ES2098433T3 - Suelta de arma de precision autonoma que emplea un radar de red sintetica. - Google Patents
Suelta de arma de precision autonoma que emplea un radar de red sintetica.Info
- Publication number
- ES2098433T3 ES2098433T3 ES92121647T ES92121647T ES2098433T3 ES 2098433 T3 ES2098433 T3 ES 2098433T3 ES 92121647 T ES92121647 T ES 92121647T ES 92121647 T ES92121647 T ES 92121647T ES 2098433 T3 ES2098433 T3 ES 2098433T3
- Authority
- ES
- Spain
- Prior art keywords
- missile
- radar
- platform
- flight path
- calculation
- 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
- 238000004364 calculation method Methods 0.000 abstract 3
- 238000000034 method Methods 0.000 abstract 2
- 230000035939 shock Effects 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
- F41G7/007—Preparatory measures taken before the launching of the guided 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
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data
- F41G7/346—Direction control systems for self-propelled missiles based on predetermined target position data using global navigation satellite systems, e.g. GPS, GALILEO, GLONASS
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data
- F41G7/36—Direction control systems for self-propelled missiles based on predetermined target position data using inertial references
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Computer Networks & Wireless Communication (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar Systems Or Details Thereof (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Navigation (AREA)
- Complex Calculations (AREA)
- Feedback Control In General (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
UN SISTEMA (10) Y UN METODO QUE HACE USO DE UN CALCULO DIFERENCIAL DE LA POSICION RELATIVA A UN SISTEMA DE COORDENADAS DE UN SISTEMA DE POSICIONAMIENTO GLOBAL (GPS) (12) Y DEL CALCULO DE UNA TRAYECTORIA OPTIMA DE VUELO DEL MISIL (19) PARA GUIAR A UN MISIL (14) HACIA UN BLANCO FIJO, INMOVIL O RELOCALIZABLE (15). EL SISTEMA (10) CONSTA DE UNA PLATAFORMA AEROPORTADA (13) QUE UTILIZA UN SUBSISTEMA DE NAVEGACION QUE UTILIZA EL SISTEMA SATELITE GPS (12) PARA PROPORCIONAR EL SISTEMA DE COORDENADAS Y UN RADAR CON UN SISTEMA DE RED DE ANTENAS SINTETICO (SAR) (16) PARA LOCALIZAR LOS BLANCOS DESEADOS (15). LA LOCALIZACION DEL BLANCO SE HACE ANTES DE LANZAR EL MISIL, POR LO QUE EL MISIL (14) SOLO NECESITA UN SUBSISTEMA DE NAVEGACION QUE TAMBIEN UTILIZA EL SISTEMA SATELITE GPS (12) PARA PROPORCIONAR EL MISMO SISTEMA DE COORDENADAS QUE EL UTILIZADO POR LA PLATAFORMA, UNA CABEZA DE COMBATE Y UN SISTEMA DE PROPULSION (SOLO PARA MISILES PROPULSADOS). ESTO DA COMO RESULTADO UN MISIL MUY BARATO CON CAPACIDADDE LANZAMIENTO Y DE SALIDA (AUTONOMA). EL SISTEMA DE CALCULO UTILIZADO EN LA PLATAFORMA UTILIZA VARIAS MEDIDAS TOMADAS POR RADAR (18) SEPARADAS EN MUCHOS GRADOS. CUANTAS MAS MEDIDAS SE TOMEN, MAYOR SERA LA PRECISION. EL ALGORITMO DE COMPUTO UTILIZA LAS MEDIDAS TOMADAS POR EL RADAR (18) PARA DETERMINAR EL PUNTO EN UN PLANO DONDE SE PIENSA QUE ESTA EL BLANCO (15) Y LA TRAYECTORIA OPTIMA DE VUELO (19) A TRAVES DE ESE PUNTO. AL MISIL (14) SE LE HACE VOLAR A LO LARGO DE LA TRAYECTORIA OPTIMA DE VUELO (19) Y EL CHOQUE CON LA TIERRA DA COMO RESULTADO UN CEP MUY BUENO CUANDO SE TOMAN UN NUMERO SUFICIENTE DE MEDIDAS CON EL RADAR (18). LA PRESENTE INVENCION PROPORCIONA UN SISTEMA DE ENVIO DE MISILES DE GRAN PRECISION, AUTONOMO Y PARA TODO TIEMPO AL TIEMPO QUE EL PRECIO RESULTA RELATIVAMENTE BAJO. EL PODER GUIAR LOS MISILES CON GRAN PRECISION SE CONSIGUE MEDIANTE LA TECNICA DE GUIA DIFERENCIAL UNICA (SI SE UTILIZA UN SISTEMA DE NAVEGACION LO SUFICIENTEMENTE PRECISO Y ESTABLE).
