WO2006067220A3 - Missile equipe d'un autodirecteur comportant une antenne de radar asynthese d'ouverture et procede deguidage associe - Google Patents

Missile equipe d'un autodirecteur comportant une antenne de radar asynthese d'ouverture et procede deguidage associe Download PDF

Info

Publication number
WO2006067220A3
WO2006067220A3 PCT/EP2005/057117 EP2005057117W WO2006067220A3 WO 2006067220 A3 WO2006067220 A3 WO 2006067220A3 EP 2005057117 W EP2005057117 W EP 2005057117W WO 2006067220 A3 WO2006067220 A3 WO 2006067220A3
Authority
WO
WIPO (PCT)
Prior art keywords
missile
autodirector
asynthesis
radar antenna
aperture radar
Prior art date
Application number
PCT/EP2005/057117
Other languages
English (en)
Other versions
WO2006067220A2 (fr
WO2006067220B1 (fr
Inventor
Marc Malot
Original Assignee
Sagem Defense Securite
Marc Malot
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 Sagem Defense Securite, Marc Malot filed Critical Sagem Defense Securite
Priority to EP05825298A priority Critical patent/EP1839009A2/fr
Publication of WO2006067220A2 publication Critical patent/WO2006067220A2/fr
Publication of WO2006067220A3 publication Critical patent/WO2006067220A3/fr
Publication of WO2006067220B1 publication Critical patent/WO2006067220B1/fr

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
    • F41G7/2246—Active homing systems, i.e. comprising both a transmitter and a receiver
    • 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
    • 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
    • G01S13/883—Radar or analogous systems specially adapted for specific applications for missile homing, autodirectors
    • 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
    • G01S13/9041—Squint mode

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • General Physics & Mathematics (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

L'invention concerne un missile (1) équipé d'un autodirecteur comportant une antenne (7) d'un radar à synthèse d'ouverture présentant une direction (70) principale de détection, caractérisé en ce que l'antenne est agencée par rapport au missile de sorte que la direction principale de l'antenne est fixe par rapport au missile et décalée d'un angle (β) constant par rapport à un axe longitudinal (6) du missile. L'invention concerne également un procédé de guidage en asservissement d'altitude du missile associé.
PCT/EP2005/057117 2004-12-22 2005-12-22 Missile equipe d'un autodirecteur comportant une antenne de radar asynthese d'ouverture et procede deguidage associe WO2006067220A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP05825298A EP1839009A2 (fr) 2004-12-22 2005-12-22 Missile equipe d'un autodirecteur comportant une antenne de radar a synthese d'ouverture et procede de guidage associe

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0413713 2004-12-22
FR0413713A FR2879753B1 (fr) 2004-12-22 2004-12-22

Publications (3)

Publication Number Publication Date
WO2006067220A2 WO2006067220A2 (fr) 2006-06-29
WO2006067220A3 true WO2006067220A3 (fr) 2006-08-24
WO2006067220B1 WO2006067220B1 (fr) 2006-11-02

Family

ID=35241216

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2005/057117 WO2006067220A2 (fr) 2004-12-22 2005-12-22 Missile equipe d'un autodirecteur comportant une antenne de radar asynthese d'ouverture et procede deguidage associe

Country Status (3)

Country Link
EP (1) EP1839009A2 (fr)
FR (1) FR2879753B1 (fr)
WO (1) WO2006067220A2 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011062765A2 (fr) 2009-11-17 2011-05-26 The Regents Of The University Of Michigan 1,4-benzodiazépine-2,5-diones et composés apparentés présentant des propriétés thérapeutiques
GB2509787B (en) 2013-01-15 2017-09-13 Mbda Uk Ltd A missile seeker and guidance method
FR3106902B1 (fr) * 2020-01-30 2022-01-07 Mbda France Système radioélectrique à réseaux d’antennes multiples et à formes d’onde adaptatives.

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3430888A1 (de) * 1984-08-22 1986-03-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Einrichtung zur detektion und bekaempfung untergezogener bodenziele
DE3540808A1 (de) * 1984-08-22 1987-05-21 Messerschmitt Boelkow Blohm Einrichtung zur detektion und bekaempfung untergezogener bodenziele
DE4309295A1 (de) * 1992-06-29 1995-10-05 Daimler Benz Aerospace Ag Verfahren zur eigenständigen Steuerung eines lenkbaren und mit einem Gefechtskopf versehenen Flugkörpers und Anordnung zur Durchführung des Verfahrens
US5473331A (en) * 1994-10-31 1995-12-05 Hughes Aircraft Company Combined SAR monopulse and inverse monopulse weapon guidance
US5826819A (en) * 1997-06-27 1998-10-27 Raytheon Company Weapon system employing a transponder bomb and guidance method thereof

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5755400A (en) * 1980-10-02 1998-05-26 Raytheon Company Inertial instrumentation correction technique
DE3114600A1 (de) * 1981-04-10 1982-11-04 Licentia Gmbh Verfahren und anordnung zur gelaendeueberwachung mit einem verschiessbaren sensor
DE3145374C2 (de) * 1981-11-14 1984-12-20 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren und Einrichtung zur Bekämpfung von Bodenzielen mittels Flugkörper
US5232182A (en) * 1982-10-27 1993-08-03 The United States Of America As Represented By The Secretary Of The Air Force Autonomous system for initializing synthetic aperture radar seeker acquisition

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3430888A1 (de) * 1984-08-22 1986-03-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Einrichtung zur detektion und bekaempfung untergezogener bodenziele
DE3540808A1 (de) * 1984-08-22 1987-05-21 Messerschmitt Boelkow Blohm Einrichtung zur detektion und bekaempfung untergezogener bodenziele
DE4309295A1 (de) * 1992-06-29 1995-10-05 Daimler Benz Aerospace Ag Verfahren zur eigenständigen Steuerung eines lenkbaren und mit einem Gefechtskopf versehenen Flugkörpers und Anordnung zur Durchführung des Verfahrens
US5473331A (en) * 1994-10-31 1995-12-05 Hughes Aircraft Company Combined SAR monopulse and inverse monopulse weapon guidance
US5826819A (en) * 1997-06-27 1998-10-27 Raytheon Company Weapon system employing a transponder bomb and guidance method thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP1839009A2 *

Also Published As

Publication number Publication date
WO2006067220A2 (fr) 2006-06-29
EP1839009A2 (fr) 2007-10-03
WO2006067220B1 (fr) 2006-11-02
FR2879753B1 (fr) 2007-04-20
FR2879753A1 (fr) 2006-06-23

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