FR2730303B1 - Procede pour changer rapidement la direction de deplacement d'un vehicule, notamment d'un missile et machine pour sa mise en oeuvre - Google Patents
Procede pour changer rapidement la direction de deplacement d'un vehicule, notamment d'un missile et machine pour sa mise en oeuvreInfo
- Publication number
- FR2730303B1 FR2730303B1 FR9601289A FR9601289A FR2730303B1 FR 2730303 B1 FR2730303 B1 FR 2730303B1 FR 9601289 A FR9601289 A FR 9601289A FR 9601289 A FR9601289 A FR 9601289A FR 2730303 B1 FR2730303 B1 FR 2730303B1
- Authority
- FR
- France
- Prior art keywords
- missile
- implementing
- vehicle
- movement
- machine
- 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 - Fee Related
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/10—Simultaneous control of position or course in three dimensions
- G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/383,720 US5631830A (en) | 1995-02-03 | 1995-02-03 | Dual-control scheme for improved missle maneuverability |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2730303A1 FR2730303A1 (fr) | 1996-08-09 |
FR2730303B1 true FR2730303B1 (fr) | 2000-02-11 |
Family
ID=23514416
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9601289A Expired - Fee Related FR2730303B1 (fr) | 1995-02-03 | 1996-02-02 | Procede pour changer rapidement la direction de deplacement d'un vehicule, notamment d'un missile et machine pour sa mise en oeuvre |
FR9908299A Withdrawn FR2779246A1 (fr) | 1995-02-03 | 1999-06-29 | Procede et systeme pour changer rapidement la direction de deplacement d'un vehicule se deplacant dans un milieu fluide |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9908299A Withdrawn FR2779246A1 (fr) | 1995-02-03 | 1999-06-29 | Procede et systeme pour changer rapidement la direction de deplacement d'un vehicule se deplacant dans un milieu fluide |
Country Status (3)
Country | Link |
---|---|
US (3) | US5631830A (fr) |
DE (1) | DE19603771A1 (fr) |
FR (2) | FR2730303B1 (fr) |
Families Citing this family (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5631830A (en) | 1995-02-03 | 1997-05-20 | Loral Vought Systems Corporation | Dual-control scheme for improved missle maneuverability |
US6539290B1 (en) * | 1995-06-07 | 2003-03-25 | Dabulamanzi Holdings, Llc | Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation |
US5995882A (en) * | 1997-02-12 | 1999-11-30 | Patterson; Mark R. | Modular autonomous underwater vehicle system |
US6073262A (en) * | 1997-05-30 | 2000-06-06 | United Technologies Corporation | Method and apparatus for estimating an actual magnitude of a physical parameter on the basis of three or more redundant signals |
US6473747B1 (en) * | 1998-01-09 | 2002-10-29 | Raytheon Company | Neural network trajectory command controller |
US6308911B1 (en) | 1998-10-30 | 2001-10-30 | Lockheed Martin Corp. | Method and apparatus for rapidly turning a vehicle in a fluid medium |
AU7836900A (en) * | 1999-09-28 | 2001-04-30 | Cfph, L.L.C. | Systems and methods for transferring items with restricted transferability |
US6502785B1 (en) * | 1999-11-17 | 2003-01-07 | Lockheed Martin Corporation | Three axis flap control system |
US6695251B2 (en) * | 2001-06-19 | 2004-02-24 | Space Systems/Loral, Inc | Method and system for synchronized forward and Aft thrust vector control |
US6629668B1 (en) * | 2002-02-04 | 2003-10-07 | The United States Of America As Represented By The Secretary Of The Army | Jump correcting projectile system |
JP4339016B2 (ja) * | 2002-05-20 | 2009-10-07 | 川崎重工業株式会社 | 推力配分方法及び推力配分装置 |
GB0310010D0 (en) * | 2003-04-29 | 2003-11-26 | Mass Consultants Ltd | Control system for craft and a method of controlling craft |
US7628352B1 (en) * | 2005-11-01 | 2009-12-08 | Richard Low | MEMS control surface for projectile steering |
US7851732B2 (en) * | 2006-03-07 | 2010-12-14 | Raytheon Company | System and method for attitude control of a flight vehicle using pitch-over thrusters |