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/810,630 US5260709A (en) | 1991-12-19 | 1991-12-19 | Autonomous precision weapon delivery using synthetic array radar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2098433T3 true ES2098433T3 (es) | 1997-05-01 |
Family
ID=25204290
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES92121647T Expired - Lifetime ES2098433T3 (es) | 1991-12-19 | 1992-12-18 | Suelta de arma de precision autonoma que emplea un radar de red sintetica. |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US5260709A (es) |
| EP (1) | EP0547637B1 (es) |
| JP (1) | JP2525539B2 (es) |
| KR (1) | KR960014821B1 (es) |
| AU (1) | AU640091B1 (es) |
| CA (1) | CA2085847C (es) |
| DE (1) | DE69218143T2 (es) |
| ES (1) | ES2098433T3 (es) |
| IL (1) | IL104181A (es) |
Families Citing this family (68)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0583972A1 (en) * | 1992-08-17 | 1994-02-23 | Texas Instruments Incorporated | Improvements in and relating to precision targeting |
| US5344105A (en) * | 1992-09-21 | 1994-09-06 | Hughes Aircraft Company | Relative guidance using the global positioning system |
| DE4234878C2 (de) * | 1992-10-16 | 1995-03-30 | Deutsche Aerospace | Verfahren zur autonomen Lagesteuerung von Lenkflugkörpern |
| US5424742A (en) * | 1992-12-31 | 1995-06-13 | Raytheon Company | Synthetic aperture radar guidance system and method of operating same |
| US5430445A (en) * | 1992-12-31 | 1995-07-04 | Raytheon Company | Synthetic aperture radar guidance system and method of operating same |
| DE4325218C2 (de) * | 1993-07-28 | 1998-10-22 | Diehl Stiftung & Co | Artillerie-Rakete und Verfahren zur Leistungssteigerung einer Artillerie-Rakete |
| US5432520A (en) * | 1993-10-18 | 1995-07-11 | Hughes Aircraft Company | SAR/GPS inertial method of range measurement |
| US5424743A (en) * | 1994-06-01 | 1995-06-13 | U.S. Department Of Energy | 2-D weighted least-squares phase unwrapping |
| US5657947A (en) * | 1994-08-24 | 1997-08-19 | Loral Corp. | Precision guidance system for aircraft launched bombs |
| US5473331A (en) * | 1994-10-31 | 1995-12-05 | Hughes Aircraft Company | Combined SAR monopulse and inverse monopulse weapon guidance |
| US5647558A (en) * | 1995-02-14 | 1997-07-15 | Bofors Ab | Method and apparatus for radial thrust trajectory correction of a ballistic projectile |
| US5554994A (en) * | 1995-06-05 | 1996-09-10 | Hughes Missile Systems Company | Self-surveying relative GPS (global positioning system) weapon guidance system |
| US5832187A (en) | 1995-11-03 | 1998-11-03 | Lemelson Medical, Education & Research Foundation, L.P. | Fire detection systems and methods |
| US5809457A (en) * | 1996-03-08 | 1998-09-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Inertial pointing and positioning system |
| DE19703736C2 (de) * | 1996-03-22 | 1998-04-09 | Joao R Dr Ing Moreira | Verfahren zur Automatisierung eines Radars mit synthetischer Apertur (SAR) und zur Flugführung eines Trägers sowie Einrichtung zur Durchführung des Verfahrens |
| WO2000003193A1 (en) * | 1998-07-09 | 2000-01-20 | Raytheon Company | Geographically limited missile |
| US6237496B1 (en) | 1997-02-26 | 2001-05-29 | Northrop Grumman Corporation | GPS guided munition |
| US5943009A (en) * | 1997-02-27 | 1999-08-24 | Abbott; Anthony Steven | GPS guided munition |
| US5963653A (en) * | 1997-06-19 | 1999-10-05 | Raytheon Company | Hierarchical information fusion object recognition system and method |
