DE10245496A1 - Leitsystem - Google Patents
Leitsystem Download PDFInfo
- Publication number
- DE10245496A1 DE10245496A1 DE10245496A DE10245496A DE10245496A1 DE 10245496 A1 DE10245496 A1 DE 10245496A1 DE 10245496 A DE10245496 A DE 10245496A DE 10245496 A DE10245496 A DE 10245496A DE 10245496 A1 DE10245496 A1 DE 10245496A1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft
- moving object
- radar
- desired location
- steering
- 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.)
- Withdrawn
Links
- 238000000034 method Methods 0.000 abstract 2
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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/12—Target-seeking control
-
- 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
-
- 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
- F41G7/30—Command link guidance systems
- F41G7/301—Details
- F41G7/303—Sighting or tracking devices especially provided for simultaneous observation of the target and of the missile
-
- 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
-
- 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
- G01S13/66—Radar-tracking systems; Analogous systems
- G01S13/72—Radar-tracking systems; Analogous systems for two-dimensional tracking, e.g. combination of angle and range tracking, track-while-scan radar
- G01S13/723—Radar-tracking systems; Analogous systems for two-dimensional tracking, e.g. combination of angle and range tracking, track-while-scan radar by using numerical data
-
- 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
-
- 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
-
- 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
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/02—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using radio waves
- G01S3/14—Systems for determining direction or deviation from predetermined direction
- G01S3/16—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived sequentially from receiving antennas or antenna systems having differently-oriented directivity characteristics or from an antenna system having periodically-varied orientation of directivity characteristic
- G01S3/20—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived sequentially from receiving antennas or antenna systems having differently-oriented directivity characteristics or from an antenna system having periodically-varied orientation of directivity characteristic derived by sampling signal received by an antenna system having periodically-varied orientation of directivity characteristic
-
- 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
- G01S13/93—Radar or analogous systems specially adapted for specific applications for anti-collision purposes
- G01S13/933—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft
- G01S13/935—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft for terrain-avoidance
-
- 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
- G01S13/02—Systems using reflection of radio waves, e.g. primary radar systems; Analogous systems
- G01S2013/0236—Special technical features
- G01S2013/0272—Multifunction radar
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Electromagnetism (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
Lenksystem zum Lenken eines beweglichen Objekts durch ein Luftfahrzeug, mit einem am Luftfahrzeug angeordneten Radar mit synthetischer Blende und Kommunikationsmitteln für die Kommunikation vom Luftfahrzeug zum beweglichen Objekt, wobei das Radar mit synthetischer Blende zum Bestimmen der Position und Orientierung des Luftfahrzeugs relativ zu einem gewünschten Ort in der Lage ist und von dem Radar bereitgestellte Information über die Kommunikationsmittel zum Lenken des beweglichen Objekts zu dem gewünschten Ort benutzt wird. Die Erfindung umfaßt ferner ein Lenksystem, bei welchem ein Sucher auf dem beweglichen Objekt vorgesehen ist, sowie ein Verfahren zum Lenken eines beweglichen Objekts von einem Luftfahrzeug aus zu einem gewünschten Ort mit Verwendung eines Radars mit synthetischer Blende zur Bestimmung der Position und/oder Orientierung des Luftfahrzeugs relativ zu einem gewünschten Ort, Erstellen einer Kommunikationsverbindung vom Luftfahrzeug mit dem beweglichen Objekt und Übertragung von Information zum beweglichen Objekt zum Lenken desselben zu dem gewünschten Ort, wobei auch ein auf dem beweglichen Objekt vorgesehener Sucher eingesetzt werden kann. Die Erfindung umfaßt weiter Verfahren zum Ausrichten eines Radarstrahls auf ein Ziel in einem Radarbild.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB0123638A GB0123638D0 (en) | 2001-09-26 | 2001-09-26 | A guidance system |
