ES2143575T3 - Guiamiento de arma combinando un radar de abertura sintetica por monoimpulsos y monoimpulsos inversos. - Google Patents
Guiamiento de arma combinando un radar de abertura sintetica por monoimpulsos y monoimpulsos inversos.Info
- Publication number
- ES2143575T3 ES2143575T3 ES95116920T ES95116920T ES2143575T3 ES 2143575 T3 ES2143575 T3 ES 2143575T3 ES 95116920 T ES95116920 T ES 95116920T ES 95116920 T ES95116920 T ES 95116920T ES 2143575 T3 ES2143575 T3 ES 2143575T3
- Authority
- ES
- Spain
- Prior art keywords
- weapon
- monoimpulsos
- target
- alternate
- guidance
- 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
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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
-
- 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
- G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
- G01S1/08—Systems for determining direction or position line
- G01S1/14—Systems for determining direction or position line using amplitude comparison of signals transmitted simultaneously from antennas or antenna systems having differently oriented overlapping directivity-characteristics
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/86—Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/89—Radar or analogous systems specially adapted for specific applications for mapping or imaging
- G01S13/90—Radar or analogous systems specially adapted for specific applications for mapping or imaging using synthetic aperture techniques, e.g. synthetic aperture radar [SAR] techniques
- G01S13/904—SAR modes
- G01S13/9092—SAR modes combined with monopulse techniques
Abstract
UN SISTEMA DE GUIADO DE ARMAS POR MONOIMPULSOS DE SAR Y MONOIMPULSOS INVERSOS (10) PARA GUIAR UN ARMA (13) A UN BLANCO (15) QUE CONSTA DE UNA PLATAFORMA DE LANZAMIENTO (11) Y DE UN RADAR DE APERTURA SINTETICA (12) DISPUESTO SOBRE LA PLATAFORMA DE LANZAMIENTO (11) PARA GENERAR UN MAPA DE MONOIMPULSOS RADARICOS DE APERTURA SINTETICA DE UN AREA QUE RODEA AL BLANCO (15), PARA SEÑALAR LA UBICACION DEL BLANCO (15), Y PARA TRANSMITIR UNA ILUMINACION POR MONOIMPULSOS INVERSOS QUE CONTIENE UNA SECUENCIA DE PATRONES DE DIFERENCIA DE ELEVACION Y ACIMUT SIMULTANEOS Y DE SUMA ALTERNOS CENTRADOS SOBRE EL BLANCO (15). EL ARMA (13) CONSTA DE UN SISTEMA DE GUIADO DEL ARMA Y DE UN PROYECTIL BUSCADOR DEL BLANCO RADARICO NO COHERENTE (14) QUE RESPONDE A LOS COMANDOS DE GUIADO TRASMITIDOS POR LA PLATAFORMA DE LANZAMIENTO (11), PARA RECIBIR LAS REFLEXIONES DEL PATRON DE DIFERENCIA DE ELEVACION Y ACIMUT COMBINADOS Y DE SUMA ALTERNOS DEL BLANCO (15), Y PARA UTILIZAR ESTAS REFLEXIONES PARA ADQUIRIR Y SEGUIR EL PATRON DE DIFERENCIA DE ELEVACION Y ACIMUT CERO SOBRE EL BLANCO (15) PARA ASI VOLAR SEGUN LA TRAYECTORIA OPTIMA AL BLANCO (15) (FIG.1). TAMBIEN SE PRESENTA UN METODO CORRESPONDIENTE PARA EL GUIADO DEL ARMA (13) AL BLANCO (15).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/332,004 US5473331A (en) | 1994-10-31 | 1994-10-31 | Combined SAR monopulse and inverse monopulse weapon guidance |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2143575T3 true ES2143575T3 (es) | 2000-05-16 |
Family
ID=23296294
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES95116920T Expired - Lifetime ES2143575T3 (es) | 1994-10-31 | 1995-10-27 | Guiamiento de arma combinando un radar de abertura sintetica por monoimpulsos y monoimpulsos inversos. |
Country Status (8)
Country | Link |
---|---|
US (1) | US5473331A (es) |
EP (1) | EP0709691B1 (es) |
JP (1) | JP2802052B2 (es) |
KR (1) | KR100186819B1 (es) |
AU (1) | AU677529B2 (es) |
CA (1) | CA2161044C (es) |
DE (1) | DE69515790T2 (es) |
ES (1) | ES2143575T3 (es) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5736956A (en) * | 1996-06-04 | 1998-04-07 | Hughes Electronics | Unlocked W-band receiver with coherent features |
US5742250A (en) * | 1996-08-29 | 1998-04-21 | Raytheon Company | Enhanced beamsplitting technique for use with three-dimensional synthetic array radar |
US5826819A (en) * | 1997-06-27 | 1998-10-27 | Raytheon Company | Weapon system employing a transponder bomb and guidance method thereof |
US5918305A (en) * | 1997-08-27 | 1999-06-29 | Trw Inc. | Imaging self-referencing tracker and associated methodology |
ES2149692B1 (es) * | 1998-06-10 | 2001-05-01 | Ingenieria Diseno Y Analisis S | Sistema de trayectografia por radar secundario para tiro con proyectiles de artilleria. |
FR2793885A1 (fr) * | 1999-05-17 | 2000-11-24 | Thomson Csf | Procede et dispositif de guidage electromagnetique, appliques notamment a la poursuite de cibles |
US6313784B1 (en) * | 2000-05-22 | 2001-11-06 | The United States Of America As Represented By The Secretary Of The Army | Millimeter-wave zoom antenna for guilding beamrider hypervelocity missile |