| US6142411A (en) * | 1997-06-26 | 2000-11-07 | Cobleigh; Nelson E. | Geographically limited missile |
| US6021374A (en) * | 1997-10-09 | 2000-02-01 | Mcdonnell Douglas Corporation | Stand alone terrain conflict detector and operating methods therefor |
| WO1999061933A2 (en) * | 1998-04-16 | 1999-12-02 | Raytheon Company | Airborne gps guidance system for defeating multiple jammers |
| DE19828644C2 (de) * | 1998-06-26 | 2001-12-06 | Lfk Gmbh | Verfahren zum ferngesteuerten Bekämpfen bodennaher und/oder bodengebundener Ziele |
| US6157875A (en) * | 1998-07-17 | 2000-12-05 | The United States Of America As Represented By The Secretary Of The Navy | Image guided weapon system and method |
| US6166679A (en) | 1999-01-13 | 2000-12-26 | Lemelson Jerome H. | Friend or foe detection system and method and expert system military action advisory system and method |
| IL135449A (en) | 2000-04-04 | 2003-04-10 | Frucht Yaacov | Method and system for guiding submunitions |
| IL136566A (en) * | 2000-06-05 | 2007-07-24 | Rafael Advanced Defense Sys | Method for adjusting an inertial measurement unit in the presence of delays in unknown aircraft measurements |
| GB0117541D0 (en) * | 2001-07-19 | 2003-08-06 | Bae Systems Plc | Automatic registration of images in digital terrain elevation data |
| US6573486B1 (en) * | 2002-02-22 | 2003-06-03 | Northrop Grumman Corporation | Projectile guidance with accelerometers and a GPS receiver |
| US6691947B2 (en) * | 2002-03-12 | 2004-02-17 | The Boeing Company | Repetitive image targeting system |
| EP1570289A4 (en) * | 2002-11-15 | 2008-01-23 | Lockheed Corp | PRECISION GUIDANCE AND NAVIGATION SYSTEM FOR ALL WEATHER POSITIONS |
| US6919840B2 (en) * | 2002-11-21 | 2005-07-19 | Alliant Techsystems Inc. | Integration of a semi-active laser seeker into the DSU-33 proximity sensor |
| US6779752B1 (en) * | 2003-03-25 | 2004-08-24 | Northrop Grumman Corporation | Projectile guidance with accelerometers and a GPS receiver |
| US6883747B2 (en) * | 2003-03-28 | 2005-04-26 | Northrop Grumman Corporation | Projectile guidance with accelerometers and a GPS receiver |
| US6796213B1 (en) * | 2003-05-23 | 2004-09-28 | Raytheon Company | Method for providing integrity bounding of weapons |
| GB2402825B (en) * | 2003-06-12 | 2007-02-14 | Anthony Michael O'doherty | Monitoring system and method |
| US7032857B2 (en) * | 2003-08-19 | 2006-04-25 | Cuong Tu Hua | Multi-sensor guidance system for extreme force launch shock applications |
| US7121183B2 (en) * | 2004-03-29 | 2006-10-17 | Honeywell International Inc. | Methods and systems for estimating weapon effectiveness |
| IL163450A (en) * | 2004-08-10 | 2009-12-24 | Rafael Advanced Defense Sys | Guided missile with distributed guidance mechanism |
| US20060071849A1 (en) * | 2004-09-30 | 2006-04-06 | Lockheed Martin Corporation | Tactical all weather precision guidance and navigation system |
| US7121502B2 (en) * | 2005-01-26 | 2006-10-17 | Raytheon Company | Pseudo GPS aided multiple projectile bistatic guidance |
| US7834300B2 (en) * | 2005-02-07 | 2010-11-16 | Bae Systems Information And Electronic Systems Integration Inc. | Ballistic guidance control for munitions |
| US8450668B2 (en) * | 2005-02-07 | 2013-05-28 | Bae Systems Information And Electronic Systems Integration Inc. | Optically guided munition control system and method |
| WO2006088687A1 (en) * | 2005-02-07 | 2006-08-24 | Bae Systems Information And Electronic Systems Integration Inc. | Optically guided munition |
| US7503521B2 (en) * | 2005-02-07 | 2009-03-17 | Bae Systems Information And Electronic Systems Integration Inc. | Radiation homing tag |
