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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 fluide

Info

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
Application number
FR9913457A
Other languages
English (en)
Other versions
FR2785381A1 (fr
Inventor
Wayne K Schroeder
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.)
Lockheed Martin Corp
Original Assignee
Lockheed Corp
Lockheed Martin Corp
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 Lockheed Corp, Lockheed Martin Corp filed Critical Lockheed Corp
Publication of FR2785381A1 publication Critical patent/FR2785381A1/fr
Application granted granted Critical
Publication of FR2785381B1 publication Critical patent/FR2785381B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H25/00Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/02Initiating means for steering, for slowing down, otherwise than by use of propulsive elements, or for dynamic anchoring
    • B63H25/04Initiating means for steering, for slowing down, otherwise than by use of propulsive elements, or for dynamic anchoring automatic, e.g. reacting to compass
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H25/00Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C15/00Attitude, flight direction, or altitude control by jet reaction
    • B64C15/02Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
    • B64C15/12Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/62Steering 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)
FR9913457A 1998-10-30 1999-10-27 Procede et dispositif pour permettre l'execution, par un vehicule, d'un virage rapide dans un milieu fluide Expired - Fee Related FR2785381B1 (fr)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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