GB2430722B (en) * | 2001-09-26 | 2007-08-22 | Mbda Uk Ltd | A guidance system |
US6608584B1 (en) * | 2002-02-12 | 2003-08-19 | Raytheon Company | System and method for bistatic SAR image generation with phase compensation |
US6842138B1 (en) * | 2002-08-12 | 2005-01-11 | The United States Of America As Represented By The Secretary Of The Navy | Target designation system |
US6762710B2 (en) * | 2002-08-12 | 2004-07-13 | The United States Of America As Represented By The Secretary Of The Navy | Target designation system |
US6650277B1 (en) * | 2002-08-12 | 2003-11-18 | The United States Of America As Represented By The Secretary Of The Navy | Target designation system |
US7040570B2 (en) * | 2003-09-29 | 2006-05-09 | The United States Of America As Represented By The Secretary Of The Army | Weather-agile reconfigurable automatic target recognition system |
FR2879753B1 (es) * | 2004-12-22 | 2007-04-20 | Sagem | |
GB2450075A (en) * | 2007-03-08 | 2008-12-17 | Selex Sensors & Airborne Sys | Tracking device for guiding a flight vehicle towards a target |
US8354958B2 (en) | 2010-11-22 | 2013-01-15 | Raytheon Company | Alignment system |
US8274425B2 (en) * | 2010-12-29 | 2012-09-25 | Raytheon Company | Single channel semi-active radar seeker |
KR101213043B1 (ko) * | 2011-04-19 | 2012-12-18 | 국방과학연구소 | 탐지추적 레이더, 이를 구비한 고속 이동체 방어시스템 및 탐지추적 레이더의 고속 이동체 추적방법 |
US8610041B1 (en) * | 2011-05-23 | 2013-12-17 | Lockheed Martin Corporation | Missile tracking by GPS reflections |
CN110501704B (zh) * | 2019-07-16 | 2021-05-07 | 中国科学院电子学研究所 | 一种全极化图像极化分解方法、装置及存储介质 |
DE102020001157A1 (de) | 2020-02-21 | 2021-08-26 | Diehl Defence Gmbh & Co. Kg | Verfahren zur Zielführung eines Flugkörpers, Flugkörpersteuerung und Flugkörper |
DE102020001155A1 (de) | 2020-02-21 | 2021-08-26 | Diehl Defence Gmbh & Co. Kg | Steuerungsverfahren für einen Flugkörperradarsensor eines Flugkörpers, Flugkörpersteuereinheit und Flugkörper |
DE102020001153B4 (de) | 2020-02-21 | 2022-03-10 | Diehl Defence Gmbh & Co. Kg | Flugkörper, insbesondere Lenkflugkörper, mit einer Radarsensoreinheit |
CN111693979B (zh) * | 2020-05-25 | 2022-10-11 | 北京理工大学 | 一种基于泰勒展开的数字阵列单脉冲测角方法 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2685090A1 (fr) * | 1972-05-29 | 1993-06-18 | Raytheon Co | Dispositif radar de poursuites. |
US5173703A (en) * | 1980-12-29 | 1992-12-22 | Raytheon Company | All weather strike system (AWTSS) and method of operation |
US4501399A (en) * | 1981-07-20 | 1985-02-26 | The United States Of America As Represented By The Secretary Of The Army | Hybrid monopulse/sequential lobing beamrider guidance |
US4589610A (en) * | 1983-11-08 | 1986-05-20 | Westinghouse Electric Corp. | Guided missile subsystem |
DE3343604C2 (de) * | 1983-12-02 | 1986-05-22 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Verfahren und Einrichtung zum Bekämpfen von Bodenzielen mittels eines radargelenkten Flugkörpers |
DE3823814A1 (de) * | 1988-07-14 | 1990-02-01 | Messerschmitt Boelkow Blohm | Flugkoerperfuehrungssystem |
US5260709A (en) * | 1991-12-19 | 1993-11-09 | Hughes Aircraft Company | Autonomous precision weapon delivery using synthetic array radar |
US5424742A (en) * | 1992-12-31 | 1995-06-13 | Raytheon Company | Synthetic aperture radar guidance system and method of operating same |
US5344099A (en) * | 1993-04-12 | 1994-09-06 | The United States Of America As Represented By The Secretary Of The Army | Missile beamrider guidance using polarization-agile beams |
-
1994
- 1994-10-31 US US08/332,004 patent/US5473331A/en not_active Expired - Lifetime
-
1995
- 1995-10-20 CA CA002161044A patent/CA2161044C/en not_active Expired - Lifetime
- 1995-10-27 ES ES95116920T patent/ES2143575T3/es not_active Expired - Lifetime
- 1995-10-27 EP EP95116920A patent/EP0709691B1/en not_active Expired - Lifetime
- 1995-10-27 DE DE69515790T patent/DE69515790T2/de not_active Expired - Lifetime
- 1995-10-30 KR KR1019950038021A patent/KR100186819B1/ko active IP Right Grant
- 1995-10-31 AU AU34565/95A patent/AU677529B2/en not_active Expired
- 1995-10-31 JP JP7283418A patent/JP2802052B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH08210798A (ja) | 1996-08-20 |
KR100186819B1 (ko) | 1999-04-15 |
EP0709691A1 (en) | 1996-05-01 |
AU677529B2 (en) | 1997-04-24 |
AU3456595A (en) | 1996-05-23 |
KR960014966A (ko) | 1996-05-22 |
CA2161044A1 (en) | 1996-05-01 |
DE69515790T2 (de) | 2000-11-09 |
DE69515790D1 (de) | 2000-04-27 |
JP2802052B2 (ja) | 1998-09-21 |
EP0709691B1 (en) | 2000-03-22 |
CA2161044C (en) | 1999-02-09 |
US5473331A (en) | 1995-12-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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