CA2134578A1 - Systeme de defense antiaerien et missile de defense pour un tel systeme - Google Patents

Systeme de defense antiaerien et missile de defense pour un tel systeme

Info

Publication number
CA2134578A1
CA2134578A1 CA002134578A CA2134578A CA2134578A1 CA 2134578 A1 CA2134578 A1 CA 2134578A1 CA 002134578 A CA002134578 A CA 002134578A CA 2134578 A CA2134578 A CA 2134578A CA 2134578 A1 CA2134578 A1 CA 2134578A1
Authority
CA
Canada
Prior art keywords
missile
defense
trajectory
air
seeker
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.)
Granted
Application number
CA002134578A
Other languages
English (en)
Other versions
CA2134578C (fr
Inventor
Pierre Laures
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.)
Airbus Group SAS
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of CA2134578A1 publication Critical patent/CA2134578A1/fr
Application granted granted Critical
Publication of CA2134578C publication Critical patent/CA2134578C/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • F41G7/2273—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
    • F41G7/22—Homing guidance systems
    • F41G7/2206—Homing guidance systems using a remote control station
    • 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
    • F41G7/2213—Homing guidance systems maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
    • 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

Landscapes

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

Abstract

- Système de défense antiaérien susceptible d'intercepter des engins aériens à grande vitesse (3), comportant une installation de commande fixe (1) et des missiles (2) de défense. - Selon la présente invention : . au point (F) commun à la trajectoire d'approche (T) dudit engin aérien (3) et à la trajectoire d'interception (t) dudit missile de défense (2), ladite trajectoire d'interception est transversale à la trajectoire d'approche ; . l'axe central de l'autodirecteur du missile de défense (2) est incliné latéralement par rapport à l'axe dudit missile de défense (2) ; et . ledit missile de défense (2) est stabilisé en roulis, de façon que ledit axe central dudit autodirecteur soit disposé du côté dudit engin aérien (3).
CA002134578A 1993-11-25 1994-10-28 Systeme de defense antiaerien et missile de defense pour un tel systeme Expired - Fee Related CA2134578C (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9314082A FR2712972B1 (fr) 1993-11-25 1993-11-25 Système de défense antiaérien et missile de défense pour un tel système.
FR9314082 1993-11-25

Publications (2)

Publication Number Publication Date
CA2134578A1 true CA2134578A1 (fr) 1995-05-26
CA2134578C CA2134578C (fr) 2005-05-24

Family

ID=9453208

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002134578A Expired - Fee Related CA2134578C (fr) 1993-11-25 1994-10-28 Systeme de defense antiaerien et missile de defense pour un tel systeme

Country Status (8)

Country Link
US (1) US5464174A (fr)
EP (1) EP0655599B1 (fr)
JP (1) JP3630181B2 (fr)
CA (1) CA2134578C (fr)
DE (1) DE69411514T2 (fr)
ES (1) ES2119983T3 (fr)
FR (1) FR2712972B1 (fr)
IL (1) IL111419A (fr)

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US6825792B1 (en) 2003-10-06 2004-11-30 Howard Letovsky Missile detection and neutralization system
US7066427B2 (en) * 2004-02-26 2006-06-27 Chang Industry, Inc. Active protection device and associated apparatus, system, and method
US7104496B2 (en) * 2004-02-26 2006-09-12 Chang Industry, Inc. Active protection device and associated apparatus, system, and method
DE102004037235A1 (de) * 2004-07-31 2006-03-23 Diehl Bgt Defence Gmbh & Co. Kg Verfahren zum Schützen einer Immobilie gegen ein angreifendes Projektil
DE102004038264A1 (de) * 2004-08-06 2006-03-16 Diehl Bgt Defence Gmbh & Co. Kg Selbstschutz-Verfahren gegen die Bedrohung durch ein angreifendes Projektil
IL163450A (en) * 2004-08-10 2009-12-24 Rafael Advanced Defense Sys Guided missile with distributed guidance mechanism
US7264198B2 (en) * 2004-12-13 2007-09-04 Lockheed Martin Corporation Time-to-go missile guidance method and system
US7387060B1 (en) * 2005-05-17 2008-06-17 The United States Of America As Represented By The Secretary Of The Navy Rocket exhaust defense system and method
US8130137B1 (en) 2005-07-26 2012-03-06 Lockheed Martin Corporation Template updated boost algorithm
US7511252B1 (en) * 2006-05-09 2009-03-31 Lockheed Martin Corporation Multihypothesis threat missile propagator for boost-phase missile defense
US7473876B1 (en) * 2006-05-09 2009-01-06 Lockheed Martin Corporation Boost phase intercept missile fire control system architecture
US7755011B2 (en) * 2006-06-23 2010-07-13 Lockheed Martin Corporation Target maneuver detection
US7977614B2 (en) * 2006-09-03 2011-07-12 E.C.S. Engineering Consulting Services-Aerospace Ltd. Method and system for defense against incoming rockets and missiles
US8134103B2 (en) * 2006-12-27 2012-03-13 Lockheed Martin Corporation Burnout time estimation and early thrust termination determination for a boosting target
US8288696B1 (en) * 2007-07-26 2012-10-16 Lockheed Martin Corporation Inertial boost thrust vector control interceptor guidance
DE102007049438B4 (de) * 2007-10-16 2018-10-31 Mbda Deutschland Gmbh Verfahren zur Abwehr von ballistischen Geschossen mit Hilfe von Lenkflugkörpern
US7875837B1 (en) * 2008-01-09 2011-01-25 Lockheed Martin Corporation Missile tracking with interceptor launch and control
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JP2009300063A (ja) * 2008-06-10 2009-12-24 Haruo Wakabayashi 飛行体捕捉システムおよび飛行体捕捉方法
JP5224934B2 (ja) * 2008-06-25 2013-07-03 株式会社東芝 飛翔体、飛翔体の飛翔方法及びコンピュータプログラム
US8173946B1 (en) * 2008-08-26 2012-05-08 Raytheon Company Method of intercepting incoming projectile
US8063347B1 (en) * 2009-01-19 2011-11-22 Lockheed Martin Corporation Sensor independent engagement decision processing
US8380367B2 (en) * 2009-03-26 2013-02-19 The University Of North Dakota Adaptive surveillance and guidance system for vehicle collision avoidance and interception
GB2479211B (en) * 2010-03-31 2014-07-23 Qinetiq Ltd System for the detection of incoming munitions
CN101982720B (zh) * 2010-09-29 2012-11-14 北京机械设备研究所 一种低空慢速小目标的拦截方法
CN102087082B (zh) * 2010-11-22 2013-05-08 北京机械设备研究所 一种基于射表拟合的低空慢速小目标拦截方法
US8963765B1 (en) * 2010-12-14 2015-02-24 Lockheed Martin Corporation System and method for detecting use of booster rockets by ballistic missiles
CN103134387B (zh) * 2011-11-29 2014-10-15 北京航天长峰科技工业集团有限公司 一种低空慢速小目标探测与拦截系统标定方法
US9316733B2 (en) * 2012-01-04 2016-04-19 Farrokh Mohamadi W-band, ultra-wide band (UWB) trajectory detector
CN103575167B (zh) * 2013-11-07 2014-12-03 北京机械设备研究所 一种民用拦截弹弹道修正方法
RU2611683C2 (ru) * 2014-12-12 2017-02-28 Николай Евгеньевич Староверов Система преодоления противоракетной обороны противника, алгоритм её работы и боеголовка для неё
CN106643298B (zh) * 2016-11-29 2018-04-27 北京宇航系统工程研究所 一种基于预置命中点的大气层内反导拦截器中制导方法
CN111369832B (zh) * 2019-12-27 2021-07-16 中国人民解放军海军大连舰艇学院 一种单艘区域舰空导弹舰艇纵横向水平机动掩护单艘邻舰方法

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Also Published As

Publication number Publication date
CA2134578C (fr) 2005-05-24
DE69411514D1 (de) 1998-08-13
US5464174A (en) 1995-11-07
IL111419A (en) 1998-02-22
JP3630181B2 (ja) 2005-03-16
IL111419A0 (en) 1995-01-24
FR2712972A1 (fr) 1995-06-02
JPH07190695A (ja) 1995-07-28
FR2712972B1 (fr) 1996-01-26
DE69411514T2 (de) 1998-12-10
EP0655599B1 (fr) 1998-07-08
EP0655599A1 (fr) 1995-05-31
ES2119983T3 (es) 1998-10-16

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Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed
MKLA Lapsed

Effective date: 20091028

MKLA Lapsed

Effective date: 20091028