SE511986C2 - Sätt att korrigera projektilbanan för rotationsstabiliserande projektiler - Google Patents

Sätt att korrigera projektilbanan för rotationsstabiliserande projektiler

Info

Publication number
SE511986C2
SE511986C2 SE9503469A SE9503469A SE511986C2 SE 511986 C2 SE511986 C2 SE 511986C2 SE 9503469 A SE9503469 A SE 9503469A SE 9503469 A SE9503469 A SE 9503469A SE 511986 C2 SE511986 C2 SE 511986C2
Authority
SE
Sweden
Prior art keywords
projectile
rotation
point
grenade
trajectory
Prior art date
Application number
SE9503469A
Other languages
English (en)
Swedish (sv)
Other versions
SE9503469L (sv
Inventor
Kjell Albrektsson
Torsten Wik
Ulf Hellman
Original Assignee
Bofors Ab
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 Bofors Ab filed Critical Bofors Ab
Priority to SE9503469A priority Critical patent/SE511986C2/sv
Priority to ES99850139T priority patent/ES2239438T3/es
Priority to DE69925368T priority patent/DE69925368T2/de
Priority to EP99850139A priority patent/EP1087201B1/de
Priority to AT99850139T priority patent/ATE295956T1/de
Priority to US09/406,778 priority patent/US6616093B1/en
Publication of SE9503469L publication Critical patent/SE9503469L/
Publication of SE511986C2 publication Critical patent/SE511986C2/sv

Links

Classifications

    • 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
    • F42B10/32Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/54Spin braking means
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/107Simultaneous control of position or course in three dimensions specially adapted for missiles
    • G05D1/108Simultaneous control of position or course in three dimensions specially adapted for missiles animated with a rolling movement

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
SE9503469A 1995-10-06 1995-10-06 Sätt att korrigera projektilbanan för rotationsstabiliserande projektiler SE511986C2 (sv)

Priority Applications (6)

Application Number Priority Date Filing Date Title
SE9503469A SE511986C2 (sv) 1995-10-06 1995-10-06 Sätt att korrigera projektilbanan för rotationsstabiliserande projektiler
ES99850139T ES2239438T3 (es) 1995-10-06 1999-09-23 Metodo y dispositivo para corregir la trayectoria de un proyectil estabilizado por giro.
DE69925368T DE69925368T2 (de) 1995-10-06 1999-09-23 Methode und Vorrichtung zur Korrektur der Flugbahn eines rotationsstabilisierten Geschosses
EP99850139A EP1087201B1 (de) 1995-10-06 1999-09-23 Methode und Vorrichtung zur Korrektur der Flugbahn eines rotationsstabilisierten Geschosses
AT99850139T ATE295956T1 (de) 1995-10-06 1999-09-23 Methode und vorrichtung zur korrektur der flugbahn eines rotationsstabilisierten geschosses
US09/406,778 US6616093B1 (en) 1995-10-06 1999-09-28 Method and device for correcting the trajectory of a spin-stabilised projectile

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
SE9503469A SE511986C2 (sv) 1995-10-06 1995-10-06 Sätt att korrigera projektilbanan för rotationsstabiliserande projektiler
EP99850139A EP1087201B1 (de) 1995-10-06 1999-09-23 Methode und Vorrichtung zur Korrektur der Flugbahn eines rotationsstabilisierten Geschosses
US09/406,778 US6616093B1 (en) 1995-10-06 1999-09-28 Method and device for correcting the trajectory of a spin-stabilised projectile

Publications (2)

Publication Number Publication Date
SE9503469L SE9503469L (sv) 1999-10-07
SE511986C2 true SE511986C2 (sv) 2000-01-10

Family

ID=29553828

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9503469A SE511986C2 (sv) 1995-10-06 1995-10-06 Sätt att korrigera projektilbanan för rotationsstabiliserande projektiler

Country Status (6)

Country Link
US (1) US6616093B1 (de)
EP (1) EP1087201B1 (de)
AT (1) ATE295956T1 (de)
DE (1) DE69925368T2 (de)
ES (1) ES2239438T3 (de)
SE (1) SE511986C2 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1366339A2 (de) * 2001-02-01 2003-12-03 United Defense, L.P. Zweidimensionale geschossflugbahnkorrekturvorrichtung

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10143312C1 (de) * 2001-09-04 2003-06-18 Diehl Munitionssysteme Gmbh Bremseinrichtung für ein bahnkorrigierbares drallstabilisiertes Artillerieprojektil
US7163176B1 (en) * 2004-01-15 2007-01-16 Raytheon Company 2-D projectile trajectory correction system and method
US7611095B1 (en) * 2006-04-28 2009-11-03 The Boeing Company Aerodynamic re-entry vehicle control with active and passive yaw flaps
US7963442B2 (en) * 2006-12-14 2011-06-21 Simmonds Precision Products, Inc. Spin stabilized projectile trajectory control
WO2011127338A2 (en) * 2010-04-08 2011-10-13 Bae Systems Information And Electronic Systems Integration Inc. Predictive roll capture

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5439188A (en) * 1964-09-04 1995-08-08 Hughes Missile Systems Company Control system
US4037806A (en) * 1964-09-16 1977-07-26 General Dynamics Corporation Control system for rolling missile with target seeker head
SE445952B (sv) 1983-03-25 1986-07-28 Bofors Ab Anordning for att minska projektilspridning
DE3524925A1 (de) * 1985-07-12 1987-01-22 Diehl Gmbh & Co Verfahren zum ansteuern eines zieles
DE3737997A1 (de) * 1986-04-29 1996-05-30 Royal Ordnance Plc Drallgedämpftes Übungsgeschoß mit wählbarer Sicherheitsflugweite
SE461750B (sv) * 1987-03-20 1990-03-19 Lars Johan Schleimann Jensen Foerfarande foer styrning av ett flygande objekt, saasom en projektil, mot ett maal och projektil foer foerfarandets genomfoerande
US5131602A (en) 1990-06-13 1992-07-21 Linick James M Apparatus and method for remote guidance of cannon-launched projectiles
US5425514A (en) * 1993-12-29 1995-06-20 Raytheon Company Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same
US5647558A (en) 1995-02-14 1997-07-15 Bofors Ab Method and apparatus for radial thrust trajectory correction of a ballistic projectile
US5775636A (en) * 1996-09-30 1998-07-07 The United States Of America As Represented By The Secretary Of The Army Guided artillery projectile and method
FR2761769B1 (fr) * 1997-04-08 1999-07-02 Tda Armements Sas Dispositif de microgouverne pour la correction de trajectoire de munition stabilisee par rotation
DE19740888C2 (de) * 1997-09-17 1999-09-02 Rheinmetall W & M Gmbh Verfahren zum autonomen Lenken eines drallstabilisierten Artilleriegeschosses und autonom gelenktes Artilleriegeschoß zur Durchführung des Verfahrens

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1366339A2 (de) * 2001-02-01 2003-12-03 United Defense, L.P. Zweidimensionale geschossflugbahnkorrekturvorrichtung
EP1366339A4 (de) * 2001-02-01 2006-07-19 United Defense Lp Zweidimensionale geschossflugbahnkorrekturvorrichtung

Also Published As

Publication number Publication date
DE69925368T2 (de) 2006-01-19
US6616093B1 (en) 2003-09-09
ATE295956T1 (de) 2005-06-15
ES2239438T3 (es) 2005-09-16
DE69925368D1 (de) 2005-06-23
SE9503469L (sv) 1999-10-07
EP1087201A1 (de) 2001-03-28
EP1087201B1 (de) 2005-05-18

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NUG Patent has lapsed