ZA200802165B - Projectile trajectory control system - Google Patents
Projectile trajectory control systemInfo
- Publication number
- ZA200802165B ZA200802165B ZA200802165A ZA200802165A ZA200802165B ZA 200802165 B ZA200802165 B ZA 200802165B ZA 200802165 A ZA200802165 A ZA 200802165A ZA 200802165 A ZA200802165 A ZA 200802165A ZA 200802165 B ZA200802165 B ZA 200802165B
- Authority
- ZA
- South Africa
- Prior art keywords
- control system
- trajectory control
- projectile trajectory
- projectile
- trajectory
- Prior art date
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
-
- 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
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US71567305P | 2005-09-09 | 2005-09-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ZA200802165B true ZA200802165B (en) | 2009-10-28 |
Family
ID=37836503
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ZA200802165A ZA200802165B (en) | 2005-09-09 | 2008-03-07 | Projectile trajectory control system |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US7354017B2 (xx) |
| EP (1) | EP1929236B1 (xx) |
| ES (1) | ES2398968T3 (xx) |
| IL (1) | IL190009A (xx) |
| NO (1) | NO20081272L (xx) |
| PL (1) | PL1929236T3 (xx) |
| WO (1) | WO2007030687A2 (xx) |
| ZA (1) | ZA200802165B (xx) |
Families Citing this family (71)
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|---|---|---|---|---|
| US10408587B1 (en) * | 2006-04-20 | 2019-09-10 | United States Of America As Represented By The Secretary Of The Army | On-board power generation for rolling motor missiles |
| US7696459B2 (en) | 2007-06-12 | 2010-04-13 | Hr Textron, Inc. | Techniques for articulating a nose member of a guidable projectile |
| US7791007B2 (en) | 2007-06-21 | 2010-09-07 | Woodward Hrt, Inc. | Techniques for providing surface control to a guidable projectile |
| US7856929B2 (en) | 2007-06-29 | 2010-12-28 | Taser International, Inc. | Systems and methods for deploying an electrode using torsion |
| US20110168048A1 (en) * | 2007-09-17 | 2011-07-14 | Ruhlman James D | Multi-Faceted Structure for Bombs and Warheads Including Penetrating Warheads |
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| US9939238B1 (en) | 2009-11-09 | 2018-04-10 | Orbital Research Inc. | Rotational control actuation system for guiding projectiles |
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| US8237096B1 (en) | 2010-08-19 | 2012-08-07 | Interstate Electronics Corporation, A Subsidiary Of L-3 Communications Corporation | Mortar round glide kit |
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| US8916810B2 (en) | 2011-03-30 | 2014-12-23 | Raytheon Company | Steerable spin-stabilized projectile |
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| US8993948B2 (en) * | 2011-08-23 | 2015-03-31 | Raytheon Company | Rolling vehicle having collar with passively controlled ailerons |
| US8561898B2 (en) | 2011-11-18 | 2013-10-22 | Simmonds Precision Products, Inc. | Ratio-metric horizon sensing using an array of thermopiles |
| US8698059B2 (en) | 2012-05-03 | 2014-04-15 | Raytheon Company | Deployable lifting surface for air vehicle |
| DE102012020740B4 (de) * | 2012-10-23 | 2014-11-13 | Diehl Bgt Defence Gmbh & Co. Kg | Verfahren zum Umrüsten einer Munition für eine schulterstützbare Waffe |
| IL224075A (en) * | 2012-12-31 | 2017-11-30 | Bae Systems Rokar Int Ltd | Cheap shell kit and method of use |
| US9012825B2 (en) | 2013-01-23 | 2015-04-21 | Simmonds Precision Products, Inc. | Systems and methods for retaining and deploying canards |
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| WO2014172118A2 (en) * | 2013-04-17 | 2014-10-23 | Saudi Arabian Oil Company | Apparatus for driving and maneuvering wireline logging tools in high-angled wells |
