DE60233113D1 - Zweidimensionale geschossflugbahnkorrekturvorrichtung - Google Patents

Zweidimensionale geschossflugbahnkorrekturvorrichtung

Info

Publication number
DE60233113D1
DE60233113D1 DE60233113T DE60233113T DE60233113D1 DE 60233113 D1 DE60233113 D1 DE 60233113D1 DE 60233113 T DE60233113 T DE 60233113T DE 60233113 T DE60233113 T DE 60233113T DE 60233113 D1 DE60233113 D1 DE 60233113D1
Authority
DE
Germany
Prior art keywords
correction device
store flight
dimensional store
gate correction
flight gate
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 - Lifetime
Application number
DE60233113T
Other languages
English (en)
Inventor
John G Rupert
Jeff Siewart
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.)
BAE Systems Land and Armaments LP
Original Assignee
BAE Systems Land and Armaments LP
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 BAE Systems Land and Armaments LP filed Critical BAE Systems Land and Armaments LP
Application granted granted Critical
Publication of DE60233113D1 publication Critical patent/DE60233113D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
    • 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/50—Brake flaps, e.g. inflatable
    • 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/54—Spin braking 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
DE60233113T 2001-02-01 2002-01-29 Zweidimensionale geschossflugbahnkorrekturvorrichtung Expired - Lifetime DE60233113D1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US26572501P 2001-02-01 2001-02-01
US26579401P 2001-02-01 2001-02-01
PCT/US2002/002553 WO2002061363A2 (en) 2001-02-01 2002-01-29 2-d projectile trajectory corrector

Publications (1)

Publication Number Publication Date
DE60233113D1 true DE60233113D1 (de) 2009-09-10

Family

ID=26951391

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60233113T Expired - Lifetime DE60233113D1 (de) 2001-02-01 2002-01-29 Zweidimensionale geschossflugbahnkorrekturvorrichtung

Country Status (6)

Country Link
US (2) US6502786B2 (de)
EP (1) EP1366339B1 (de)
AT (1) ATE438074T1 (de)
AU (1) AU2002245348A1 (de)
DE (1) DE60233113D1 (de)
WO (1) WO2002061363A2 (de)

