ATE40467T1 - Verfahren zur endphasenlenkung und dieses verfahren verwendender lenkflugkoerper. - Google Patents

Verfahren zur endphasenlenkung und dieses verfahren verwendender lenkflugkoerper.

Info

Publication number
ATE40467T1
ATE40467T1 AT82402180T AT82402180T ATE40467T1 AT E40467 T1 ATE40467 T1 AT E40467T1 AT 82402180 T AT82402180 T AT 82402180T AT 82402180 T AT82402180 T AT 82402180T AT E40467 T1 ATE40467 T1 AT E40467T1
Authority
AT
Austria
Prior art keywords
missile
section
phase guidance
fins
trajectory
Prior art date
Application number
AT82402180T
Other languages
English (en)
Inventor
Pierre Metz
Original Assignee
Thomson Brandt Armements
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 filed Critical Thomson Brandt Armements
Application granted granted Critical
Publication of ATE40467T1 publication Critical patent/ATE40467T1/de

Links

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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
AT82402180T 1981-12-09 1982-11-30 Verfahren zur endphasenlenkung und dieses verfahren verwendender lenkflugkoerper. ATE40467T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8123025A FR2517818A1 (fr) 1981-12-09 1981-12-09 Methode de guidage terminal et missile guide operant selon cette methode
EP82402180A EP0081421B1 (de) 1981-12-09 1982-11-30 Verfahren zur Endphasenlenkung und dieses Verfahren verwendender Lenkflugkörper

Publications (1)

Publication Number Publication Date
ATE40467T1 true ATE40467T1 (de) 1989-02-15

Family

ID=9264837

Family Applications (1)

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

Country Status (8)

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

Families Citing this family (62)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4522356A (en) * 1973-11-12 1985-06-11 General Dynamics, Pomona Division Multiple target seeking clustered munition and system
DE3323685C2 (de) * 1983-07-01 1985-12-05 Dornier Gmbh, 7990 Friedrichshafen Verfahren zur selbsttätigen Annäherung von Submunition aus der Luft an insbesondere bewegte Bodenziele
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
GB2459914B (en) * 1989-10-17 2010-05-19 Aerospatiale Guidance system for a missile provided with a photosensitive detector
ES2118744T3 (es) * 1990-01-16 1998-10-01 Tda Armements Sas Municion perforadora para objetivos o blancos de alta resistencia mecanica.
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
US5076511A (en) * 1990-12-19 1991-12-31 Honeywell Inc. Discrete impulse spinning-body hard-kill (disk)
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.
FR2695992B1 (fr) * 1992-09-21 1994-12-30 Giat Ind Sa Sous munition à effet dirigé.
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
RU2148235C1 (ru) * 1999-08-16 2000-04-27 ОАО "Фазотрон - Научно-исследовательский институт радиостроения" Способ пропорционального наведения летательных аппаратов на наземные объекты
CN1153949C (zh) * 1999-11-03 2004-06-16 斯托姆金属有限公司 成套防御装置
RU2189556C2 (ru) * 1999-11-26 2002-09-20 Калинкин Виктор Алексеевич Способ формирования сигналов управления летательным аппаратом при наведении на воздушную цель
US6422509B1 (en) * 2000-11-28 2002-07-23 Xerox Corporation Tracking device
RU2220397C1 (ru) * 2002-05-21 2003-12-27 ОАО "Корпорация "Фазотрон-НИИР" Способ наведения летательных аппаратов на наземные цели при полуактивном синтезировании апертуры антенны
US6817568B2 (en) * 2003-02-27 2004-11-16 Raytheon Company Missile system with multiple submunitions
RU2231734C1 (ru) * 2003-09-16 2004-06-27 Закрытое акционерное общество Научно-технический комплекс "Автоматизация и механизация технологий" Комплекс корректируемого артиллерийского вооружения с лазерным наведением
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
RU2292562C2 (ru) * 2005-03-09 2007-01-27 Федеральное государственное унитарное предприятие "НИИ "Экран" Устройство для измерения угла встречи активного радиолокатора с сосредоточенной воздушной целью
RU2290661C2 (ru) * 2005-03-09 2006-12-27 Федеральное государственное унитарное предприятие "НИИ "Экран" Способ измерения угла встречи активного радиолокатора с сосредоточенной воздушной целью
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
RU2392575C2 (ru) * 2008-07-31 2010-06-20 Федеральное государственное унитарное предприятие "НИИ "Экран" Устройство самонаведения
CA2759383C (en) * 2009-02-02 2017-11-21 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
DK3133019T3 (en) 2009-09-09 2019-02-18 Aerovironment Inc NOISE DEVICE FOR A DRONE PROTECTION PIPE
US8436284B1 (en) * 2009-11-21 2013-05-07 The Boeing Company Cavity flow shock oscillation damping mechanism
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
US11448486B2 (en) * 2019-09-03 2022-09-20 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

