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WO1996008688A1 - Systeme et procede permettant d'atteindre une cible dans un groupe de cibles - Google Patents

Systeme et procede permettant d'atteindre une cible dans un groupe de cibles Download PDF

Info

Publication number
WO1996008688A1
WO1996008688A1 PCT/US1995/012591 US9512591W WO9608688A1 WO 1996008688 A1 WO1996008688 A1 WO 1996008688A1 US 9512591 W US9512591 W US 9512591W WO 9608688 A1 WO9608688 A1 WO 9608688A1
Authority
WO
WIPO (PCT)
Prior art keywords
bomb
cluster
targets
location
flight
Prior art date
Application number
PCT/US1995/012591
Other languages
English (en)
Inventor
Rami Fabian
Original Assignee
State Of Israel - Ministry Of Defence Rafael - Armament Development Authority
Friedman, Mark, M.
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 State Of Israel - Ministry Of Defence Rafael - Armament Development Authority, Friedman, Mark, M. filed Critical State Of Israel - Ministry Of Defence Rafael - Armament Development Authority
Priority to AU39457/95A priority Critical patent/AU3945795A/en
Publication of WO1996008688A1 publication Critical patent/WO1996008688A1/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
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • F41G7/308—Details for guiding a plurality of missiles
    • 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
    • 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
    • F41G7/2233—Multimissile systems

Definitions

  • the present invention relates to systems and methods for targeting
  • one or more support vehicles or a column of tanks which may either be
  • the missiles have accuracies which are at least as good
  • a bomb including: (i) a navigational system for
  • the present invention successfully addresses the shortcomings of the
  • the present invention discloses a novel system and method which
  • the bomb guides itself to the vicinity of the cluster using
  • head homes in on a specific target from among the cluster of targets and
  • the present invention is of a system and method for hitting one or
  • Bomb 10 may be of various suitable type. Typically, bomb 10
  • an explosive warhead and a homing head which may include any
  • suitable transmitter/receiver units preferably one which operates using
  • Bomb 10 also includes various aerodynamics members, such as
  • bomb 10 includes a navigational system, which
  • GPS Global Position System
  • IMU Inertial Measurement Unit
  • INS Inertial Navigation System
  • Bomb 10 further includes suitable means for calculating the
  • Bomb 10 may be a gliding bomb so it is launched
  • bomb 10 or preferably a number of bombs 10, are launched from an attack
  • the intelligence can be obtained on the location of a cluster of targets 14.
  • Synthetic Aperture Radar mounted on attack aircraft 12 or on any combination
  • bomb 10 is fed the location of the cluster of targets.
  • bomb 10 continually receives or generates
  • navigational information as through its GPS receiver, IMU or INS as to
  • Bomb 10 uses the navigational information and the
  • Navigational system information continues to be received or
  • bomb 10 typically extends from launch until bomb 10 is approximately from about
  • the bomb homing head acquires the target
  • cluster and further trajectory corrections are based on homing head.
  • homing head of a specific bomb 10 selects a
  • homing head is divided into a number of sectors or a number of individual
  • bomb 10 reaches the vicinity of the targets, which for a typical launch from
  • bomb 10 The updating of bomb 10 is effected through the equipping of bomb
  • a suitable electromagnetic receiver preferably a UHF receiver
  • bomb 10 is approximately 2000 to 7000 meters ground distance from

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

Système et procédé permettant d'atteindre une cible dans un groupe de cibles (14). Le procédé consiste à obtenir des renseignements concernant l'emplacement du groupe de cibles (14), à transmettre ces renseignements, puis à lancer une bombe ou un missile (10) comprenant un système de navigation apte à fournir des informations concernant la position de la bombe ou du missile (10) au cours d'une première partie du vol de la bombe ou du missile (10), et un mécanisme de commande de la trajectoire de la bombe ou du missile (10) en fonction des informations concernant la position de la bombe ou du missile (10), et des renseignements concernant l'emplacement du groupe de cibles (14), et ce au cours de la première partie du vol de la bombe ou du missile (10). En outre, la bombe ou le missile (10) comprend un mécanisme permettant de sélectionner un secteur ou une cible au sein du groupe de cibles (14) au cours d'une partie ultérieure du vol, ainsi qu'un mécanisme permettant de commander la trajectoire de la bombe ou du missile (10) au cours de la partie ultérieure de son vol.
PCT/US1995/012591 1994-09-13 1995-09-06 Systeme et procede permettant d'atteindre une cible dans un groupe de cibles WO1996008688A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU39457/95A AU3945795A (en) 1994-09-13 1995-09-06 System and method for hitting a target in a cluster

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IL110960 1994-09-13
IL11096094A IL110960A0 (en) 1994-09-13 1994-09-13 System and method for hitting a target in a cluster

Publications (1)

Publication Number Publication Date
WO1996008688A1 true WO1996008688A1 (fr) 1996-03-21

Family

ID=11066553

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1995/012591 WO1996008688A1 (fr) 1994-09-13 1995-09-06 Systeme et procede permettant d'atteindre une cible dans un groupe de cibles

Country Status (3)