GB0205397A GB0205397D0 (en) | 2002-03-07 | 2002-03-07 | A guidance system |
Publications (1)
Publication Number | Publication Date |
---|---|
DE10245496A1 true DE10245496A1 (de) | 2007-05-16 |
Family
ID=36687545
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE10245496A Withdrawn DE10245496A1 (de) | 2001-09-26 | 2002-09-18 | Leitsystem |
Country Status (4)
Country | Link |
---|---|
US (1) | US7537181B2 (de) |
DE (1) | DE10245496A1 (de) |
FR (1) | FR2890760B1 (de) |
GB (6) | GB2430722B (de) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012022042A1 (de) * | 2012-11-09 | 2014-05-15 | Mbda Deutschland Gmbh | Kommunikationssystem mit Radarfunktion |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
IL154396A0 (de) * | 2002-12-29 | 2009-02-11 | Haim Niv | |
US8207480B2 (en) * | 2007-05-14 | 2012-06-26 | Raytheon Company | Methods and apparatus for fire control during launch of an effector |
US8178825B2 (en) * | 2007-10-29 | 2012-05-15 | Honeywell International Inc. | Guided delivery of small munitions from an unmanned aerial vehicle |
US8295548B2 (en) * | 2009-06-22 | 2012-10-23 | The Johns Hopkins University | Systems and methods for remote tagging and tracking of objects using hyperspectral video sensors |
DE102011010987A1 (de) * | 2010-03-24 | 2011-09-29 | Lfk-Lenkflugkörpersysteme Gmbh | Navigationsverfahren für einen Flugkörper |
DE102010022728A1 (de) * | 2010-06-04 | 2011-12-08 | Diehl Bgt Defence Gmbh & Co. Kg | Verfahren zum Einweisen eines Flugkörpers auf ein Ziel |
US8487807B2 (en) * | 2010-06-28 | 2013-07-16 | Institut National D'optique | Synthetic aperture imaging interferometer |
CA2802784C (en) | 2010-06-28 | 2016-03-15 | Institut National D'optique | Method and apparatus for compensating for a parameter change in a synthetic aperture imaging system |
US8567077B2 (en) * | 2011-10-20 | 2013-10-29 | Raytheon Company | Laser tracker system and technique for antenna boresight alignment |
DE102012002067A1 (de) * | 2012-02-03 | 2013-08-08 | Eads Deutschland Gmbh | Luft-Boden-Überwachungs- und/oder Wirksystem und Verfahren zur luftgestützten Inspektion und/oder Bekämpfung von auf dem Land oder auf See befindlichen Objekten |
CN102707726B (zh) * | 2012-05-28 | 2014-03-26 | 北京航空航天大学 | 一种无人机目标定位方法 |
DE102012012898B4 (de) * | 2012-06-28 | 2017-01-12 | Tesat-Spacecom Gmbh & Co.Kg | System und Verfahren zur Positionsbestimmung einer Kommunikationsplattform |
RU2506523C1 (ru) * | 2012-08-02 | 2014-02-10 | Алексей Вячеславович Бытьев | Способ управления вооружением зенитного ракетно-пушечного комплекса |
RU2525650C2 (ru) * | 2012-11-02 | 2014-08-20 | Открытое акционерное общество "Научно-производственное предприятие "Радар ммс" | Способ наведения летательных аппаратов на наземные объекты |
CN104076361B (zh) * | 2014-07-04 | 2017-03-08 | 西安电子科技大学 | 无人机载战场监视雷达超分辨广域成像方法 |
US20160349746A1 (en) * | 2015-05-29 | 2016-12-01 | Faro Technologies, Inc. | Unmanned aerial vehicle having a projector and being tracked by a laser tracker |
CN105004266A (zh) * | 2015-06-26 | 2015-10-28 | 哈尔滨工程大学 | 一种具有滤波器的多管火箭射击精度测量仪 |
WO2017068331A1 (en) * | 2015-10-20 | 2017-04-27 | Mbda Uk Limited | Improvements in and relating to missile targeting |
CN105867426B (zh) * | 2016-04-11 | 2018-08-21 | 西北工业大学 | 针对移动目标的飞机自动投放物资引导方法 |
WO2018080609A2 (en) | 2016-07-29 | 2018-05-03 | Remote Sensing Solutions, Inc. | Mobile radar for visualizing topography |
US10690766B2 (en) * | 2017-03-06 | 2020-06-23 | Government Of The United States, As Represented By The Secretary Of The Air Force | Biometric authentication using wideband UHF/VHF radar |