Families Citing this family (69)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10130383A1 (de) * 2001-06-23 2003-01-09 Diehl Munitionssysteme Gmbh Artillerie-Projektil mit austauschbarer Nutzlast
US20040041059A1 (en) * 2002-09-03 2004-03-04 Kennedy Kevin D. Device for projectile control
FR2845763B1 (fr) * 2002-10-11 2006-12-01 Tda Armements Sas Systeme autonome de guidage pour munition d'artillerie et munition d'artillerie guidee
US6869043B1 (en) * 2003-03-24 2005-03-22 At&T Corp. Deployable flare with simplified design
US6745978B1 (en) * 2003-03-24 2004-06-08 At&T Corp. Aerodynamic stabilization of a projectile
US6783095B1 (en) * 2003-03-24 2004-08-31 At&T Corp. Deployable flare for aerodynamically stabilizing a projectile
US20090120653A1 (en) * 2003-07-31 2009-05-14 Michael Steven Thomas Fire suppression delivery system
US6981672B2 (en) * 2003-09-17 2006-01-03 Aleiant Techsystems Inc. Fixed canard 2-D guidance of artillery projectiles
US7163176B1 (en) * 2004-01-15 2007-01-16 Raytheon Company 2-D projectile trajectory correction system and method
DE102005039902A1 (de) * 2005-02-04 2006-08-10 Rheinmetall Waffe Munition Gmbh Einrichtung zur Steigerung der Präzision heckflügelstabilisierter Munition
WO2006088687A1 (en) * 2005-02-07 2006-08-24 Bae Systems Information And Electronic Systems Integration Inc. Optically guided munition
US7698983B1 (en) * 2005-11-04 2010-04-20 The United States Of America As Represented By The Secretary Of The Army Reconfigurable fire control apparatus and method
US7566027B1 (en) 2006-01-30 2009-07-28 Alliant Techsystems Inc. Roll orientation using turns-counting fuze
US7611095B1 (en) * 2006-04-28 2009-11-03 The Boeing Company Aerodynamic re-entry vehicle control with active and passive yaw flaps
US7800032B1 (en) * 2006-11-30 2010-09-21 Raytheon Company Detachable aerodynamic missile stabilizing system
US7963442B2 (en) * 2006-12-14 2011-06-21 Simmonds Precision Products, Inc. Spin stabilized projectile trajectory control
US7849800B2 (en) 2007-06-24 2010-12-14 Raytheon Company Hybrid spin/fin stabilized projectile
US8338769B1 (en) * 2008-02-07 2012-12-25 Simmonds Precision Products, Inc. Pyrotechnic fin deployment and retention mechanism
US8124921B2 (en) 2008-04-25 2012-02-28 Raytheon Company Methods and apparatus for guidance of ordnance delivery device
US8049149B2 (en) * 2008-05-16 2011-11-01 Raytheon Company Methods and apparatus for air brake retention and deployment
WO2010011245A2 (en) * 2008-05-20 2010-01-28 Raytheon Company Multi-caliber fuze kit and methods for same
US8193476B2 (en) * 2008-06-13 2012-06-05 Raytheon Company Solid-fuel pellet thrust and control actuation system to maneuver a flight vehicle
WO2010039322A2 (en) 2008-07-09 2010-04-08 Bae Systems Land & Armaments L.P. Roll isolation bearing
US7986265B2 (en) 2008-08-29 2011-07-26 Interstate Electronics Corporation Systems and methods for determining a rotational position of an object
US9040885B2 (en) * 2008-11-12 2015-05-26 General Dynamics Ordnance And Tactical Systems, Inc. Trajectory modification of a spinning projectile
US7964830B2 (en) * 2009-02-23 2011-06-21 Raytheon Company Large cross-section interceptor vehicle and method
WO2010099228A1 (en) 2009-02-24 2010-09-02 Blue Origin, Llc Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods
WO2010141124A1 (en) * 2009-02-24 2010-12-09 Blue Origin, Llc Launch vehicles with fixed and deployable deceleration surfaces, and/or shaped fuel tanks, and associated systems and methods
US8076623B2 (en) * 2009-03-17 2011-12-13 Raytheon Company Projectile control device
IL203642A (en) * 2010-02-01 2014-01-30 Yesaiahu Redler A system and method for optimizing electric current utilization in the control of multiplex motors, and a projectile device containing it
US8026465B1 (en) 2009-05-20 2011-09-27 The United States Of America As Represented By The Secretary Of The Navy Guided fuse with variable incidence panels
EP2443038A4 (de) * 2009-06-15 2017-09-13 Blue Origin, LLC Seelandung von raumabwurffahrzeugen und zugehörige systeme und verfahren
US8424808B2 (en) 2009-06-15 2013-04-23 Blue Origin, Llc Compensating for wind prior to engaging airborne propulsion devices
US8729442B2 (en) * 2009-06-15 2014-05-20 Blue Origin, Llc Predicting and correcting trajectories
US8319164B2 (en) * 2009-10-26 2012-11-27 Nostromo, Llc Rolling projectile with extending and retracting canards
US9939238B1 (en) * 2009-11-09 2018-04-10 Orbital Research Inc. Rotational control actuation system for guiding projectiles
JP4732546B1 (ja) * 2010-11-22 2011-07-27 英世 村上 飛行装置
US8916810B2 (en) * 2011-03-30 2014-12-23 Raytheon Company Steerable spin-stabilized projectile
US8816261B1 (en) * 2011-06-29 2014-08-26 Raytheon Company Bang-bang control using tangentially mounted surfaces
US9228815B2 (en) * 2011-07-04 2016-01-05 Omnitek Partners Llc Very low-power actuation devices
SE535991C2 (sv) 2011-07-07 2013-03-19 Bae Systems Bofors Ab Rotationsstabiliserad styrbar projektil och förfarande därför
US9086259B2 (en) 2011-08-26 2015-07-21 Bae Systems Information And Electronic Systems Integration Inc. Apparatus for deploying stowed control surfaces of a projectile
SE536255C2 (sv) * 2012-02-06 2013-07-23 Bae Systems Bofors Ab Bromspanel för ett tändrör eller en projektil
JP5510979B1 (ja) * 2013-02-15 2014-06-04 防衛省技術研究本部長 抵抗翼構造体
US9487308B2 (en) 2013-03-15 2016-11-08 Blue Origin, Llc Launch vehicles with ring-shaped external elements, and associated systems and methods
US20160187111A1 (en) * 2014-08-10 2016-06-30 Jahangir S Rastegar Methods and Devices For Guidance and Control of High-Spin Stabilized Rounds
US9702673B1 (en) * 2014-09-24 2017-07-11 The United States Of America As Represented By The Secretary Of The Army Projectile tail boom with self-locking fin
KR101628154B1 (ko) * 2015-03-05 2016-06-08 국방과학연구소 수신 신호 세기를 이용한 다중 표적 추적 방법
FR3035205B1 (fr) * 2015-04-20 2018-10-05 Roxel France Dispositif de correction de trajectoire d'un projectile et procede de correction de trajectoire
US9983315B1 (en) 2015-05-29 2018-05-29 Interstate Electronics Corporation Satellite navigation receiver for a rapidly rotating object with improved resistance to jamming
FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
DE102015013913A1 (de) 2015-10-27 2017-04-27 Deutsch Französisches Forschungsinstitut Saint Louis Vollkalibriges, drallstabilisiertes Lenkgeschoss mit einer hohen Reichweite
US10508892B1 (en) 2016-08-15 2019-12-17 The United States Of America As Represented By The Secretary Of The Navy Distributed fuze architecture for highly reliable submunitions
WO2018125942A1 (en) 2016-12-28 2018-07-05 Blue Origin, Llc Vertical landing systems for space vehicles and associated methods
KR101903254B1 (ko) * 2016-12-28 2018-10-01 주식회사 한화 정밀유도키트용 롤 및 피치카나드 구동장치
US11555679B1 (en) 2017-07-07 2023-01-17 Northrop Grumman Systems Corporation Active spin control
US11578956B1 (en) 2017-11-01 2023-02-14 Northrop Grumman Systems Corporation Detecting body spin on a projectile
US11349201B1 (en) 2019-01-24 2022-05-31 Northrop Grumman Systems Corporation Compact antenna system for munition
US11560243B2 (en) 2019-02-22 2023-01-24 Blue Origin, Llc Spacecraft multifunction connecting mechanisms including interchangeable port opening docking mechanisms, and associated systems and methods
US11565628B2 (en) 2019-03-29 2023-01-31 Blue Origin, Llc Spacecraft with increased cargo capacities, and associated systems and methods
US11581632B1 (en) 2019-11-01 2023-02-14 Northrop Grumman Systems Corporation Flexline wrap antenna for projectile
CN111578793B (zh) * 2020-05-07 2022-08-23 北京星途探索科技有限公司 一种有风时火箭整流罩分离的侧滑角控制方法
US11573069B1 (en) 2020-07-02 2023-02-07 Northrop Grumman Systems Corporation Axial flux machine for use with projectiles
US11885601B1 (en) 2021-03-09 2024-01-30 United States Of America As Represented By The Secretary Of The Air Force Variable angle load transfer device
CN113091524B (zh) * 2021-03-18 2022-08-30 中北大学 可重复展开的一维弹道阻力片连续修正机构及方法
US11835319B2 (en) * 2021-06-07 2023-12-05 The Boeing Company Guided projectile and countermeasure systems and methods for use therewith
CN113720213B (zh) * 2021-08-02 2022-10-14 北京理工大学 制导炮弹用船尾及制导炮弹
DE102022002226A1 (de) 2021-08-21 2023-06-15 Kastriot Merlaku Leucht-System, das ein Stadion beleuchten soll
CN114413690B (zh) * 2022-01-18 2024-04-05 南京理工大学 一种用于火箭一子级落区控制的修正系统及方法

