IL67424A - Missile terminal flight guidance method and a guided missile operating according to this method - Google Patents
Missile terminal flight guidance method and a guided missile operating according to this methodInfo
- Publication number
- IL67424A IL67424A IL67424A IL6742482A IL67424A IL 67424 A IL67424 A IL 67424A IL 67424 A IL67424 A IL 67424A IL 6742482 A IL6742482 A IL 6742482A IL 67424 A IL67424 A IL 67424A
- Authority
- IL
- Israel
- Prior art keywords
- missile
- operating according
- flight guidance
- section
- guidance method
- Prior art date
Links
- 230000000087 stabilizing effect Effects 0.000 abstract 1
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)
Applications Claiming Priority (1)
| 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 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IL67424A true IL67424A (en) | 1989-03-31 |
Family
ID=9264837
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IL67424A IL67424A (en) | 1981-12-09 | 1982-12-06 | Missile terminal flight guidance method and a guided missile operating according to this method |
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)
| 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 |
| IT9021755A1 (it) * | 1989-10-17 | 1991-04-18 | Aerospatiale Soc Nat Indus Trielle | Sistema di guida per missile dotato di un rivelatore fotosensibile. |
| ATE168768T1 (de) * | 1990-01-16 | 1998-08-15 | Tda Armements Sas | Penetratormunition für ziele mit hohem mechanischem widerstand |
| 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 |
| CN1536324A (zh) * | 1999-11-03 | 2004-10-13 | ��������ķ������ | 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 |
| RU2290661C2 (ru) * | 2005-03-09 | 2006-12-27 | Федеральное государственное унитарное предприятие "НИИ "Экран" | Способ измерения угла встречи активного радиолокатора с сосредоточенной воздушной целью |
| 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 |
| 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 |
| EP2391863B1 (de) | 2009-02-02 | 2020-08-05 | Aerovironment | Multimodales unbemanntes fluggerät |
| 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 |
| KR101831119B1 (ko) | 2009-09-09 | 2018-02-21 | 에어로바이론먼트, 인크. | 휴대용 rf 투명 발사관을 구비한 원격 조종 무인 항공기 포성 억제 발사장치를 위한 시스템 및 장치 |
| 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 |
| 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 |
Family Cites Families (21)
| 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 |
-
1981
- 1981-12-09 FR FR8123025A patent/FR2517818A1/fr active Granted
-
1982
- 1982-11-30 DE DE8282402180T patent/DE3279397D1/de not_active Expired
- 1982-11-30 EP EP82402180A patent/EP0081421B1/de not_active Expired
- 1982-11-30 AT AT82402180T patent/ATE40467T1/de not_active IP Right Cessation
- 1982-12-03 US US06/446,728 patent/US4568040A/en not_active Expired - Fee Related
- 1982-12-06 IL IL67424A patent/IL67424A/xx not_active IP Right Cessation
- 1982-12-06 CA CA000417036A patent/CA1209232A/en not_active Expired
- 1982-12-08 JP JP57215357A patent/JPS58127100A/ja active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| CA1209232A (en) | 1986-08-05 |
| DE3279397D1 (en) | 1989-03-02 |
| EP0081421A1 (de) | 1983-06-15 |
| ATE40467T1 (de) | 1989-02-15 |
| FR2517818B1 (de) | 1985-02-22 |
| JPH0449040B2 (de) | 1992-08-10 |
| US4568040A (en) | 1986-02-04 |
| JPS58127100A (ja) | 1983-07-28 |
| EP0081421B1 (de) | 1989-01-25 |
| FR2517818A1 (fr) | 1983-06-10 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| IL67424A (en) | Missile terminal flight guidance method and a guided missile operating according to this method | |
| DE3276528D1 (en) | A control mechanism for gas jet steering and a missile equipped with such a mechanism | |
| IL78454A0 (en) | Super agile tactical fighter aircraft and method of flying it in supernormal flight | |
| CA2414793A1 (en) | Fin-stabilized guidable missile | |
| ES450215A1 (es) | Sistema de control de actitud de un cuerpo cilindrico en desplazamiento en un fluido e ingenio que incorpora dicho sistema. | |
| WO1994019047A3 (en) | Oxy-hydrogen propelled torpedo for introducing angioplasty guide wire | |
| US4763857A (en) | Guidance apparatus for projectiles | |
| SE8200194L (sv) | Laddning | |
| DE3274294D1 (en) | Multiple component penetrator projectile | |
| ATE301816T1 (de) | Einrichtung zur veränderung der flugrichtung eines rotationsstabilisierten lenkgeschosses | |
| US4003531A (en) | Reverse flow reaction control system | |
| FR2424510A1 (fr) | Procede pour la mise a feu de l'explosif dans des installations de formage par explosion | |
| EP0069440A3 (de) | Einrichtung zum Erzeugen eines Gas-Schubkraft | |
| US8119959B1 (en) | Flight control of missiles | |
| US2910953A (en) | Jet driven torpedoes | |
| JPS6474160A (en) | Stable running device for high speed vehicle and control method thereof | |
| GB1117580A (en) | Improvements in or relating to control systems for aerial missiles and like vehicles | |
| GB2167831B (en) | The controlled propulsive wing | |
| DE3565891D1 (en) | Missile for practice ammunition having a limited range, and use of the same | |
| GB2005606A (en) | Rocket propulsion unit | |
| IT1102670B (it) | Perfezionamento nei sistemi di gui da per veicoli | |
| JPS5321375A (en) | Floating gyroscope | |
| JPS6463794A (en) | Guided missile | |
| FR2405869A1 (fr) | Procede et installation pour le controle de l'efficacite des surfaces aerodynamiques d'un aeronef | |
| RU97110346A (ru) | Способ запуска управляемой ракеты и устройство для его осуществления |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RH | Patent void |