IT1237006B - Procedimento e dispositivo di pilotaggio di un proiettile secondo tre assi di rollio, beccheggio ed imbardatura - Google Patents

Procedimento e dispositivo di pilotaggio di un proiettile secondo tre assi di rollio, beccheggio ed imbardatura

Info

Publication number
IT1237006B
IT1237006B IT8867332A IT6733288A IT1237006B IT 1237006 B IT1237006 B IT 1237006B IT 8867332 A IT8867332 A IT 8867332A IT 6733288 A IT6733288 A IT 6733288A IT 1237006 B IT1237006 B IT 1237006B
Authority
IT
Italy
Prior art keywords
piloting
harness
picking
procedure
rolling axes
Prior art date
Application number
IT8867332A
Other languages
English (en)
Italian (it)
Other versions
IT8867332A0 (it
Inventor
Hubert Barre
Original Assignee
Thomson Brandt Armements
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 filed Critical Thomson Brandt Armements
Publication of IT8867332A0 publication Critical patent/IT8867332A0/it
Application granted granted Critical
Publication of IT1237006B publication Critical patent/IT1237006B/it

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
IT8867332A 1987-04-22 1988-04-12 Procedimento e dispositivo di pilotaggio di un proiettile secondo tre assi di rollio, beccheggio ed imbardatura IT1237006B (it)

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
IT8867332A0 IT8867332A0 (it) 1988-04-12
IT1237006B true IT1237006B (it) 1993-05-13

Family

ID=9350375

Family Applications (1)

Application Number Title Priority Date Filing Date
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

Country Status (5)

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

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
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
US9501055B2 (en) 2012-03-02 2016-11-22 Orbital Atk, Inc. Methods and apparatuses for engagement management of aerial threats
US11947349B2 (en) 2012-03-02 2024-04-02 Northrop Grumman Systems Corporation 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
DE3378783D1 (en) * 1983-01-20 1989-02-02 Ford Aerospace & Communication Ram air combustion steering system for a guided missile
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
FR2686687A1 (fr) 1993-07-30
FR2686687B1 (fr) 1994-05-13
SE8801461D0 (sv) 1988-04-20
GB8809391D0 (en) 1993-05-26
IT8867332A0 (it) 1988-04-12
GB2265342B (en) 1994-05-18
DE3812588A1 (de) 1993-12-09
GB2265342A (en) 1993-09-29

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