IL107844A - Flying object control system - Google Patents

Flying object control system

Info

Publication number
IL107844A
IL107844A IL10784493A IL10784493A IL107844A IL 107844 A IL107844 A IL 107844A IL 10784493 A IL10784493 A IL 10784493A IL 10784493 A IL10784493 A IL 10784493A IL 107844 A IL107844 A IL 107844A
Authority
IL
Israel
Prior art keywords
frame
control device
flight control
fin
main shaft
Prior art date
Application number
IL10784493A
Other languages
English (en)
Hebrew (he)
Other versions
IL107844A0 (en
Inventor
Moshe Epstein
Moshe Ben Ezri
Original Assignee
Ministry Of Defence Armaments
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 Ministry Of Defence Armaments filed Critical Ministry Of Defence Armaments
Priority to IL10784493A priority Critical patent/IL107844A/en
Priority to GB9423896A priority patent/GB2284397A/en
Priority to DE4442461A priority patent/DE4442461A1/de
Priority to FR9414447A priority patent/FR2713330B1/fr
Priority to US08/347,800 priority patent/US5584448A/en
Publication of IL107844A0 publication Critical patent/IL107844A0/xx
Publication of IL107844A publication Critical patent/IL107844A/en

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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • 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
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
IL10784493A 1993-12-02 1993-12-02 Flying object control system IL107844A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
IL10784493A IL107844A (en) 1993-12-02 1993-12-02 Flying object control system
GB9423896A GB2284397A (en) 1993-12-02 1994-11-25 Flight control device
DE4442461A DE4442461A1 (de) 1993-12-02 1994-11-29 Flugsteuerungsvorrichtung
FR9414447A FR2713330B1 (fr) 1993-12-02 1994-12-01 Dispositif de commande de vol.
US08/347,800 US5584448A (en) 1993-12-02 1994-12-01 Flight control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IL10784493A IL107844A (en) 1993-12-02 1993-12-02 Flying object control system

Publications (2)

Publication Number Publication Date
IL107844A0 IL107844A0 (en) 1995-07-31
IL107844A true IL107844A (en) 1996-06-18

Family

ID=11065539

Family Applications (1)

Application Number Title Priority Date Filing Date
IL10784493A IL107844A (en) 1993-12-02 1993-12-02 Flying object control system

Country Status (5)

Country Link
US (1) US5584448A (de)
DE (1) DE4442461A1 (de)
FR (1) FR2713330B1 (de)
GB (1) GB2284397A (de)
IL (1) IL107844A (de)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69627322T2 (de) * 1995-05-11 2004-02-12 Vympel State Machine Building Design Bureau (Gosmkb "Vympel") Rakete mit gitterruder
US5816531A (en) * 1997-02-04 1998-10-06 The United States Of America As Represented By The Secretary Of The Army Range correction module for a spin stabilized projectile
DE10015514B4 (de) * 2000-03-30 2007-10-04 Rheinmetall Waffe Munition Gmbh Flügelstabilisiertes Geschoß
DE10118216A1 (de) * 2001-04-12 2002-10-17 Diehl Munitionssysteme Gmbh Ruderblatt-Lagereinrichtung für ein Geschoß
US6685143B1 (en) * 2003-01-03 2004-02-03 Orbital Research Inc. Aircraft and missile forebody flow control device and method of controlling flow
FR2860577B1 (fr) * 2003-10-06 2006-01-27 Giat Ind Sa Dispositif de deploiement d'une ailette d'un projectile
US8080772B2 (en) * 2007-11-02 2011-12-20 Honeywell International Inc. Modular, harnessless electromechanical actuation system assembly
US8438977B2 (en) * 2008-12-25 2013-05-14 Lockheed Martin Corporation Projectile having deployable fin
CN105151275B (zh) * 2009-09-09 2017-05-31 威罗门飞行公司 升降副翼控制系统
JP5626768B2 (ja) * 2010-05-28 2014-11-19 株式会社Ｉｈｉエアロスペース 飛翔体
RU2549044C2 (ru) * 2013-01-24 2015-04-20 Открытое акционерное общество "Корпорация "Тактическое ракетное вооружение" Складная рулевая поверхность авиационного средства поражения с пружинным механизмом раскладывания
KR101338177B1 (ko) * 2013-08-02 2013-12-09 국방과학연구소 휴대용 유도탄 조종날개 조정 장치
CN104859842B (zh) * 2015-06-11 2017-05-17 贵州华烽电器有限公司 一种纵向角位移工装结构
RU2635705C2 (ru) * 2015-12-10 2017-11-15 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Устройство стабилизации ракеты
US11300390B1 (en) 2018-03-05 2022-04-12 Dynamic Structures And Materials, Llc Control surface deployment apparatus and method of use
RU2717327C1 (ru) * 2019-06-13 2020-03-20 Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") Рулевой блок беспилотного управляемого летательного аппарата
CN111854541A (zh) * 2020-06-23 2020-10-30 西北工业大学 一种折叠翼微型导弹平台

