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 method

Info

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
Application number
IL67424A
Other languages
English (en)
Original Assignee
Thomson Brandt
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 filed Critical Thomson Brandt
Publication of IL67424A publication Critical patent/IL67424A/xx

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
IL67424A 1981-12-09 1982-12-06 Missile terminal flight guidance method and a guided missile operating according to this method IL67424A (en)

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 (xx)
EP (1) EP0081421B1 (xx)
JP (1) JPS58127100A (xx)
AT (1) ATE40467T1 (xx)
CA (1) CA1209232A (xx)
DE (1) DE3279397D1 (xx)
FR (1) FR2517818A1 (xx)
IL (1) IL67424A (xx)

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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
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DE3342958A1 (de) * 1983-11-26 1985-06-05 Diehl GmbH & Co, 8500 Nürnberg Sensoranordnung in einem suchkopf
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DE3427227A1 (de) * 1984-07-24 1986-01-30 Diehl GmbH & Co, 8500 Nürnberg Endphasen-steuerbarer munitionsartikel und verfahren zu seiner zielnavigation
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FR2684723B1 (fr) * 1991-12-10 1995-05-19 Thomson Csf Propulseur a propergol solide a poussee modulable et missile equipe.
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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
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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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Also Published As

Publication number Publication date
CA1209232A (en) 1986-08-05
ATE40467T1 (de) 1989-02-15
EP0081421B1 (fr) 1989-01-25
FR2517818A1 (fr) 1983-06-10
FR2517818B1 (xx) 1985-02-22
JPH0449040B2 (xx) 1992-08-10
JPS58127100A (ja) 1983-07-28
DE3279397D1 (en) 1989-03-02
US4568040A (en) 1986-02-04
EP0081421A1 (fr) 1983-06-15

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