ES2078320T3 - Sistema de control de lanzaderas para misiles con radar activo lanzados desde el suelo. - Google Patents
Sistema de control de lanzaderas para misiles con radar activo lanzados desde el suelo.Info
- Publication number
- ES2078320T3 ES2078320T3 ES90312730T ES90312730T ES2078320T3 ES 2078320 T3 ES2078320 T3 ES 2078320T3 ES 90312730 T ES90312730 T ES 90312730T ES 90312730 T ES90312730 T ES 90312730T ES 2078320 T3 ES2078320 T3 ES 2078320T3
- Authority
- ES
- Spain
- Prior art keywords
- launcher
- airported
- vehicle
- control system
- target position
- 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
Links
- 238000010276 construction Methods 0.000 abstract 1
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
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
- F41G7/306—Details for transmitting guidance signals
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)
- Radar Systems Or Details Thereof (AREA)
- Feedback Control In General (AREA)
- Aerials With Secondary Devices (AREA)
Abstract
UN SISTEMA DE ARMAMENTO (10) QUE TIENE INCORPORADO UN SENSOR DE LA POSICION DEL BLANCO (14), UN SISTEMA DE INFORMACION (16), UNA FUENTE DE POTENCIA (24), UN LANZADOR (20) Y UN VEHICULO AEROPORTADO (18), UN SISTEMA DE CONTROL DEL LANZADOR (12) QUE TIENE UNA INTERFASE DE COMUNICACION (26) PARA ACOPLAR EL SISTEMA DE INFORMACION (16) Y EL SENSOR DE POSICION DEL BLANCO (14) A UN LANZADOR (20) Y UN VEHICULO AEROPORTADO (18). LA INTERFASE DE COMUNICACION (26) RECIBE LA INFORMACION SOBRE LA POSICION DEL BLANCO Y SOBRE LAS ORDENES DE LANZAMIENTO Y DE CONTROL Y PROPORCIONA UN ESTADO DEL LANZADOR Y DEL VEHICULO AEROPORTADO. UNA INTERFASE DE VEHICULO AEROPORTADO (28) ACOPLA EL LANZADOR (20) Y EL VEHICULO AEROPORTADO AL SISTEMA DE INFORMACION (16) Y A UNA FUENTE DE POTENCIA (22) . UN TRANSMISOR (30) COMUNICA INFORMACION SOBRE LA POSICION DEL BLANCO ACTUALIZADA AL VEHICULO AEROPORTADO DESPUES DEL LANZAMIENTO. UN MEDIO DE CONTROL DE POTENCIA (32) CONVIERTE Y REGULA LA POTENCIA DE DIFERENTES FUENTES DE POTENCIA (22) A SER UTILIZADA POR EL SISTEMA DE CONTROL DEL LANZADOR (12). EL LANZADOR (20) QUE TIENE EL SISTEMA DE CONTROL DEL LANZADOR (12) TIENE PREFERIBLEMENTE UNA CONSTRUCCION MODULAR Y ESTA SEPARADO DEL SISTEMA DE INFORMACION (16) Y DEL SENSOR DE LA POSICION DEL BLANCO (14).
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/447,320 US5080300A (en) | 1989-12-07 | 1989-12-07 | Launcher control system for surface launched active radar missiles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2078320T3 true ES2078320T3 (es) | 1995-12-16 |
Family
ID=23775894
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES90312730T Expired - Lifetime ES2078320T3 (es) | 1989-12-07 | 1990-11-22 | Sistema de control de lanzaderas para misiles con radar activo lanzados desde el suelo. |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US5080300A (es) |
| EP (1) | EP0431804B1 (es) |
| JP (1) | JPH081359B2 (es) |
| CA (1) | CA2029281C (es) |
| DE (1) | DE69023103T2 (es) |
| ES (1) | ES2078320T3 (es) |
| GR (1) | GR3018677T3 (es) |
| IL (1) | IL96263A (es) |
| NO (1) | NO302317B1 (es) |
| TR (1) | TR26546A (es) |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5118050A (en) * | 1989-12-07 | 1992-06-02 | Hughes Aircraft Company | Launcher control system |
| FR2712972B1 (fr) * | 1993-11-25 | 1996-01-26 | Aerospatiale | Système de défense antiaérien et missile de défense pour un tel système. |
| US5671139A (en) * | 1995-07-06 | 1997-09-23 | Bessacini; Anthony F. | Hierarchical fuzzy controller for beam rider guidance |
| US5671140A (en) * | 1995-07-06 | 1997-09-23 | The United States Of America As Represented By The Secretary Of The Navy | Fuzzy controller for target intercept guidance |
| US5671138A (en) * | 1995-07-06 | 1997-09-23 | The United States Of America As Represented By The Secretary Of The Navy | Fuzzy controller for acoustic vehicle target intercept guidance |
| US5828571A (en) * | 1995-08-30 | 1998-10-27 | The United States Of America As Represented By The Secretary Of The Navy | Method and apparatus for directing a pursuing vehicle to a target with evasion capabilities |
