DE60023007D1 - Geschosslenkung mittels einer ringanordnung und optisch ausgelösten ablenkvorrichtungen - Google Patents

Geschosslenkung mittels einer ringanordnung und optisch ausgelösten ablenkvorrichtungen

Info

Publication number
DE60023007D1
DE60023007D1 DE60023007T DE60023007T DE60023007D1 DE 60023007 D1 DE60023007 D1 DE 60023007D1 DE 60023007 T DE60023007 T DE 60023007T DE 60023007 T DE60023007 T DE 60023007T DE 60023007 D1 DE60023007 D1 DE 60023007D1
Authority
DE
Germany
Prior art keywords
ring arrangement
deflection devices
shuttle
steering
optically
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
DE60023007T
Other languages
English (en)
Other versions
DE60023007T2 (de
Inventor
G Horwath
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.)
General Dynamics Ordnance and Tactical Systems Inc
Original Assignee
General Dynamics Ordnance and Tactical Systems Inc
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 General Dynamics Ordnance and Tactical Systems Inc filed Critical General Dynamics Ordnance and Tactical Systems Inc
Publication of DE60023007D1 publication Critical patent/DE60023007D1/de
Application granted granted Critical
Publication of DE60023007T2 publication Critical patent/DE60023007T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/226—Semi-active homing systems, i.e. comprising a receiver and involving auxiliary illuminating means, e.g. using auxiliary guiding missiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • 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
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Fluid Mechanics (AREA)
  • Electromagnetism (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
DE60023007T 1999-07-21 2000-07-20 Geschosslenkung mittels einer ringanordnung und optisch ausgelösten ablenkvorrichtungen Expired - Fee Related DE60023007T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US14491899P 1999-07-21 1999-07-21
US144918P 1999-07-21
PCT/US2000/019925 WO2001016547A2 (en) 1999-07-21 2000-07-20 Ring array projectile steering with optically-triggered diverter elements

Publications (2)

Publication Number Publication Date
DE60023007D1 true DE60023007D1 (de) 2006-02-16
DE60023007T2 DE60023007T2 (de) 2006-07-13

Family

ID=22510742

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60023007T Expired - Fee Related DE60023007T2 (de) 1999-07-21 2000-07-20 Geschosslenkung mittels einer ringanordnung und optisch ausgelösten ablenkvorrichtungen

Country Status (4)

Country Link
EP (1) EP1196733B1 (de)
AU (1) AU2245801A (de)
DE (1) DE60023007T2 (de)
WO (1) WO2001016547A2 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10147837A1 (de) 2001-09-27 2003-04-24 Rheinmetall Landsysteme Gmbh Wurfsystem für einen Gefechtskopf mit einer Richtvorrichtung zur Neutralisierung von Minen
DE102004029343B4 (de) * 2004-06-17 2009-04-30 Diehl Bgt Defence Gmbh & Co. Kg Zielführungsvorrichtung für ein Fluggerät
DE102007002336A1 (de) * 2007-01-16 2008-07-17 Lfk-Lenkflugkörpersysteme Gmbh Suchkopf für einen Lenkflugkörper zur Erfassung und Verfolgung eines Zieles und Verfahren zu dessen Anwendung
DE102009016147A1 (de) 2009-04-03 2010-10-07 Rheinmetall Soldier Electronics Gmbh Zerlegendes Geschoss
US8164037B2 (en) * 2009-09-26 2012-04-24 Raytheon Company Co-boresighted dual-mode SAL/IR seeker including a SAL spreader

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3000307A (en) * 1953-08-04 1961-09-19 Jr Herbert Trotter Device for correcting the course of a missile
US4006356A (en) * 1961-10-27 1977-02-01 Aeronutronic Ford Corporation Radiant energy tracking device
GB1605228A (en) * 1970-10-01 1985-03-20 British Aerospace Missiles
US4231533A (en) * 1975-07-09 1980-11-04 The United States Of America As Represented By The Secretary Of The Air Force Static self-contained laser seeker system for active missile guidance
US5102065A (en) 1988-02-17 1992-04-07 Thomson - Csf System to correct the trajectory of a projectile
US5127604A (en) * 1989-08-18 1992-07-07 Raytheon Company Optical system
DE4007712A1 (de) * 1990-03-10 1991-09-12 Tzn Forschung & Entwicklung Geschoss mit einem bugseitig angeordneten ir-suchsystem
US5529262A (en) 1993-06-23 1996-06-25 Horwath; Tibor G. Guidance seeker for small spinning projectiles
US5456429A (en) * 1993-08-02 1995-10-10 Loral Corp. Thrust maneuver system
DE4408085C2 (de) * 1994-03-10 1999-08-12 Rheinmetall W & M Gmbh Vorrichtung zur Lenkung eines nicht um seine Längsachse rotierenden Flugkörpers
DE4410326C2 (de) * 1994-03-25 1998-07-02 Rheinmetall Ind Ag Geschoß mit einer Vorrichtung zur Flugbahnkorrektur
DE4443134C2 (de) * 1994-12-03 2001-07-05 Diehl Stiftung & Co Sensoreinrichtung für einen Flugkörper
IL116438A (en) 1995-12-18 2000-01-31 Israel State Laser sensor
US5695152A (en) * 1996-09-18 1997-12-09 Israel Aircraft Industries Ltd. System for correcting flight trajectory of a projectile
US6076765A (en) 1997-01-02 2000-06-20 Primex Technologies, Inc. Reticle for use in a guidance seeker for a spinning projectile

Also Published As

Publication number Publication date
WO2001016547A2 (en) 2001-03-08
EP1196733A2 (de) 2002-04-17
AU2245801A (en) 2001-03-26
WO2001016547A3 (en) 2001-06-21
EP1196733A4 (de) 2003-07-02
EP1196733B1 (de) 2005-10-05
DE60023007T2 (de) 2006-07-13

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee