EP0081421B1 - Méthode de guidage terminal et missile guidé opérant selon cette méthode - Google Patents

Méthode de guidage terminal et missile guidé opérant selon cette méthode Download PDF

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Publication number
EP0081421B1
EP0081421B1 EP82402180A EP82402180A EP0081421B1 EP 0081421 B1 EP0081421 B1 EP 0081421B1 EP 82402180 A EP82402180 A EP 82402180A EP 82402180 A EP82402180 A EP 82402180A EP 0081421 B1 EP0081421 B1 EP 0081421B1
Authority
EP
European Patent Office
Prior art keywords
missile
section
target
sensor
trajectory
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.)
Expired
Application number
EP82402180A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP0081421A1 (fr
Inventor
Pierre Metz
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.)
Thomson Brandt Armements SA
Original Assignee
Thomson Brandt Armements SA
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 Thomson Brandt Armements SA filed Critical Thomson Brandt Armements SA
Priority to AT82402180T priority Critical patent/ATE40467T1/de
Publication of EP0081421A1 publication Critical patent/EP0081421A1/fr
Application granted granted Critical
Publication of EP0081421B1 publication Critical patent/EP0081421B1/fr
Expired legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
    • 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
    • F41G7/222—Homing guidance systems for spin-stabilized 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
    • 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
    • F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • 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
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C13/00—Proximity fuzes; Fuzes for remote detonation
    • F42C13/006—Proximity fuzes; Fuzes for remote detonation for non-guided, spinning, braked or gravity-driven weapons, e.g. parachute-braked sub-munitions
EP82402180A 1981-12-09 1982-11-30 Méthode de guidage terminal et missile guidé opérant selon cette méthode Expired EP0081421B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT82402180T ATE40467T1 (de) 1981-12-09 1982-11-30 Verfahren zur endphasenlenkung und dieses verfahren verwendender lenkflugkoerper.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8123025 1981-12-09
FR8123025A FR2517818A1 (fr) 1981-12-09 1981-12-09 Methode de guidage terminal et missile guide operant selon cette methode

Publications (2)

Publication Number Publication Date
EP0081421A1 EP0081421A1 (fr) 1983-06-15
EP0081421B1 true EP0081421B1 (fr) 1989-01-25

Family

ID=9264837

Family Applications (1)

Application Number Title Priority Date Filing Date
EP82402180A Expired EP0081421B1 (fr) 1981-12-09 1982-11-30 Méthode de guidage terminal et missile guidé opérant selon cette méthode

Country Status (8)

Country Link
US (1) US4568040A (ja)
EP (1) EP0081421B1 (ja)
JP (1) JPS58127100A (ja)
AT (1) ATE40467T1 (ja)
CA (1) CA1209232A (ja)
DE (1) DE3279397D1 (ja)
FR (1) FR2517818A1 (ja)
IL (1) IL67424A (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4032982B3 (de) * 1989-10-17 2010-05-20 Aerospatiale Societe Nationale Industrielle Lenksystem für mit einem photoempfindlichen Detektor versehene Flugkörper

