GB8809391D0 - 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
GB8809391D0
GB8809391D0 GB888809391A GB8809391A GB8809391D0 GB 8809391 D0 GB8809391 D0 GB 8809391D0 GB 888809391 A GB888809391 A GB 888809391A GB 8809391 A GB8809391 A GB 8809391A GB 8809391 D0 GB8809391 D0 GB 8809391D0
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.)
Granted
Application number
GB888809391A
Other versions
GB2265342B (en
GB2265342A (en
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 (en) 1987-04-22 1987-04-22 METHOD AND DEVICE FOR DRIVING A PROJECTILE ACCORDING TO ITS THREE AXES OF ROLL TANGAGE AND LACE.

Publications (3)

Publication Number Publication Date
GB8809391D0 true GB8809391D0 (en) 1993-05-26
GB2265342A GB2265342A (en) 1993-09-29
GB2265342B 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 (en)
FR (1) FR2686687B1 (en)
GB (1) GB2265342B (en)
IT (1) IT1237006B (en)
SE (1) SE8801461D0 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE501082C2 (en) * 1993-03-30 1994-11-07 Bofors Ab Method and apparatus for giving an airborne combat section a desired pattern of movement
GB9618126D0 (en) * 1996-08-29 1997-01-08 British Aerospace Thruster pack for missile control
DE102005052474B3 (en) 2005-11-03 2007-07-12 Junghans Feinwerktechnik Gmbh & Co. Kg Spiked artillery projectile
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 (en) * 2011-05-19 2017-09-01 Snecma Propulsion Solide SYSTEM FOR FORCE DRIVING AND ATTITUDE CONTROL IN FLIGHT OF A VEHICLE AND A VEHICLE COMPRISING SUCH A SYSTEM
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
US9551552B2 (en) 2012-03-02 2017-01-24 Orbital Atk, Inc. Methods and apparatuses for aerial interception 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 (en) * 1970-11-10 1972-05-18 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Device for generating control torques in rocket-propelled missiles
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 (en) * 1981-06-30 1985-06-07 Thomson Brandt GAS JET STEERING DEVICE FOR A GUIDED MACHINE
FR2536720A1 (en) * 1982-11-29 1984-06-01 Aerospatiale SYSTEM FOR CONTROLLING A MISSILE USING LATERAL GAS JETS AND MISSILE HAVING SUCH A SYSTEM
DE3378783D1 (en) * 1983-01-20 1989-02-02 Ford Aerospace & Communication Ram air combustion steering system for a guided missile
DE3429798C1 (en) * 1984-08-13 1985-12-12 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Device for correcting the trajectory of a projectile
DE3531686A1 (en) * 1985-09-05 1987-03-12 Rheinmetall Gmbh CONTROL BLOCK
GB8611406D0 (en) * 1986-05-09 1986-08-20 Lucas Ind Plc Missile flight control system

Also Published As

Publication number Publication date
SE8801461D0 (en) 1988-04-20
FR2686687A1 (en) 1993-07-30
IT8867332A0 (en) 1988-04-12
IT1237006B (en) 1993-05-13
GB2265342B (en) 1994-05-18
GB2265342A (en) 1993-09-29
DE3812588A1 (en) 1993-12-09
FR2686687B1 (en) 1994-05-13

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Legal Events

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

Effective date: 19940818