| US5944762A (en) * | 1996-04-01 | 1999-08-31 | The United States Of America As Represented By The Secretary Of The Navy | Hierarchical target intercept fuzzy controller with forbidden zone |
| US5987362A (en) * | 1997-10-06 | 1999-11-16 | The United States Of America As Represented By The Secretary Of The Navy | Final approach trajectory control with fuzzy controller |
| US6161061A (en) * | 1998-06-26 | 2000-12-12 | The United States Of America As Represented By The Secretary Of The Navy | Guidance controller for a minimal discrete command set |
| RU2151359C1 (ru) * | 1998-11-02 | 2000-06-20 | Научно-производственное объединение машиностроения | Устройство для управления пуском ракет |
| US6845938B2 (en) * | 2001-09-19 | 2005-01-25 | Lockheed Martin Corporation | System and method for periodically adaptive guidance and control |
| RU2236666C2 (ru) * | 2002-09-30 | 2004-09-20 | Федеральное государственное унитарное предприятие "Научно-производственное предприятие "Рубин" | Аппаратура приема и реализации целеуказания |
| RU2311659C2 (ru) * | 2005-06-14 | 2007-11-27 | Санкт-Петербургское высшее училище радиоэлектроники ПВО | Радиолокационная система целеуказания |
| US7910867B1 (en) * | 2006-03-03 | 2011-03-22 | Lockheed Martin Corporation | Architecture for a launch controller |
| IL178840A0 (en) * | 2006-10-24 | 2007-09-20 | Rafael Advanced Defense Sys | System |
| JP5308189B2 (ja) * | 2009-02-25 | 2013-10-09 | 三菱重工業株式会社 | 飛しょう体発射装置 |
| US9803958B2 (en) * | 2012-02-22 | 2017-10-31 | Sikorsky Aircraft Corporation | Weapons stores processor panel for aircraft |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3987447A (en) * | 1965-06-21 | 1976-10-19 | The United States Of America As Represented By The Secretary Of The Navy | Missile command link with pulse deletion command coding |
| US4093153A (en) * | 1965-11-18 | 1978-06-06 | The United States Of America As Represented By The Secretary Of The Army | Ground-controlled guided-missile system |
| US3962537A (en) * | 1975-02-27 | 1976-06-08 | The United States Of America As Represented By The Secretary Of The Navy | Gun launched reconnaissance system |
| IL78757A0 (en) * | 1986-05-12 | 1986-08-31 | Israel State | Launcher for an optically guided,wire-controlled missile with improved electronic circuitry |
| FR2603695B1 (fr) * | 1986-09-09 | 1990-10-19 | Thomson Csf | Procede et dispositif de visualisation des cibles et/ou des positions des cibles utilisant des moyens d'acquisition des donnees d'un systeme d'armes |
-
1989
- 1989-12-07 US US07/447,320 patent/US5080300A/en not_active Expired - Lifetime
-
1990
- 1990-11-05 CA CA002029281A patent/CA2029281C/en not_active Expired - Fee Related
- 1990-11-06 IL IL9626390A patent/IL96263A/en not_active IP Right Cessation
- 1990-11-22 EP EP90312730A patent/EP0431804B1/en not_active Expired - Lifetime
- 1990-11-22 DE DE69023103T patent/DE69023103T2/de not_active Expired - Lifetime
- 1990-11-22 ES ES90312730T patent/ES2078320T3/es not_active Expired - Lifetime
- 1990-11-27 NO NO905129A patent/NO302317B1/no not_active IP Right Cessation
- 1990-11-29 TR TR90/1147A patent/TR26546A/xx unknown
- 1990-11-30 JP JP2336915A patent/JPH081359B2/ja not_active Expired - Lifetime
-
1996
- 1996-01-17 GR GR960400078T patent/GR3018677T3/el unknown
Also Published As
| Publication number | Publication date |
|---|---|
| CA2029281C (en) | 1995-07-04 |
| NO905129L (no) | 1991-06-10 |
| US5080300A (en) | 1992-01-14 |
| EP0431804A3 (en) | 1992-09-23 |
| DE69023103D1 (de) | 1995-11-23 |
| JPH03181798A (ja) | 1991-08-07 |
| TR26546A (tr) | 1995-03-15 |
| JPH081359B2 (ja) | 1996-01-10 |
| DE69023103T2 (de) | 1996-03-21 |
| GR3018677T3 (en) | 1996-04-30 |
| IL96263A (en) | 1995-05-26 |
| CA2029281A1 (en) | 1991-06-08 |
| NO905129D0 (no) | 1990-11-27 |
| EP0431804A2 (en) | 1991-06-12 |
| NO302317B1 (no) | 1998-02-16 |
| EP0431804B1 (en) | 1995-10-18 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG2A | Definitive protection |
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