FR2785381B1 - Procede et dispositif pour permettre l'execution, par un vehicule, d'un virage rapide dans un milieu fluide - Google Patents
Procede et dispositif pour permettre l'execution, par un vehicule, d'un virage rapide dans un milieu fluideInfo
- Publication number
- FR2785381B1 FR2785381B1 FR9913457A FR9913457A FR2785381B1 FR 2785381 B1 FR2785381 B1 FR 2785381B1 FR 9913457 A FR9913457 A FR 9913457A FR 9913457 A FR9913457 A FR 9913457A FR 2785381 B1 FR2785381 B1 FR 2785381B1
- Authority
- FR
- France
- Prior art keywords
- execute
- allowing
- vehicle
- fluid medium
- fast turn
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
- B63H25/02—Initiating means for steering, for slowing down, otherwise than by use of propulsive elements, or for dynamic anchoring
- B63H25/04—Initiating means for steering, for slowing down, otherwise than by use of propulsive elements, or for dynamic anchoring automatic, e.g. reacting to compass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
- B64C15/12—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (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 |
|---|---|---|---|
| US09/183,502 US6308911B1 (en) | 1998-10-30 | 1998-10-30 | Method and apparatus for rapidly turning a vehicle in a fluid medium |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2785381A1 FR2785381A1 (fr) | 2000-05-05 |
| FR2785381B1 true FR2785381B1 (fr) | 2003-09-05 |
Family
ID=22673079
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR9913457A Expired - Fee Related FR2785381B1 (fr) | 1998-10-30 | 1999-10-27 | Procede et dispositif pour permettre l'execution, par un vehicule, d'un virage rapide dans un milieu fluide |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6308911B1 (fr) |
| DE (1) | DE19949640A1 (fr) |
| FR (1) | FR2785381B1 (fr) |
| GB (1) | GB2343425B (fr) |
| IL (1) | IL132444A0 (fr) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6502785B1 (en) * | 1999-11-17 | 2003-01-07 | Lockheed Martin Corporation | Three axis flap control system |
| 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 |
| US8417395B1 (en) * | 2003-01-03 | 2013-04-09 | Orbitol Research Inc. | Hierarchical closed-loop flow control system for aircraft, missiles and munitions |
| IL177527A (en) * | 2006-08-16 | 2014-04-30 | Rafael Advanced Defense Sys | Missile survey targets |
| CN102466429A (zh) * | 2011-07-04 | 2012-05-23 | 北京科实医学图像技术研究所 | 宇宙火箭推力装置的改进方案 |
| RU2489329C1 (ru) * | 2012-03-27 | 2013-08-10 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Ракета-носитель |
| IN2014DN10149A (fr) * | 2012-04-30 | 2015-08-21 | Univ Pennsylvania | |
| CN103440406B (zh) * | 2013-08-13 | 2016-08-10 | 北京电子工程总体研究所 | 一种离线迭代质点弹道计算方法 |
| DE102014004251A1 (de) * | 2013-11-20 | 2015-06-25 | Mbda Deutschland Gmbh | Lenkflugkörper und Verfahren zum Lenken eines Lenkflugkörpers |
| JP2016540211A (ja) | 2013-11-27 | 2016-12-22 | ザ トラスティーズ オブ ザ ユニバーシティー オブ ペンシルバニア | 回転翼型小型飛行体(mav)での屋内環境及び屋外環境における安定自律飛行のためのマルチセンサの融合 |
| RU2547034C1 (ru) * | 2013-12-13 | 2015-04-10 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" | Способ управления движением жидкостной ракеты космического назначения после команды на выключение маршевого двигателя отработавшей ступени |
| RU2596004C2 (ru) * | 2015-01-20 | 2016-08-27 | Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) | Способ управления движением космического аппарата на активном участке его выведения на орбиту искусственного спутника планеты |
| WO2016123201A1 (fr) | 2015-01-27 | 2016-08-04 | The Trustees Of The University Of Pennsylvania | Systèmes, dispositifs et procédés de télédétection robotique pour agriculture de précision |
| US10037028B2 (en) | 2015-07-24 | 2018-07-31 | The Trustees Of The University Of Pennsylvania | Systems, devices, and methods for on-board sensing and control of micro aerial vehicles |
| WO2017095493A2 (fr) | 2015-09-11 | 2017-06-08 | The Trustees Of The University Of Pennsylvania | Systèmes et procédés de production de trajectoires sûres pour équipes à véhicules multiples |
Family Cites Families (44)
| 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 |
| US3984072A (en) * | 1974-10-02 | 1976-10-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Attitude control system |
| DE2721656A1 (de) * | 1977-05-13 | 1978-11-16 | Ver Flugtechnische Werke | Stellanordnung zur steuerung von flugkoerpern |
| 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 |
| EP0058258A1 (fr) | 1981-02-13 | 1982-08-25 | Geoffrey Martin Spence | Système de guidage pour projectile |
| 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 |
| US4624424A (en) | 1984-11-07 | 1986-11-25 | The Boeing Company | On-board flight control drag actuator system |
| US4699333A (en) | 1984-11-07 | 1987-10-13 | The Boeing Company | On-board flight control panel 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 |
| US5129604A (en) * | 1989-07-17 | 1992-07-14 | General Dynamics Corporation, Pomona Div. | Lateral thrust assembly for missiles |
| DE59004020D1 (de) * | 1989-09-19 | 1994-02-10 | Diehl Gmbh & Co | Bahnkorrigierbares Projektil. |
| 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 |
| GB9618126D0 (en) | 1996-08-29 | 1997-01-08 | British Aerospace | Thruster pack for missile control |
| US5984229A (en) | 1997-06-02 | 1999-11-16 | Boeing North American, Inc. | Extremely short takeoff and landing of aircraft using multi-axis thrust vectoring |
-
1998
- 1998-10-30 US US09/183,502 patent/US6308911B1/en not_active Expired - Lifetime
-
1999
- 1999-09-17 GB GB9922083A patent/GB2343425B/en not_active Expired - Fee Related
- 1999-10-07 DE DE19949640A patent/DE19949640A1/de not_active Withdrawn
- 1999-10-18 IL IL13244499A patent/IL132444A0/xx not_active IP Right Cessation
- 1999-10-27 FR FR9913457A patent/FR2785381B1/fr not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US6308911B1 (en) | 2001-10-30 |
| FR2785381A1 (fr) | 2000-05-05 |
| GB9922083D0 (en) | 1999-11-17 |
| IL132444A0 (en) | 2001-03-19 |
| DE19949640A1 (de) | 2000-05-25 |
| GB2343425B (en) | 2003-01-15 |
| GB2343425A (en) | 2000-05-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |
Effective date: 20110630 |