US11555679B1 (en) | 2017-07-07 | 2023-01-17 | Northrop Grumman Systems Corporation | Active spin control |
US11578956B1 (en) | 2017-11-01 | 2023-02-14 | Northrop Grumman Systems Corporation | Detecting body spin on a projectile |
RU2733329C1 (ru) * | 2019-11-22 | 2020-10-01 | Акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" | Способ расчета установок стрельбы управляемым снарядом с лазерной полуактивной головкой самонаведения в условиях облачности |
WO2021168819A1 (zh) * | 2020-02-28 | 2021-09-02 | 深圳市大疆创新科技有限公司 | 无人机的返航控制方法和设备 |
US11222245B2 (en) * | 2020-05-29 | 2022-01-11 | Raytheon Company | Systems and methods for feature extraction and artificial decision explainability |
US11573069B1 (en) | 2020-07-02 | 2023-02-07 | Northrop Grumman Systems Corporation | Axial flux machine for use with projectiles |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
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US2950477A (en) | 1955-08-12 | 1960-08-23 | Frederick C Alpers | System for synchronization and range measurement with a semiactive radar guided missile |
US3856237A (en) | 1964-10-06 | 1974-12-24 | Fairchild Hiller Corp | Guidance system |
US4163231A (en) * | 1968-01-03 | 1979-07-31 | Raytheon Company | Radar mapping technique |
US4442431A (en) * | 1971-07-12 | 1984-04-10 | Hughes Aircraft Company | Airborne missile guidance system |
US3778007A (en) * | 1972-05-08 | 1973-12-11 | Us Navy | Rod television-guided drone to perform reconnaissance and ordnance delivery |
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 |
US4549184A (en) * | 1981-06-09 | 1985-10-22 | Grumman Aerospace Corporation | Moving target ordnance control |
DE3403558A1 (de) | 1984-02-02 | 1985-08-08 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Einrichtung zur fernlenkung eines flugkoerpers |
GB2305566B (en) | 1989-01-27 | 1998-01-07 | British Aerospace | Navigational Systems |
GB2279529B (en) * | 1989-05-18 | 1995-05-31 | Plessey Co Plc | Radar |
US5473331A (en) * | 1994-10-31 | 1995-12-05 | Hughes Aircraft Company | Combined SAR monopulse and inverse monopulse weapon guidance |
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 |
US5982319A (en) | 1998-03-12 | 1999-11-09 | Northrop Grumman Corporation | UHF synthetic aperture radar |
-
2002
- 2002-09-16 GB GB0222199A patent/GB2430722B/en not_active Expired - Fee Related
- 2002-09-18 DE DE10245496A patent/DE10245496A1/de not_active Withdrawn
- 2002-09-18 FR FR0211568A patent/FR2890760B1/fr not_active Expired - Fee Related
- 2002-09-25 US US10/265,098 patent/US7537181B2/en not_active Expired - Fee Related
-
2005
- 2005-09-30 GB GB0520356A patent/GB2430823B/en not_active Expired - Fee Related
- 2005-09-30 GB GB0520358A patent/GB2430825A/en not_active Withdrawn
- 2005-09-30 GB GB0520355A patent/GB2430723A/en not_active Withdrawn
- 2005-09-30 GB GB0520357A patent/GB2430824B/en not_active Expired - Fee Related
- 2005-09-30 GB GB0520354A patent/GB2430822B/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012022042A1 (de) * | 2012-11-09 | 2014-05-15 | Mbda Deutschland Gmbh | Kommunikationssystem mit Radarfunktion |
Also Published As
Publication number | Publication date |
---|---|
GB0520357D0 (en) | 2006-07-05 |
FR2890760B1 (fr) | 2014-06-27 |
GB2430823A (en) | 2007-04-04 |
GB0520358D0 (en) | 2006-07-05 |
GB2430822B (en) | 2007-08-22 |
GB0520356D0 (en) | 2006-07-05 |
US7537181B2 (en) | 2009-05-26 |
GB2430722B (en) | 2007-08-22 |
US20080012751A1 (en) | 2008-01-17 |
GB2430722A (en) | 2007-04-04 |
GB2430723A (en) | 2007-04-04 |
GB2430824A (en) | 2007-04-04 |
GB2430822A (en) | 2007-04-04 |
GB2430825A (en) | 2007-04-04 |
GB0520355D0 (en) | 2006-07-05 |
GB2430824B (en) | 2007-08-22 |
FR2890760A1 (fr) | 2007-03-16 |
GB0222199D0 (en) | 2006-07-05 |
GB0520354D0 (en) | 2006-07-05 |
GB2430823B (en) | 2007-08-22 |
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R119 | Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee | ||
R011 | All appeals rejected, refused or otherwise settled |