GB2265342B - Method and device for controlling a projectile about its three axes of roll,pitch and yaw - Google Patents

Method and device for controlling a projectile about its three axes of roll,pitch and yaw

Info

Publication number
GB2265342B
GB2265342B GB8809391A GB8809391A GB2265342B GB 2265342 B GB2265342 B GB 2265342B GB 8809391 A GB8809391 A GB 8809391A GB 8809391 A GB8809391 A GB 8809391A GB 2265342 B GB2265342 B GB 2265342B
Authority
GB
United Kingdom
Prior art keywords
projectile
yaw
pitch
axes
roll
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
GB8809391A
Other languages
English (en)
Other versions
GB8809391D0 (en
GB2265342A (en
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
Publication of GB8809391D0 publication Critical patent/GB8809391D0/en
Publication of GB2265342A publication Critical patent/GB2265342A/en
Application granted granted Critical
Publication of GB2265342B publication Critical patent/GB2265342B/en
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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GB8809391A 1987-04-22 1988-04-21 Method and device for controlling a projectile about its three axes of roll,pitch and yaw Expired - Fee Related GB2265342B (en)

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 (3)

Publication Number Publication Date
GB8809391D0 GB8809391D0 (en) 1993-05-26
GB2265342A GB2265342A (en) 1993-09-29
GB2265342B true GB2265342B (en) 1994-05-18

Family

ID=9350375

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8809391A Expired - Fee Related GB2265342B (en) 1987-04-22 1988-04-21 Method and device for controlling a projectile about its three axes of roll,pitch and yaw

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
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

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1359864A (en) * 1970-11-10 1974-07-10 Messerschmitt Boelkow Blohm Missile
EP0068972A1 (fr) * 1981-06-30 1983-01-05 Thomson-Brandt Armements Dispositif de pilotage par jets de gaz pour engin guidé
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
WO1984002975A1 (fr) * 1983-01-20 1984-08-02 Ford Aerospace & Communication Systeme de guidage par combustion d'air sous pression dynamique
GB2163240A (en) * 1984-08-13 1986-02-19 Messerschmitt Boelkow Blohm Apparatus for the in-flight alteration of the trajectory of a projectile or missile
EP0244971A2 (fr) * 1986-05-09 1987-11-11 LUCAS INDUSTRIES public limited company Dispositif de pilotage pour missile

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE3531686A1 (de) * 1985-09-05 1987-03-12 Rheinmetall Gmbh Steuerblock

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1359864A (en) * 1970-11-10 1974-07-10 Messerschmitt Boelkow Blohm Missile
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
EP0068972A1 (fr) * 1981-06-30 1983-01-05 Thomson-Brandt Armements Dispositif de pilotage par jets de gaz pour engin guidé
WO1984002975A1 (fr) * 1983-01-20 1984-08-02 Ford Aerospace & Communication Systeme de guidage par combustion d'air sous pression dynamique
GB2163240A (en) * 1984-08-13 1986-02-19 Messerschmitt Boelkow Blohm Apparatus for the in-flight alteration of the trajectory of a projectile or missile
EP0244971A2 (fr) * 1986-05-09 1987-11-11 LUCAS INDUSTRIES public limited company Dispositif de pilotage pour missile

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
IT1237006B (it) 1993-05-13
DE3812588A1 (de) 1993-12-09
GB2265342A (en) 1993-09-29

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940818