| FR3011919B1 (fr) * | 2013-10-15 | 2017-05-19 | Nexter Munitions | Dispositif de freinage en rotation d'une enveloppe d'une charge utile, et projectile gyrostabilise equipe d'un tel dispositif |
| USD729896S1 (en) | 2013-12-19 | 2015-05-19 | Elio Martinez | Air vehicle rotatable wind-driven sleeve |
| TWI551513B (zh) * | 2014-03-18 | 2016-10-01 | 國立屏東科技大學 | 減轉裝置 |
| CN104089546B (zh) * | 2014-04-29 | 2015-09-30 | 北京理工大学 | 弹体的可变气动布局结构 |
| US9464876B2 (en) * | 2014-05-30 | 2016-10-11 | General Dynamics Ordnance and Tacital Systems, Inc. | Trajectory modification of a spinning projectile by controlling the roll orientation of a decoupled portion of the projectile that has actuated aerodynamic surfaces |
| US9724502B2 (en) * | 2015-07-10 | 2017-08-08 | Coloplast A/S | Dilator and method for penile prosthetic implantation |
| DE102015009980B4 (de) * | 2015-07-31 | 2023-04-27 | Junghans Microtec Gmbh | Kurskorrekturvorrichtung und Verfahren für Zünder von Drallgeschossen |
| US11371814B2 (en) * | 2015-08-24 | 2022-06-28 | Leigh Aerosystems Corporation | Ground-projectile guidance system |
| FR3041744B1 (fr) * | 2015-09-29 | 2018-08-17 | Nexter Munitions | Projectile d'artillerie ayant une phase pilotee. |
| IL242320B (en) * | 2015-10-28 | 2022-02-01 | Israel Aerospace Ind Ltd | Projectile, and system and method for steering a projectile |
| US10118696B1 (en) | 2016-03-31 | 2018-11-06 | Steven M. Hoffberg | Steerable rotating projectile |
| US10288393B2 (en) * | 2016-08-05 | 2019-05-14 | Raytheon Company | Flight vehicle with control surfaces usable as momentum wheels |
| 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 |
| US10618668B2 (en) * | 2016-09-06 | 2020-04-14 | Analytical Mechanics Associates, Inc. | Systems and apparatus for controlling movement of objects through a fluid |
| CN106500550A (zh) * | 2016-12-15 | 2017-03-15 | 福州幻科机电科技有限公司 | 带有遥控滑翔翼尾舵翼的逃逸塔整流罩助推火箭 |
| US11555679B1 (en) | 2017-07-07 | 2023-01-17 | Northrop Grumman Systems Corporation | Active spin control |
| US12031802B2 (en) | 2017-07-26 | 2024-07-09 | Northrop Grumman Systems Corporation | Despun wing control system for guided projectile maneuvers |
| US11578956B1 (en) | 2017-11-01 | 2023-02-14 | Northrop Grumman Systems Corporation | Detecting body spin on a projectile |
| US11712637B1 (en) | 2018-03-23 | 2023-08-01 | Steven M. Hoffberg | Steerable disk or ball |
| US11300389B1 (en) * | 2018-05-04 | 2022-04-12 | The United States Of America As Represented By The Secretary Of The Army | Slip baseplate |
| US11808868B2 (en) | 2018-08-31 | 2023-11-07 | Bae Systems Information And Electronic Systems Integration Inc. | Early velocity measurement for projectiles by detecting spin |
| IL263880B (en) | 2018-12-20 | 2022-02-01 | Elbit Systems Rokar Ltd | Projectile fuze assembly and methods of assembling and use |
| US11067371B2 (en) * | 2019-03-22 | 2021-07-20 | Bae Systems Information And Electronic Systems Integration Inc. | Trimmable tail kit rudder |
| US11573069B1 (en) | 2020-07-02 | 2023-02-07 | Northrop Grumman Systems Corporation | Axial flux machine for use with projectiles |
| US12123687B2 (en) | 2020-07-30 | 2024-10-22 | Bae Systems Plc | Steerable projectile |
| EP3945279A1 (en) * | 2020-07-30 | 2022-02-02 | BAE SYSTEMS plc | Steerable projectile |
| US11650033B2 (en) * | 2020-12-04 | 2023-05-16 | Bae Systems Information And Electronic Systems Integration Inc. | Control plate-based control actuation system |
| US11747121B2 (en) | 2020-12-04 | 2023-09-05 | Bae Systems Information And Electronic Systems Integration Inc. | Despin maintenance motor |
| CN112923805A (zh) * | 2021-01-20 | 2021-06-08 | 西北工业大学 | 一种小型高机动导弹气动布局 |