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2520433A (en) * 1941-11-10 1950-08-29 Marion B Robinson Directed missile
US3374967A (en) * 1949-12-06 1968-03-26 Navy Usa Course-changing gun-launched missile
FR59801E (fr) * 1952-10-25 1954-08-23 Viseur universel sur avion (ou navire) pour la dérivométrie, l'atterrissage de précision, la conduite du pilotage, du bombardement en piqué par bombes ou fusées, dutir sur but au sol ou but aérien et du torpillage
US3000307A (en) * 1953-08-04 1961-09-19 Jr Herbert Trotter Device for correcting the course of a missile
US3072365A (en) * 1957-09-16 1963-01-08 Missile Corp Pilotless craft guidance method and means
DE1092312B (de) * 1957-10-02 1960-11-03 Philips Nv Flugzeug mit Signalsender
DE1092313B (de) * 1958-02-28 1960-11-03 Ignaz V Maydell Dipl Ing Verfahren und Vorrichtung zur Beeinflussung der Bahn eines ferngelenkten oder ferngesteuerten fliegenden Koerpers
US4193567A (en) * 1962-07-17 1980-03-18 Novatronics, Inc. Guidance devices
US3282540A (en) * 1964-05-05 1966-11-01 Henry S Lipinski Gun launched terminal guided projectile
US3843076A (en) * 1972-01-03 1974-10-22 Trw Projectile trajectory correction system
GB1467035A (en) * 1973-05-25 1977-03-16 Messerschmitt Boelkow Blohm Attacking flying targets from a submarine
FR2231947A1 (en) * 1973-06-01 1974-12-27 Realisations Applic Techn Et Rocket guidance system - clock device actuates pulse type target dector and course controller
FR2321723A1 (fr) * 1975-07-29 1977-03-18 Thomson Brandt Systeme de controle d'attitude et engin equipe d'un tel systeme
US4039246A (en) * 1976-01-22 1977-08-02 General Dynamics Corporation Optical scanning apparatus with two mirrors rotatable about a common axis
US4383663A (en) * 1976-06-01 1983-05-17 The United States Of America As Represented By The Secretary Of The Navy Active optical terminal homing
US4183664A (en) * 1976-09-23 1980-01-15 Raytheon Company Optical apparatus
FR2463909B1 (fr) * 1979-08-17 1985-10-25 Thomson Brandt Procede de pilotage et de guidage d'un missile, et missile equipe de moyens de mise en oeuvre de ce procede
FR2469345A1 (fr) * 1979-11-09 1981-05-22 Thomson Brandt Procede de pilotage et de guidage de projectiles en phase terminale et projectiles comportant les moyens de mise en oeuvre de ce procede
FR2478297B1 (fr) * 1980-03-12 1986-09-05 Serat Perfectionnements apportes aux tetes militaires, notamment antichars, agissant en survol d'un objectif ou d'un groupe d'objectifs
US4394997A (en) * 1980-04-14 1983-07-26 General Dynamics, Pomona Division Sequential time discrimination system for sub-delivery systems
US4347996A (en) * 1980-05-22 1982-09-07 Raytheon Company Spin-stabilized projectile and guidance system therefor

Also Published As

Publication number Publication date
JPH0449040B2 (de) 1992-08-10
JPS58127100A (ja) 1983-07-28
CA1209232A (en) 1986-08-05
EP0081421A1 (de) 1983-06-15
IL67424A (en) 1989-03-31
FR2517818A1 (fr) 1983-06-10
US4568040A (en) 1986-02-04
EP0081421B1 (de) 1989-01-25
FR2517818B1 (de) 1985-02-22
DE3279397D1 (en) 1989-03-02

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