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3154015A (en) * 1962-09-19 1964-10-27 Martin Marietta Corp Missile flight control system
FR1528934A (fr) * 1966-06-21 1968-06-14 Gen Dynamics Corp Dispositif de commande perfectionné pour engins volants, notamment pour missiles
GB1187035A (en) * 1966-08-02 1970-04-08 British Aircraft Corp Ltd Aerial Guided Missiles with Fins.
SE331242B (de) * 1969-05-14 1970-12-14 Bofors Ab
FR2226641B1 (de) * 1973-04-17 1976-11-12 France Etat
DE2342783C2 (de) * 1973-08-24 1983-12-22 Rheinmetall GmbH, 4000 Düsseldorf Mit einem Leitwerk versehenes Geschoß
GB2041502B (en) * 1979-02-08 1982-09-08 British Aerospace Folding fin assembly
US4398682A (en) * 1979-09-18 1983-08-16 British Aerospace Public Limited Company Displacement mechanism
US4323208A (en) * 1980-02-01 1982-04-06 British Aerospace Folding fins
US4523728A (en) * 1983-03-07 1985-06-18 Ford Aerospace & Communications Corporation Passive auto-erecting alignment wings for long rod penetrator
US4560121A (en) * 1983-05-17 1985-12-24 The Garrett Corporation Stabilization of automotive vehicle
GB2150092B (en) * 1983-11-25 1987-07-22 British Aerospace Deployment and actuation mechanisms
US4575025A (en) * 1984-04-25 1986-03-11 Sadvary John W Fin deployment mechanism for missiles
DE3441534A1 (de) * 1984-11-14 1986-05-15 Diehl GmbH & Co, 8500 Nürnberg Lageranordnung fuer das ruderblatt eines flugkoerpers
SE444612B (sv) * 1984-12-13 1986-04-21 Ffv Affersverket Styrverk for utfellning av fenor hos projektil
FR2623898B1 (fr) * 1987-11-26 1990-03-23 France Etat Armement Dispositif de deploiement d'une ailette de projectile
DE3712704A1 (de) * 1987-04-14 1988-11-03 Diehl Gmbh & Co Flugkoerper mit ausklappbaren fluegeln
GB2214882A (en) * 1988-02-17 1989-09-13 British Aerospace A canard actuation assembly
DE4020897C2 (de) * 1990-06-30 1993-11-11 Diehl Gmbh & Co Einrichtung zum Entriegeln und Ausschwenken der Ruderblätter eines Projektiles
DE4135557C2 (de) * 1991-10-29 1999-05-06 Diehl Stiftung & Co Ruderstelleinrichtung

Also Published As

Publication number Publication date
DE4442461A1 (de) 1995-06-08
US5584448A (en) 1996-12-17
GB2284397A (en) 1995-06-07
GB9423896D0 (en) 1995-01-11
IL107844A0 (en) 1995-07-31
FR2713330B1 (fr) 1997-01-10
FR2713330A1 (fr) 1995-06-09

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Legal Events

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