US7624941B1 (en) * | 2006-05-02 | 2009-12-01 | Orbital Research Inc. | Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators |
US7947938B2 (en) * | 2007-03-15 | 2011-05-24 | Raytheon Company | Methods and apparatus for projectile guidance |
US8546736B2 (en) | 2007-03-15 | 2013-10-01 | Raytheon Company | Modular guided projectile |
US8436283B1 (en) | 2008-07-11 | 2013-05-07 | Davidson Technologies Inc. | System and method for guiding and controlling a missile using high order sliding mode control |
US8173946B1 (en) | 2008-08-26 | 2012-05-08 | Raytheon Company | Method of intercepting incoming projectile |
US11947349B2 (en) | 2012-03-02 | 2024-04-02 | Northrop Grumman Systems Corporation | Methods and apparatuses for engagement management of aerial threats |
US9551552B2 (en) | 2012-03-02 | 2017-01-24 | Orbital Atk, Inc. | Methods and apparatuses for aerial interception of aerial threats |
US9501055B2 (en) | 2012-03-02 | 2016-11-22 | Orbital Atk, Inc. | Methods and apparatuses for engagement management of aerial threats |
US11313650B2 (en) | 2012-03-02 | 2022-04-26 | Northrop Grumman Systems Corporation | Methods and apparatuses for aerial interception of aerial threats |
US9170070B2 (en) | 2012-03-02 | 2015-10-27 | Orbital Atk, Inc. | Methods and apparatuses for active protection from aerial threats |
RU2512047C1 (ru) * | 2012-11-29 | 2014-04-10 | Открытое акционерное общество "Конструкторское бюро приборостроения" | Управляемая пуля |
US9068808B2 (en) | 2013-01-17 | 2015-06-30 | Raytheon Company | Air vehicle with bilateral steering thrusters |
US9121680B2 (en) | 2013-01-17 | 2015-09-01 | Raytheon Company | Air vehicle with control surfaces and vectored thrust |
DE102014004251A1 (de) * | 2013-11-20 | 2015-06-25 | Mbda Deutschland Gmbh | Lenkflugkörper und Verfahren zum Lenken eines Lenkflugkörpers |
CN104019701B (zh) * | 2014-05-28 | 2016-07-06 | 中国人民解放军海军航空工程学院 | 一种利用直接力气动力复合控制的前向拦截制导方法 |
US10113844B1 (en) | 2016-11-21 | 2018-10-30 | Lockheed Martin Corporation | Missile, chemical plasm steering system, and method |
US10914559B1 (en) | 2016-11-21 | 2021-02-09 | Lockheed Martin Corporation | Missile, slot thrust attitude controller system, and method |
CN108168381B (zh) * | 2018-01-04 | 2019-10-08 | 北京理工大学 | 一种多枚导弹协同作战的控制方法 |
CN114417730B (zh) * | 2022-01-27 | 2022-09-16 | 哈尔滨逐宇航天科技有限责任公司 | 基于集成神经网络的飞行器滑翔段飞行范围在线预示方法 |
DE102022001289A1 (de) * | 2022-04-13 | 2023-10-19 | Diehl Defence Gmbh & Co. Kg | Verfahren zum Ausweichen eines Flugkörpers vor einem Abfangflugkörper |
Family Cites Families (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3139033A (en) | 1959-07-23 | 1964-06-30 | Ernst D Geissler | Aerodynamically stable missile |
US3034434A (en) * | 1960-03-08 | 1962-05-15 | Frank H Swaim | Thrust vector control system |
US3362658A (en) | 1964-07-30 | 1968-01-09 | Honeywell Inc | Vehicle trajectory control apparatus |
US5439188A (en) | 1964-09-04 | 1995-08-08 | Hughes Missile Systems Company | Control system |
US3282541A (en) * | 1965-02-19 | 1966-11-01 | James E Webb | Attitude control system for sounding rockets |
GB1605390A (en) | 1965-03-25 | 1995-04-26 | Short Brothers & Harland Ltd | Improvements relating to control systems for missiles |
CH520316A (de) | 1970-02-27 | 1972-03-15 | Oerlikon Buehrle Ag | Drallstabilisiertes Raketengeschoss |
US4116404A (en) | 1977-07-22 | 1978-09-26 | The United States Of America As Represented By The Secretary Of The Army | Automatic balancing concept |
GB2203223B (en) | 1977-08-18 | 1989-02-15 | British Aerospace | Control means |
US4171115A (en) | 1977-12-12 | 1979-10-16 | Sperry Rand Corporation | Stability augmentation system for relaxed static stability aircraft |
FR2536720A1 (fr) | 1982-11-29 | 1984-06-01 | Aerospatiale | Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux et missile comportant un tel systeme |
DE3317583C2 (de) | 1983-05-13 | 1986-01-23 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Vorrichtung mit einer von einer Treibmittelquelle versorgten Düsenanordnung |