| WO2006086532A2 (en) * | 2005-02-07 | 2006-08-17 | Bae Systems Information And Electronic Systems | Three axis aerodynamic control of guided munitions |
| US7728264B2 (en) * | 2005-10-05 | 2010-06-01 | Raytheon Company | Precision targeting |
| US8084724B1 (en) | 2006-02-01 | 2011-12-27 | Raytheon Company | Enhanced multiple kill vehicle (MKV) interceptor for intercepting exo and endo-atmospheric targets |
| US7494090B2 (en) * | 2006-03-01 | 2009-02-24 | Raytheon Company | Multiple kill vehicle (MKV) interceptor with autonomous kill vehicles |
| WO2009104015A2 (en) * | 2008-02-21 | 2009-08-27 | Mbda Uk Limited | Missile training system |
| DE102008017975A1 (de) * | 2008-04-10 | 2009-10-15 | Lfk-Lenkflugkörpersysteme Gmbh | Unbemannter Flugkörper und Verfahren zur Flugführung |
| US8558153B2 (en) * | 2009-01-23 | 2013-10-15 | Raytheon Company | Projectile with inertial sensors oriented for enhanced failure detection |
| US8076622B1 (en) * | 2009-08-31 | 2011-12-13 | Rockwell Collins, Inc. | Low profile, conformal global positioning system array for artillery |
| DE102011010987A1 (de) * | 2010-03-24 | 2011-09-29 | Lfk-Lenkflugkörpersysteme Gmbh | Navigationsverfahren für einen Flugkörper |
| US8237096B1 (en) | 2010-08-19 | 2012-08-07 | Interstate Electronics Corporation, A Subsidiary Of L-3 Communications Corporation | Mortar round glide kit |
| US8610041B1 (en) * | 2011-05-23 | 2013-12-17 | Lockheed Martin Corporation | Missile tracking by GPS reflections |
| US8525088B1 (en) * | 2012-03-21 | 2013-09-03 | Rosemont Aerospace, Inc. | View-point guided weapon system and target designation method |
| US8513580B1 (en) * | 2012-06-26 | 2013-08-20 | The United States Of America As Represented By The Secretary Of The Navy | Targeting augmentation for short-range munitions |
| KR101362911B1 (ko) * | 2012-11-09 | 2014-02-18 | 한국항공우주산업 주식회사 | 항공기에 탑재된 합성개구레이더를 구동하는 ofp시스템 및 그 제어방법 |
| IL227982B (en) * | 2013-08-15 | 2018-11-29 | Rafael Advanced Defense Systems Ltd | Missile system with navigation capability based on image processing |
| US10571224B2 (en) * | 2015-05-04 | 2020-02-25 | Propagation Research Associates, Inc. | Systems, methods and computer-readable media for improving platform guidance or navigation using uniquely coded signals |
| US10387727B2 (en) | 2017-09-13 | 2019-08-20 | Wing Aviation Llc | Backup navigation system for unmanned aerial vehicles |
| CN111077767B (zh) * | 2019-12-12 | 2021-11-30 | 南京航空航天大学 | 一种卫星星座组网同轨道面扩容重构的控制方法 |
| US11018705B1 (en) | 2020-07-17 | 2021-05-25 | Propagation Research Associates, Inc. | Interference mitigation, target detection, location and measurement using separable waveforms transmitted from spatially separated antennas |
| CN113075653B (zh) * | 2021-03-26 | 2022-11-29 | 北京理工大学 | 一种飞行器的导航方法及系统 |
| US11913757B2 (en) * | 2022-01-18 | 2024-02-27 | Rosemount Aerospace Inc. | Constraining navigational drift in a munition |
| US12375117B2 (en) * | 2022-10-17 | 2025-07-29 | Propagation Research Associates Llc | Coordinate frame projection using multiple unique signals transmitted from a localized array of spatially distributed antennas |
| CN119245437B (zh) * | 2024-02-29 | 2025-12-26 | 北京理工大学 | 一种具有时空约束的巡飞弹中制导方法 |
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| US4315609A (en) * | 1971-06-16 | 1982-02-16 | The United States Of America As Represented By The Secretary Of The Navy | Target locating and missile guidance system |