| SE547810C2 (sv) * | 2021-05-19 | 2025-12-02 | Bae Systems Bofors Ab | Projektil och tändrör för anordning på projektilen |
| US12313389B1 (en) | 2022-03-11 | 2025-05-27 | Northrop Grumman Systems Corporation | Tunable safe and arming devices and methods of manufacture |
| CN116045743A (zh) * | 2022-12-07 | 2023-05-02 | 南京航空航天大学 | 一种自启动自转旋翼式火箭回收系统及其方法 |
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| US1531624A (en) * | 1924-08-21 | 1925-03-31 | William K Richardson | Projectile |
| US2886149A (en) * | 1955-07-18 | 1959-05-12 | Baermann Max | Magnetic friction brake or clutch |
| US3260205A (en) * | 1964-09-28 | 1966-07-12 | Aerojet General Co | Fin actuated spin vane control device and method |
| GB1605390A (en) * | 1965-03-25 | 1995-04-26 | Short Brothers & Harland Ltd | Improvements relating to control systems for missiles |
| FR2321723A1 (fr) * | 1975-07-29 | 1977-03-18 | Thomson Brandt | Systeme de controle d'attitude et engin equipe d'un tel systeme |
| DE2721656A1 (de) * | 1977-05-13 | 1978-11-16 | Ver Flugtechnische Werke | Stellanordnung zur steuerung von flugkoerpern |
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| US4523728A (en) * | 1983-03-07 | 1985-06-18 | Ford Aerospace & Communications Corporation | Passive auto-erecting alignment wings for long rod penetrator |
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| 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 |
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| US6727485B2 (en) * | 2001-05-25 | 2004-04-27 | Omnitek Partners Llc | Methods and apparatus for increasing aerodynamic performance of projectiles |
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| AUPR583001A0 (en) * | 2001-06-20 | 2001-07-12 | Kusic, Tom | Aircraft spiralling mechanism |
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| US6880780B1 (en) * | 2003-03-17 | 2005-04-19 | General Dynamics Ordnance And Tactical Systems, Inc. | Cover ejection and fin deployment system for a gun-launched projectile |
| US8661980B1 (en) | 2003-05-08 | 2014-03-04 | Lone Star Ip Holdings, Lp | Weapon and weapon system employing the same |
| US6869044B2 (en) * | 2003-05-23 | 2005-03-22 | Raytheon Company | Missile with odd symmetry tail fins |
| US6752352B1 (en) * | 2003-07-07 | 2004-06-22 | Michael C. May | Gun-launched rolling projectile actuator |
| US6981672B2 (en) * | 2003-09-17 | 2006-01-03 | Aleiant Techsystems Inc. | Fixed canard 2-D guidance of artillery projectiles |
| US7255304B2 (en) * | 2003-12-08 | 2007-08-14 | General Dynamics Ordnance And Tactical Systems, Inc. | Tandem motor actuator |
-
2006
- 2006-09-08 EP EP06814322A patent/EP1929236B1/en not_active Revoked
- 2006-09-08 US US11/530,194 patent/US7354017B2/en active Active
- 2006-09-08 ES ES06814322T patent/ES2398968T3/es active Active
- 2006-09-08 PL PL06814322T patent/PL1929236T3/pl unknown
- 2006-09-08 WO PCT/US2006/034980 patent/WO2007030687A2/en not_active Ceased
-
2008
- 2008-03-06 IL IL190009A patent/IL190009A/en active IP Right Grant
- 2008-03-07 ZA ZA200802165A patent/ZA200802165B/xx unknown
- 2008-03-11 NO NO20081272A patent/NO20081272L/no not_active Application Discontinuation
Also Published As
| Publication number | Publication date |
|---|---|
| IL190009A0 (en) | 2008-08-07 |
| WO2007030687A3 (en) | 2007-12-21 |
| NO20081272L (no) | 2008-04-04 |
| PL1929236T3 (pl) | 2013-06-28 |
| US20080061188A1 (en) | 2008-03-13 |
| EP1929236A4 (en) | 2010-05-19 |
| ES2398968T3 (es) | 2013-03-22 |
| IL190009A (en) | 2014-04-30 |
| EP1929236A2 (en) | 2008-06-11 |
| EP1929236B1 (en) | 2012-11-07 |
| WO2007030687A2 (en) | 2007-03-15 |
| US7354017B2 (en) | 2008-04-08 |
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