WO2012146835A8 - Procédé de gestion automatique d'un autodirecteur monté sur un engin volant, en particulier sur un missile - Google Patents

Procédé de gestion automatique d'un autodirecteur monté sur un engin volant, en particulier sur un missile Download PDF

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Publication number
WO2012146835A8
WO2012146835A8 PCT/FR2012/000146 FR2012000146W WO2012146835A8 WO 2012146835 A8 WO2012146835 A8 WO 2012146835A8 FR 2012000146 W FR2012000146 W FR 2012000146W WO 2012146835 A8 WO2012146835 A8 WO 2012146835A8
Authority
WO
WIPO (PCT)
Prior art keywords
projectile
homing device
missile
device mounted
automatically managing
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.)
Ceased
Application number
PCT/FR2012/000146
Other languages
English (en)
Other versions
WO2012146835A1 (fr
Inventor
Francois DE PICCIOTTO
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MBDA France SAS
Original Assignee
MBDA France SAS
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 MBDA France SAS filed Critical MBDA France SAS
Priority to US14/113,519 priority Critical patent/US9234723B2/en
Priority to RU2013146844/28A priority patent/RU2595309C2/ru
Publication of WO2012146835A1 publication Critical patent/WO2012146835A1/fr
Priority to IL229036A priority patent/IL229036A/en
Anticipated expiration legal-status Critical
Publication of WO2012146835A8 publication Critical patent/WO2012146835A8/fr
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2253Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2273Homing guidance systems characterised by the type of waves
    • F41G7/2293Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

- L'engin volant (1 ) est pourvu d'un autodirecteur (2) du type à composants liés au bâti, qui présente une phase d'accrochage pendant laquelle il cherche à détecter une cible (C) et qui comprend une direction d'observation (3), ladite direction d'observation (3) étant fixe par rapport à l'engin volant (1 ) et étant dirigée selon l'axe longitudinal (4) de ce dernier, ledit engin volant (1 ) comportant de plus des moyens de commande (8) pour commander automatiquement ledit engin volant (1 ) de manière à faire décrire à son axe longitudinal (4), lors d'un vol, pendant la phase d'accrochage de l'autodirecteur (2), un cercle de rayon croissant en fonction du temps, et ceci jusqu'à la détection de la cible (C).
PCT/FR2012/000146 2011-04-28 2012-04-16 Procédé de gestion automatique d'un autodirecteur monté sur un engin volant, en particulier sur un missile Ceased WO2012146835A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US14/113,519 US9234723B2 (en) 2011-04-28 2012-04-16 Method for automatically managing a homing device mounted on a projectile, in particular on a missile
RU2013146844/28A RU2595309C2 (ru) 2011-04-28 2012-04-16 Способ автоматического управления головкой самонаведения, установленной на реактивном снаряде, в частности на ракете
IL229036A IL229036A (en) 2011-04-28 2013-10-23 A method of automatically managing a domestication facility consisting of a launchable element, in particular on a missile

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1101320A FR2974625B1 (fr) 2011-04-28 2011-04-28 Procede de gestion automatique d'un autodirecteur monte sur un engin volant, en particulier sur un missile
FR1101320 2011-04-28

Publications (2)

Publication Number Publication Date
WO2012146835A1 WO2012146835A1 (fr) 2012-11-01
WO2012146835A8 true WO2012146835A8 (fr) 2013-11-28

Family

ID=46017757

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2012/000146 Ceased WO2012146835A1 (fr) 2011-04-28 2012-04-16 Procédé de gestion automatique d'un autodirecteur monté sur un engin volant, en particulier sur un missile

Country Status (6)

Country Link
US (1) US9234723B2 (fr)
EP (1) EP2518433B8 (fr)
FR (1) FR2974625B1 (fr)
IL (1) IL229036A (fr)
RU (1) RU2595309C2 (fr)
WO (1) WO2012146835A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20170307334A1 (en) * 2016-04-26 2017-10-26 Martin William Greenwood Apparatus and System to Counter Drones Using a Shoulder-Launched Aerodynamically Guided Missile
JP6953532B2 (ja) * 2016-12-15 2021-10-27 ビーエイイー・システムズ・インフォメーション・アンド・エレクトロニック・システムズ・インテグレイション・インコーポレーテッド 軸外標的を検知するための誘導弾薬システム

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FR2692035B1 (fr) * 1980-11-07 1994-11-18 Telecommunications Sa Dispositif détecteur de proximité infrarouge pour engin volant et ensemble détecteur pour engin en autorotation incluant un tel dispositif.
US4427878A (en) * 1981-11-06 1984-01-24 Ford Aerospace & Communications Corporation Optical scanning apparatus incorporating counter-rotation of elements about a common axis by a common driving source
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DE19611595B4 (de) * 1996-03-23 2004-02-05 BODENSEEWERK GERäTETECHNIK GMBH Suchkopf für zielverfolgende Flugkörper oder Geschosse
US6626834B2 (en) * 2001-01-25 2003-09-30 Shane Dunne Spiral scanner with electronic control
RU2225975C1 (ru) * 2002-06-20 2004-03-20 Федеральное государственное унитарное предприятие "Государственное машиностроительное конструкторское бюро "Радуга" им. А.Я. Березняка" Крылатая ракета и способ ее боевого применения (варианты)
RU2253824C1 (ru) * 2004-04-05 2005-06-10 Открытое акционерное общество "Научно-исследовательский институт измерительных приборов" (ОАО "НИИИП") Способ наведения управляемой ракеты на воздушную цель (варианты) и радиолокационный комплекс для его реализации

Also Published As

Publication number Publication date
US20140042265A1 (en) 2014-02-13
US9234723B2 (en) 2016-01-12
IL229036A0 (en) 2013-12-31
EP2518433B1 (fr) 2015-04-15
EP2518433B8 (fr) 2015-05-20
EP2518433A1 (fr) 2012-10-31
FR2974625B1 (fr) 2013-05-17
WO2012146835A1 (fr) 2012-11-01
RU2595309C2 (ru) 2016-08-27
RU2013146844A (ru) 2015-06-10
FR2974625A1 (fr) 2012-11-02
IL229036A (en) 2017-09-28

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