GB2208017B (en) | 1983-11-25 | 1989-07-05 | British Aerospace | Guidance systems |
US4699333A (en) | 1984-11-07 | 1987-10-13 | The Boeing Company | On-board flight control panel system |
US4624424A (en) | 1984-11-07 | 1986-11-25 | The Boeing Company | On-board flight control drag actuator system |
FR2607917A1 (fr) | 1986-12-08 | 1988-06-10 | Roche Kerandraon Oliver | Guidage par infrarouge simplifie pour tout projectile |
DE3738580A1 (de) | 1987-11-13 | 1989-06-01 | Diehl Gmbh & Co | Gelenktes artillerieprojektil mit flugbahnregler |
GB8803164D0 (en) * | 1988-02-11 | 1988-08-24 | British Aerospace | Reaction control system |
DE3826615C2 (de) | 1988-08-05 | 1995-06-08 | Rheinmetall Gmbh | Gierwinkelfreies Geschoß |
US4867393A (en) * | 1988-08-17 | 1989-09-19 | Morton Thiokol, Inc. | Reduced fin span thrust vector controlled pulsed tactical missile |
US5058836A (en) | 1989-12-27 | 1991-10-22 | General Electric Company | Adaptive autopilot |
FR2659733B1 (fr) | 1990-03-14 | 1994-07-01 | Aerospatiale | Systeme pour le pilotage d'un missile au moyen de tuyeres laterales. |
FR2659734B1 (fr) | 1990-03-14 | 1992-07-03 | Aerospatiale | Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux. |
US5070761A (en) | 1990-08-07 | 1991-12-10 | The United States Of America As Represented By The Secretary Of The Navy | Venting apparatus for controlling missile underwater trajectory |
US5094406A (en) * | 1991-01-07 | 1992-03-10 | The Boeing Company | Missile control system using virtual autopilot |
US5088658A (en) * | 1991-03-20 | 1992-02-18 | Raytheon Company | Fin command mixing method |
US5259569A (en) * | 1992-02-05 | 1993-11-09 | Hughes Missile Systems Company | Roll damper for thrust vector controlled missile |
US5349532A (en) | 1992-04-28 | 1994-09-20 | Space Systems/Loral | Spacecraft attitude control and momentum unloading using gimballed and throttled thrusters |
RU2021577C1 (ru) * | 1992-06-30 | 1994-10-15 | Машиностроительное Конструкторское Бюро "Факел" | Способ управления снарядом |
FR2699610B1 (fr) * | 1992-12-22 | 1995-02-10 | Aerospatiale | Dispositif d'actionnement d'un organe mécanique, notamment pour le pilotage en force d'un missile, et missile équipé dudit dispositif. |
SE501082C2 (sv) | 1993-03-30 | 1994-11-07 | Bofors Ab | Sätt och anordning för att ge en luftburen stridsdel ett önskat rörelsemönster |
US5505408A (en) | 1993-10-19 | 1996-04-09 | Versatron Corporation | Differential yoke-aerofin thrust vector control system |
US5452864A (en) | 1994-03-31 | 1995-09-26 | Alliant Techsystems Inc. | Electro-mechanical roll control apparatus and method |
US5593109A (en) | 1995-01-10 | 1997-01-14 | Lucas Western, Inc. | Actuator system and method |
US5631830A (en) | 1995-02-03 | 1997-05-20 | Loral Vought Systems Corporation | Dual-control scheme for improved missle maneuverability |
US5806791A (en) | 1995-05-26 | 1998-09-15 | Raytheon Company | Missile jet vane control system and method |
US5590850A (en) | 1995-06-05 | 1997-01-07 | Hughes Missile Systems Company | Blended missile autopilot |
-
1995
- 1995-02-03 US US08/383,720 patent/US5631830A/en not_active Ceased
-
1996
- 1996-02-02 DE DE19603771A patent/DE19603771A1/de not_active Withdrawn
- 1996-02-02 FR FR9601289A patent/FR2730303B1/fr not_active Expired - Fee Related
-
1997
- 1997-05-19 US US08/858,511 patent/US5835869A/en not_active Expired - Lifetime
-
1999
- 1999-05-20 US US09/315,919 patent/USRE37331E1/en not_active Expired - Lifetime
- 1999-06-29 FR FR9908299A patent/FR2779246A1/fr not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
USRE37331E1 (en) | 2001-08-14 |
US5835869A (en) | 1998-11-10 |
US5631830A (en) | 1997-05-20 |
FR2730303A1 (fr) | 1996-08-09 |
DE19603771A1 (de) | 1996-08-08 |
FR2779246A1 (fr) | 1999-12-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
ST | Notification of lapse |
Effective date: 20131031 |