Country Link
AU (1) AU3945795A (fr)
IL (1) IL110960A0 (fr)
WO (1) WO1996008688A1 (fr)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2780154A1 (fr) * 1998-06-19 1999-12-24 Dassault Electronique Engin volant guide avec radionavigation gps et telecommande associee
US6196496B1 (en) 1998-06-29 2001-03-06 State Of Israel Ministry Of Defense Armament Development Authority Raeael Method for assigning a target to a missile
RU2212620C1 (ru) * 2002-04-09 2003-09-20 Григорьев Владимир Григорьевич Способ определения значений параметров траектории бомбы
FR2928452A1 (fr) * 2008-03-07 2009-09-11 Thales Sa Dispositif de conduite de tir bas cout sur cibles fixes et mobiles
WO2012125217A1 (fr) * 2011-03-17 2012-09-20 Raytheon Company Résolution de conflits d'armes aériennes guidées tirées en salve
RU2474843C1 (ru) * 2011-10-05 2013-02-10 Виктор Леонидович Семенов Рлс измерения мгновенной скорости пули
EP1989501A4 (fr) * 2006-03-01 2013-05-22 Raytheon Co Système d'interception de missiles balistiques ("multiple kill vehicle" ýmkv¨) comportant des véhicules d'interception autonomes
RU2484497C2 (ru) * 2011-07-21 2013-06-10 Виктор Леонидович Семенов Способ селекции малоразмерных целей и устройство для его реализации
RU2522426C2 (ru) * 2011-10-05 2014-07-10 Виктор Леонидович Семенов Способ измерения изменения скорости движения цели по дальности и устройства для его реализации
NO340726B1 (en) * 2015-08-12 2017-06-06 Kongsberg Defence & Aerospace As Method and system for planning and launching a plurality of missiles to be included in the same mission

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1000956A (fr) * 1949-12-02 1952-02-18 Raccord étanche pour fluides sous pression
DE2926215A1 (de) * 1978-07-11 1980-01-24 Chesini Snc Perfektioniertes verbindungsstueck mit kegeldichtung o.ae.
CH681558A5 (en) * 1991-04-16 1993-04-15 Tubex Ag Water supply pipe safety connection - includes fitting carrying sealing ring and incorporating locking lug or hooked lug engaging teeth on outer cap
DE4218347A1 (de) * 1992-06-04 1993-12-09 Mosmatic Ag Necker Sprührohr oder Sprühlanze eines Hochdruck-Reinigungsgerätes

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1000956A (fr) * 1949-12-02 1952-02-18 Raccord étanche pour fluides sous pression
DE2926215A1 (de) * 1978-07-11 1980-01-24 Chesini Snc Perfektioniertes verbindungsstueck mit kegeldichtung o.ae.
CH681558A5 (en) * 1991-04-16 1993-04-15 Tubex Ag Water supply pipe safety connection - includes fitting carrying sealing ring and incorporating locking lug or hooked lug engaging teeth on outer cap
DE4218347A1 (de) * 1992-06-04 1993-12-09 Mosmatic Ag Necker Sprührohr oder Sprühlanze eines Hochdruck-Reinigungsgerätes

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2780154A1 (fr) * 1998-06-19 1999-12-24 Dassault Electronique Engin volant guide avec radionavigation gps et telecommande associee
US6196496B1 (en) 1998-06-29 2001-03-06 State Of Israel Ministry Of Defense Armament Development Authority Raeael Method for assigning a target to a missile
RU2212620C1 (ru) * 2002-04-09 2003-09-20 Григорьев Владимир Григорьевич Способ определения значений параметров траектории бомбы
EP1989501A4 (fr) * 2006-03-01 2013-05-22 Raytheon Co Système d'interception de missiles balistiques ("multiple kill vehicle" ýmkv¨) comportant des véhicules d'interception autonomes
FR2928452A1 (fr) * 2008-03-07 2009-09-11 Thales Sa Dispositif de conduite de tir bas cout sur cibles fixes et mobiles
WO2009112424A3 (fr) * 2008-03-07 2009-11-26 Thales Dispositif de conduite de tir bas cout sur cibles fixes et mobiles
US8487226B2 (en) 2011-03-17 2013-07-16 Raytheon Company Deconfliction of guided airborne weapons fired in a salvo
WO2012125217A1 (fr) * 2011-03-17 2012-09-20 Raytheon Company Résolution de conflits d'armes aériennes guidées tirées en salve
RU2484497C2 (ru) * 2011-07-21 2013-06-10 Виктор Леонидович Семенов Способ селекции малоразмерных целей и устройство для его реализации
RU2474843C1 (ru) * 2011-10-05 2013-02-10 Виктор Леонидович Семенов Рлс измерения мгновенной скорости пули
RU2522426C2 (ru) * 2011-10-05 2014-07-10 Виктор Леонидович Семенов Способ измерения изменения скорости движения цели по дальности и устройства для его реализации
NO340726B1 (en) * 2015-08-12 2017-06-06 Kongsberg Defence & Aerospace As Method and system for planning and launching a plurality of missiles to be included in the same mission
US9958237B2 (en) 2015-08-12 2018-05-01 Kongsberg Defence & Aerospace As Method and system for planning and launching a plurality of missiles to be included in the same mission

Also Published As

Publication number Publication date
AU3945795A (en) 1996-03-29
IL110960A0 (en) 1995-07-31

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