DE69925368D1 - Methode und Vorrichtung zur Korrektur der Flugbahn eines rotationsstabilisierten Geschosses - Google Patents

Methode und Vorrichtung zur Korrektur der Flugbahn eines rotationsstabilisierten Geschosses

Info

Publication number
DE69925368D1
DE69925368D1 DE69925368T DE69925368T DE69925368D1 DE 69925368 D1 DE69925368 D1 DE 69925368D1 DE 69925368 T DE69925368 T DE 69925368T DE 69925368 T DE69925368 T DE 69925368T DE 69925368 D1 DE69925368 D1 DE 69925368D1
Authority
DE
Germany
Prior art keywords
trajectory
correcting
rotation
stabilized projectile
projectile
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 - Lifetime
Application number
DE69925368T
Other languages
English (en)
Other versions
DE69925368T2 (de
Inventor
Kjell Albrektsson
Torsten Wik
Ulf Hellman
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.)
BAE Systems Bofors AB
Original Assignee
Bofors Weapon Systems 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 Weapon Systems AB filed Critical Bofors Weapon Systems AB
Publication of DE69925368D1 publication Critical patent/DE69925368D1/de
Application granted granted Critical
Publication of DE69925368T2 publication Critical patent/DE69925368T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
    • F42B10/54—Spin braking means
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for missiles
    • G05D1/108—Simultaneous 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)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)
DE69925368T 1995-10-06 1999-09-23 Methode und Vorrichtung zur Korrektur der Flugbahn eines rotationsstabilisierten Geschosses Expired - Lifetime DE69925368T2 (de)

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
DE69925368D1 true DE69925368D1 (de) 2005-06-23
DE69925368T2 DE69925368T2 (de) 2006-01-19

Family

ID=29553828

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69925368T Expired - Lifetime DE69925368T2 (de) 1995-10-06 1999-09-23 Methode und Vorrichtung zur Korrektur der Flugbahn eines rotationsstabilisierten Geschosses

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)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002061363A2 (en) * 2001-02-01 2002-08-08 United Defense Lp 2-d projectile trajectory corrector
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

Also Published As

Publication number Publication date
ATE295956T1 (de) 2005-06-15
US6616093B1 (en) 2003-09-09
SE511986C2 (sv) 2000-01-10
SE9503469L (sv) 1999-10-07
DE69925368T2 (de) 2006-01-19
EP1087201A1 (de) 2001-03-28
ES2239438T3 (es) 2005-09-16
EP1087201B1 (de) 2005-05-18

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