FR2686687B1 - Procede et dispositif de pilotage d'un projectile selon ses trois axes de roulis tangage et lacet. - Google Patents

Procede et dispositif de pilotage d'un projectile selon ses trois axes de roulis tangage et lacet.

Info

Publication number
FR2686687B1
FR2686687B1 FR8705701A FR8705701A FR2686687B1 FR 2686687 B1 FR2686687 B1 FR 2686687B1 FR 8705701 A FR8705701 A FR 8705701A FR 8705701 A FR8705701 A FR 8705701A FR 2686687 B1 FR2686687 B1 FR 2686687B1
Authority
FR
France
Prior art keywords
tangage
lace
axes
roll
driving
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
FR8705701A
Other languages
English (en)
Other versions
FR2686687A1 (fr
Inventor
Hubert Barre
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.)
Thomson Brandt Armements SA
Original Assignee
Thomson Brandt Armements SA
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 Thomson Brandt Armements SA filed Critical Thomson Brandt Armements SA
Priority to FR8705701A priority Critical patent/FR2686687B1/fr
Priority to IT8867332A priority patent/IT1237006B/it
Priority to DE3812588A priority patent/DE3812588A1/de
Priority to SE8801461A priority patent/SE8801461D0/xx
Priority to GB8809391A priority patent/GB2265342B/en
Publication of FR2686687A1 publication Critical patent/FR2686687A1/fr
Application granted granted Critical
Publication of FR2686687B1 publication Critical patent/FR2686687B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control
    • 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
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR8705701A 1987-04-22 1987-04-22 Procede et dispositif de pilotage d'un projectile selon ses trois axes de roulis tangage et lacet. Expired - Fee Related FR2686687B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR8705701A FR2686687B1 (fr) 1987-04-22 1987-04-22 Procede et dispositif de pilotage d'un projectile selon ses trois axes de roulis tangage et lacet.
IT8867332A IT1237006B (it) 1987-04-22 1988-04-12 Procedimento e dispositivo di pilotaggio di un proiettile secondo tre assi di rollio, beccheggio ed imbardatura
DE3812588A DE3812588A1 (de) 1987-04-22 1988-04-15 Verfahren und Vorrichtung zur Lenkung eines Projektils um seine drei Achsen
SE8801461A SE8801461D0 (sv) 1987-04-22 1988-04-20 Projektil
GB8809391A GB2265342B (en) 1987-04-22 1988-04-21 Method and device for controlling a projectile about its three axes of roll,pitch and yaw

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8705701A FR2686687B1 (fr) 1987-04-22 1987-04-22 Procede et dispositif de pilotage d'un projectile selon ses trois axes de roulis tangage et lacet.

Publications (2)

Publication Number Publication Date
FR2686687A1 FR2686687A1 (fr) 1993-07-30
FR2686687B1 true FR2686687B1 (fr) 1994-05-13

Family

ID=9350375

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8705701A Expired - Fee Related FR2686687B1 (fr) 1987-04-22 1987-04-22 Procede et dispositif de pilotage d'un projectile selon ses trois axes de roulis tangage et lacet.

Country Status (5)

Country Link
DE (1) DE3812588A1 (fr)
FR (1) FR2686687B1 (fr)
GB (1) GB2265342B (fr)
IT (1) IT1237006B (fr)
SE (1) SE8801461D0 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE501082C2 (sv) * 1993-03-30 1994-11-07 Bofors Ab Sätt och anordning för att ge en luftburen stridsdel ett önskat rörelsemönster
GB9618126D0 (en) * 1996-08-29 1997-01-08 British Aerospace Thruster pack for missile control
DE102005052474B3 (de) 2005-11-03 2007-07-12 Junghans Feinwerktechnik Gmbh & Co. Kg Drallstbilisiertes Artillerieprojektil
US7851732B2 (en) * 2006-03-07 2010-12-14 Raytheon Company System and method for attitude control of a flight vehicle using pitch-over thrusters
US8800913B2 (en) * 2009-07-30 2014-08-12 Raytheon Company Methods and apparatus for a tandem divert and attitude control system
FR2975481B1 (fr) * 2011-05-19 2017-09-01 Snecma Propulsion Solide Systeme pour le pilotage en force et le controle d'attitude en vol d'un vehicule et engin comportant un tel systeme
US9551552B2 (en) 2012-03-02 2017-01-24 Orbital Atk, Inc. 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
US11313650B2 (en) 2012-03-02 2022-04-26 Northrop Grumman Systems Corporation Methods and apparatuses for aerial interception of aerial threats
US11947349B2 (en) 2012-03-02 2024-04-02 Northrop Grumman Systems Corporation Methods and apparatuses for engagement management of aerial threats
US9501055B2 (en) 2012-03-02 2016-11-22 Orbital Atk, Inc. Methods and apparatuses for engagement management of aerial threats

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2055088A1 (de) * 1970-11-10 1972-05-18 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum Erzeugen von Steuermomenten bei raketengetriebenen Flugkörpern
US4384690A (en) * 1981-03-06 1983-05-24 The United States Of America As Represented By The Secretary Of The Navy Thrust vector control for large deflection angles
FR2508414B1 (fr) * 1981-06-30 1985-06-07 Thomson Brandt Dispositif de pilotage par jets de gaz pour engin guide
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
WO1984002975A1 (fr) * 1983-01-20 1984-08-02 Ford Aerospace & Communication Systeme de guidage par combustion d'air sous pression dynamique
DE3429798C1 (de) * 1984-08-13 1985-12-12 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur Korrektur der Flugbahn eines Geschosses
DE3531686A1 (de) * 1985-09-05 1987-03-12 Rheinmetall Gmbh Steuerblock
GB8611406D0 (en) * 1986-05-09 1986-08-20 Lucas Ind Plc Missile flight control system

Also Published As

Publication number Publication date
IT1237006B (it) 1993-05-13
FR2686687A1 (fr) 1993-07-30
GB2265342B (en) 1994-05-18
GB2265342A (en) 1993-09-29
IT8867332A0 (it) 1988-04-12
SE8801461D0 (sv) 1988-04-20
GB8809391D0 (en) 1993-05-26
DE3812588A1 (de) 1993-12-09

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Legal Events

Date Code Title Description
ST Notification of lapse