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1947884A1 (de) * 1969-09-22 1971-04-01 Rainer Schoeffl Leitwerk insbesondere fuer Raketen
DE2650139C2 (de) * 1976-10-30 1982-04-22 Eltro GmbH, Gesellschaft für Strahlungstechnik, 6900 Heidelberg Verfahren und Vorrichtung zur Korrektur der Flugbahn eines Geschosses
SE8600380L (sv) * 1986-01-29 1987-07-30 Bofors Ab Anordning for att minska projektilspridning
DE3628129C1 (de) * 1986-08-19 1988-03-03 Rheinmetall Gmbh Flugkoerper
US5507452A (en) * 1994-08-24 1996-04-16 Loral Corp. Precision guidance system for aircraft launched bombs
US5379968A (en) * 1993-12-29 1995-01-10 Raytheon Company Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same
US5657947A (en) * 1994-08-24 1997-08-19 Loral Corp. Precision guidance system for aircraft launched bombs
SE511986C2 (sv) * 1995-10-06 2000-01-10 Bofors Ab Sätt att korrigera projektilbanan för rotationsstabiliserande projektiler
US5886257A (en) * 1996-07-03 1999-03-23 The Charles Stark Draper Laboratory, Inc. Autonomous local vertical determination apparatus and methods for a ballistic body
US5775636A (en) 1996-09-30 1998-07-07 The United States Of America As Represented By The Secretary Of The Army Guided artillery projectile and method
US5762291A (en) 1996-10-28 1998-06-09 The United States Of America As Represented By The Secretary Of The Army Drag control module for stabilized projectiles
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
FR2762080B1 (fr) * 1997-04-15 1999-07-02 Tda Armements Sas Dispositif de microgouverne pour la correction de trajectoire de munition stabilisee par rotation
US5826821A (en) * 1997-08-04 1998-10-27 The United States Of America As Represented By The Secretary Of The Army Drag control module for range correction of a spin stabil
DE19740888C2 (de) 1997-09-17 1999-09-02 Rheinmetall W & M Gmbh Verfahren zum autonomen Lenken eines drallstabilisierten Artilleriegeschosses und autonom gelenktes Artilleriegeschoß zur Durchführung des Verfahrens
FR2768809B1 (fr) 1997-09-24 1999-10-15 Giat Ind Sa Projectile d'artillerie de campagne de gros calibre a longue portee
US6310325B1 (en) * 1998-02-18 2001-10-30 Colburn Treat, Llc. Steamer oven with controlled condensing of steam
FR2786561B1 (fr) * 1998-11-30 2001-12-07 Giat Ind Sa Dispositif de freinage en translation d'un projectile sur trajectoire
FR2792400B1 (fr) 1999-04-16 2002-05-03 Giat Ind Sa Dispositif de freinage en translation d'un projectile sur trajectoire
US6345785B1 (en) 2000-01-28 2002-02-12 The United States Of America As Represented By The Secretary Of The Army Drag-brake deployment method and apparatus for range error correction of spinning, gun-launched artillery projectiles
GB2365952A (en) 2000-08-16 2002-02-27 Secr Defence Drag brake for a munition

Also Published As

Publication number Publication date
EP1366339A2 (de) 2003-12-03
EP1366339A4 (de) 2006-07-19
US20030037665A1 (en) 2003-02-27
AU2002245348A1 (en) 2002-08-12
WO2002061363A3 (en) 2003-03-13
US20020117580A1 (en) 2002-08-29
WO2002061363A2 (en) 2002-08-08
EP1366339B1 (de) 2009-07-29
ATE438074T1 (de) 2009-08-15
US6502786B2 (en) 2003-01-07
US6666402B2 (en) 2003-12-23

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Legal Events

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8364 No opposition during term of opposition