1992-01-14 Hughes Aircraft Company Launcher control system for surface launched active radar missiles
US5042742A (en) * 1989-12-22 1991-08-27 Hughes Aircraft Company Microcontroller for controlling an airborne vehicle
US5074491A (en) * 1990-08-14 1991-12-24 Hughes Aircraft Company Method for correcting misalignment between multiple missile track links
US5096139A (en) * 1990-08-16 1992-03-17 Hughes Aircraft Company Missile interface unit
US5106033A (en) * 1991-03-22 1992-04-21 Hughes Aircraft Company Missile guidance electronics assembly for portable guided missile launcher
US20050131592A1 (en) * 2003-12-15 2005-06-16 The Boeing Company In-flight control system stability margin assessment
RU2261412C1 (ru) * 2004-07-23 2005-09-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Способ наведения управляемой ракеты и пусковая установка для его реализации
US10429151B2 (en) 2017-06-13 2019-10-01 Raytheon Company Recapture of remotely-tracked command guided vehicle into the tracker's field-of-view

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE624406A (es) * 1961-11-06
US3366346A (en) * 1965-07-19 1968-01-30 Army Usa Remote missile command system
US3711046A (en) * 1969-10-22 1973-01-16 H Barhydt Automatic missile guidance system
SE364360B (es) * 1972-06-26 1974-02-18 Bofors Ab
US4406429A (en) * 1978-04-13 1983-09-27 Texas Instruments Incorporated Missile detecting and tracking unit
US4474343A (en) * 1981-05-04 1984-10-02 Hughes Aircraft Company Jitter compensating scene stabilizing missile guidance system
GB2132794B (en) * 1982-12-18 1986-02-26 British Aerospace Missile guidance system
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

Also Published As

Publication number Publication date
PT84451A (en) 1987-04-01
NO870726L (no) 1987-11-13
EP0253919A3 (en) 1989-04-26
US4705237A (en) 1987-11-10
EP0253919A2 (en) 1988-01-27
NO870726D0 (no) 1987-02-23
DK90787D0 (da) 1987-02-23
PT84451B (pt) 1989-12-29
DK90787A (da) 1987-11-13
IL78757A0 (en) 1986-08-31
GR870293B (en) 1987-09-07

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19990405