| US4204210A (en) * | 1972-09-15 | 1980-05-20 | The United States Of America As Represented By The Secretary Of The Air Force | Synthetic array radar command air launched missile system |
| US4179693A (en) * | 1977-05-23 | 1979-12-18 | Rockwell Internation Corporation | Autonomous, check-pointing, navigational system for an airborne vehicle |
| US5175554A (en) * | 1980-12-29 | 1992-12-29 | Raytheon Company | All weather tactical strike system (AWTSS) and method of operation |
| US4495580A (en) * | 1981-03-30 | 1985-01-22 | E-Systems, Inc. | Navigation system |
| US4825213A (en) * | 1981-05-15 | 1989-04-25 | Grumman Aerospace Corporation | Simultaneous triple aperture radar |
| US4549184A (en) * | 1981-06-09 | 1985-10-22 | Grumman Aerospace Corporation | Moving target ordnance control |
| DE3145374C2 (de) * | 1981-11-14 | 1984-12-20 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verfahren und Einrichtung zur Bekämpfung von Bodenzielen mittels Flugkörper |
| DE3301613A1 (de) * | 1983-01-19 | 1984-07-19 | Standard Elektrik Lorenz Ag, 7000 Stuttgart | Positionsbestimmungssystem |
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| US4741245A (en) * | 1986-10-03 | 1988-05-03 | Dkm Enterprises | Method and apparatus for aiming artillery with GPS NAVSTAR |
| US4783744A (en) * | 1986-12-08 | 1988-11-08 | General Dynamics, Pomona Division | Self-adaptive IRU correction loop design interfacing with the target state estimator for multi-mode terminal handoff |
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| DE3915633A1 (de) * | 1989-05-12 | 1990-11-15 | Dornier Luftfahrt | Verfahren zur navigation |
| US4914734A (en) * | 1989-07-21 | 1990-04-03 | The United States Of America As Represented By The Secretary Of The Air Force | Intensity area correlation addition to terrain radiometric area correlation |
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| DE3932548A1 (de) * | 1989-09-29 | 1991-04-11 | Telefunken Systemtechnik | Verfahren und vorrichtung fuer eine torpedozielsteuerung |
| US4959656A (en) * | 1989-10-31 | 1990-09-25 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Efficient detection and signal parameter estimation with application to high dynamic GPS receiver |
-
1991
- 1991-12-19 US US07/810,630 patent/US5260709A/en not_active Expired - Lifetime
-
1992
- 1992-12-18 IL IL10418192A patent/IL104181A/en not_active IP Right Cessation
- 1992-12-18 ES ES92121647T patent/ES2098433T3/es not_active Expired - Lifetime
- 1992-12-18 CA CA002085847A patent/CA2085847C/en not_active Expired - Lifetime
- 1992-12-18 DE DE69218143T patent/DE69218143T2/de not_active Expired - Lifetime
- 1992-12-18 EP EP92121647A patent/EP0547637B1/en not_active Expired - Lifetime
- 1992-12-19 KR KR1019920024847A patent/KR960014821B1/ko not_active Expired - Lifetime
- 1992-12-21 JP JP4356214A patent/JP2525539B2/ja not_active Expired - Lifetime
- 1992-12-21 AU AU30326/92A patent/AU640091B1/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| DE69218143T2 (de) | 1997-10-09 |
| EP0547637A1 (en) | 1993-06-23 |
| JP2525539B2 (ja) | 1996-08-21 |
| IL104181A (en) | 1995-12-31 |
| EP0547637B1 (en) | 1997-03-12 |
| JPH0688698A (ja) | 1994-03-29 |
| CA2085847A1 (en) | 1993-06-20 |
| US5260709A (en) | 1993-11-09 |
| KR960014821B1 (ko) | 1996-10-21 |
| CA2085847C (en) | 1996-12-03 |
| AU640091B1 (en) | 1993-08-12 |
| DE69218143D1 (de) | 1997-04-17 |
| KR930013756A (ko) | 1993-07-22 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG2A | Definitive protection |
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