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SE456036B (sv) * 1983-07-05 1988-08-29 Bofors Ab Sett och anordning for att styra en ur en kanon utskjutbar projektil mot ett mal
DE3333517A1 (de) * 1983-09-16 1986-09-04 Diehl GmbH & Co, 8500 Nürnberg Verfahren und vorrichtung zum bekaempfen von zielobjekten mittels submunition
DE3342958A1 (de) * 1983-11-26 1985-06-05 Diehl GmbH & Co, 8500 Nürnberg Sensoranordnung in einem suchkopf
FR2736147B1 (fr) * 1983-12-14 1997-12-19 Brandt Armements Methode d'acquisition d'une cible par un projectile guide et projectile operant selon cette methode
DE3427227A1 (de) * 1984-07-24 1986-01-30 Diehl GmbH & Co, 8500 Nürnberg Endphasen-steuerbarer munitionsartikel und verfahren zu seiner zielnavigation
DE3516673A1 (de) * 1985-05-09 1986-11-13 Diehl GmbH & Co, 8500 Nürnberg Endphasen-korrigierbare suchzuender-munition und verfahren zum bekaempfen gepanzerter zielobjekte
DE3522154A1 (de) * 1985-06-21 1987-01-02 Diehl Gmbh & Co Suchzuender-submunition
DE3527522A1 (de) * 1985-08-01 1987-02-12 Diehl Gmbh & Co Verfahren und verwendung von endphasenkorrigierter submunition zum bekaempfen von gepanzerten unterstaenden
FR2607917A1 (fr) * 1986-12-08 1988-06-10 Roche Kerandraon Oliver Guidage par infrarouge simplifie pour tout projectile
SE461750B (sv) * 1987-03-20 1990-03-19 Lars Johan Schleimann Jensen Foerfarande foer styrning av ett flygande objekt, saasom en projektil, mot ett maal och projektil foer foerfarandets genomfoerande
US4850275A (en) * 1987-10-30 1989-07-25 The Bdm Corporation Aircraft hollow nose cone
FR2634012A1 (fr) * 1988-07-06 1990-01-12 Roche Kerandraon Oliver Projectile antibut mobile, a echelon unique de correction, a pilotage par reference pendulaire et a trois modes de detection selectionnables
DE3826615C2 (de) * 1988-08-05 1995-06-08 Rheinmetall Gmbh Gierwinkelfreies Geschoß
DE3906372A1 (de) * 1989-03-01 1990-09-13 Rheinmetall Gmbh Fluegelstabilisierter submunitionskoerper
US5261629A (en) * 1989-04-08 1993-11-16 Rheinmetall Gmbh Fin stabilized projectile
FR2647540B1 (fr) * 1989-05-23 1994-03-25 Thomson Csf Dispositif de ralliement de missile
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US5052637A (en) * 1990-03-23 1991-10-01 Martin Marietta Corporation Electronically stabilized tracking system
US5080305A (en) * 1990-04-16 1992-01-14 Stencel Fred B Low-altitude retro-rocket load landing system with wind drift counteraction
US5114094A (en) * 1990-10-23 1992-05-19 Alliant Techsystems, Inc. Navigation method for spinning body and projectile using same
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FR2684723B1 (fr) * 1991-12-10 1995-05-19 Thomson Csf Propulseur a propergol solide a poussee modulable et missile equipe.
DE4210113C1 (de) * 1992-03-27 1998-11-05 Athanassios Dr Ing Zacharias Verfahren zum Leiten eines Flugkörpers und Flugkörper
RU2021577C1 (ru) * 1992-06-30 1994-10-15 Машиностроительное Конструкторское Бюро "Факел" Способ управления снарядом
FR2693265B1 (fr) * 1992-07-02 1994-09-16 Giat Ind Sa Munition comportant des moyens de détection de cibles.
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US5328129A (en) * 1993-06-17 1994-07-12 The United States Of America As Represented By The Secretary Of The Navy Guidance method for unthrottled, solid-fuel divert motors
DE4410326C2 (de) * 1994-03-25 1998-07-02 Rheinmetall Ind Ag Geschoß mit einer Vorrichtung zur Flugbahnkorrektur
US6254031B1 (en) * 1994-08-24 2001-07-03 Lockhead Martin Corporation Precision guidance system for aircraft launched bombs
DE19505791C1 (de) * 1995-02-20 1996-08-14 Daimler Benz Aerospace Ag Verfahren und Vorrichtung zur Bekämpfung verdeckt operierender Hubschrauber
IL148889A0 (en) * 1999-11-03 2002-09-12 Metal Storm Ltd Set defence means
US6422509B1 (en) * 2000-11-28 2002-07-23 Xerox Corporation Tracking device
US6817568B2 (en) * 2003-02-27 2004-11-16 Raytheon Company Missile system with multiple submunitions
US7185844B2 (en) * 2004-04-30 2007-03-06 Technology Service Corporation Methods and systems for guiding an object to a target using an improved guidance law
US7851732B2 (en) * 2006-03-07 2010-12-14 Raytheon Company System and method for attitude control of a flight vehicle using pitch-over thrusters
US7781709B1 (en) 2008-05-05 2010-08-24 Sandia Corporation Small caliber guided projectile
AU2010239639B2 (en) * 2009-02-02 2015-01-15 Aerovironment Multimode unmanned aerial vehicle
US8618455B2 (en) * 2009-06-05 2013-12-31 Safariland, Llc Adjustable range munition
US8058596B2 (en) * 2009-08-27 2011-11-15 Raytheon Company Method of controlling missile flight using attitude control thrusters
EP2475578B1 (en) 2009-09-09 2017-07-19 AeroVironment, Inc. Reinforced UAV launch tube
US8436284B1 (en) * 2009-11-21 2013-05-07 The Boeing Company Cavity flow shock oscillation damping mechanism
RU2533660C2 (ru) * 2012-09-27 2014-11-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Самарский государственный технический университет" Способ и устройство автономной радиолокационной самокоррекции промаха при встрече малоразмерного летательного аппарата с объектом на заключительном участке траектории полета
CN103307938B (zh) * 2013-04-23 2015-06-03 北京电子工程总体研究所 一种旋转弹气动参数获取方法
RU2590760C2 (ru) * 2014-07-29 2016-07-10 Николай Евгеньевич Староверов Ракета и способ её работы
CN105043171B (zh) * 2015-06-30 2017-08-29 北京航天长征飞行器研究所 一种带倾角约束的火箭弹纵向导引方法
RU2644962C2 (ru) * 2016-07-07 2018-02-15 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Способ поражения цели сверхзвуковой крылатой ракетой и сверхзвуковая крылатая ракета для его осуществления
SE541615C2 (sv) * 2017-04-28 2019-11-12 Bae Systems Bofors Ab Projektil med valbar anfallsvinkel
RU2701671C1 (ru) * 2018-04-09 2019-09-30 Анатолий Борисович Атнашев Способ наведения ракеты
CN109737812B (zh) * 2018-12-27 2021-10-15 北京航天飞腾装备技术有限责任公司 空对地制导武器侧向攻击方法和装置
RU2718560C1 (ru) * 2019-07-16 2020-04-08 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Способ обнаружения и поражения воздушной цели ракетным комплексом
US11280591B2 (en) * 2019-09-03 2022-03-22 Harkind Dynamics, LLC Intelligent munition
CN114812293B (zh) * 2021-01-27 2023-03-24 北京理工大学 一种末端减速机动控制方法
CN114034215B (zh) * 2021-11-23 2023-02-28 航天科工火箭技术有限公司 一种火箭的导引方法和装置

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Publication number Priority date Publication date Assignee Title
DE4032982B3 (de) * 1989-10-17 2010-05-20 Aerospatiale Societe Nationale Industrielle Lenksystem für mit einem photoempfindlichen Detektor versehene Flugkörper

Also Published As

Publication number Publication date
CA1209232A (en) 1986-08-05
ATE40467T1 (de) 1989-02-15
FR2517818A1 (fr) 1983-06-10
FR2517818B1 (ja) 1985-02-22
JPH0449040B2 (ja) 1992-08-10
JPS58127100A (ja) 1983-07-28
DE3279397D1 (en) 1989-03-02
US4568040A (en) 1986-02-04
EP0081421A1 (fr) 1983-06-15
IL67424A (en) 1989-03-31

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