DE4032982B3 - Lenksystem für mit einem photoempfindlichen Detektor versehene Flugkörper - Google Patents

Lenksystem für mit einem photoempfindlichen Detektor versehene Flugkörper Download PDF

Info

Publication number
DE4032982B3
DE4032982B3 DE4032982A DE4032982A DE4032982B3 DE 4032982 B3 DE4032982 B3 DE 4032982B3 DE 4032982 A DE4032982 A DE 4032982A DE 4032982 A DE4032982 A DE 4032982A DE 4032982 B3 DE4032982 B3 DE 4032982B3
Authority
DE
Germany
Prior art keywords
missile
matrix
photosensitive elements
photosensitive
target image
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
DE4032982A
Other languages
German (de)
English (en)
Inventor
Jacques Roze Des Ordons
Gilles Grenier
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of DE4032982B3 publication Critical patent/DE4032982B3/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
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • F41G7/308—Details for guiding a plurality of 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
    • F41G7/2213—Homing guidance systems maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
    • 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
    • F41G7/2206—Homing guidance systems using a remote control station
    • 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
    • F41G7/222—Homing guidance systems for spin-stabilized 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
    • F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • 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
    • 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
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • F41G7/305—Details for spin-stabilized missiles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
DE4032982A 1989-10-17 1990-10-17 Lenksystem für mit einem photoempfindlichen Detektor versehene Flugkörper Expired - Fee Related DE4032982B3 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8913559 1989-10-17
FR8913559 1989-10-17

Publications (1)

Publication Number Publication Date
DE4032982B3 true DE4032982B3 (de) 2010-05-20

Family

ID=41008793

Family Applications (1)

Application Number Title Priority Date Filing Date
DE4032982A Expired - Fee Related DE4032982B3 (de) 1989-10-17 1990-10-17 Lenksystem für mit einem photoempfindlichen Detektor versehene Flugkörper

Country Status (3)

Country Link
DE (1) DE4032982B3 (enExample)
GB (1) GB2459914B (enExample)
IT (1) IT9021755A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014115722A1 (de) * 2014-10-29 2016-05-04 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Integriertes Flugkörperantriebssystem

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10837745B2 (en) 2018-07-13 2020-11-17 Simmonds Precision Products, Inc. Short-exposure imaging-seeker for spin-stabilized projectiles

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3021428A (en) * 1947-08-23 1962-02-13 Bell Telephone Labor Inc Radiant-energy translation system
US3712562A (en) * 1964-05-19 1973-01-23 Us Navy Sector gating circuit
US3782667A (en) * 1972-07-25 1974-01-01 Us Army Beamrider missile guidance method
EP0028966A1 (fr) * 1979-11-09 1981-05-20 Thomson-Brandt Armements Procédé de pilotage et de guidage de projectiles en phase terminale de vol
US4286760A (en) * 1978-03-14 1981-09-01 Thomson-Csf Photoelectric direction finder
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
DE3300709C2 (de) * 1983-01-11 1985-12-19 Friedrich Dr. 8890 Aichach Schäff Rotierender Flugkörper zum Bekämpfen von Luftzielen
US4568040A (en) * 1981-12-09 1986-02-04 Thomson-Brandt Terminal guidance method and a guided missile operating according to this method
US4645139A (en) * 1981-06-04 1987-02-24 Societe Nationale Industrielle Aeropatiale Procedure for steering a low-speed missile, weapon system and missile for implementation of the procedure
US4710028A (en) * 1985-06-17 1987-12-01 Aerospatiale Societe Nationale Industrielle System for locating a body in motion
US4796834A (en) * 1980-09-15 1989-01-10 U.S. Philips Corporation Method for combatting of targets and projectile or missile for carrying out the method
US4860968A (en) * 1988-04-15 1989-08-29 The Boeing Company Communication link between moving bodies

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3021428A (en) * 1947-08-23 1962-02-13 Bell Telephone Labor Inc Radiant-energy translation system
US3712562A (en) * 1964-05-19 1973-01-23 Us Navy Sector gating circuit
US3782667A (en) * 1972-07-25 1974-01-01 Us Army Beamrider missile guidance method
US4286760A (en) * 1978-03-14 1981-09-01 Thomson-Csf Photoelectric direction finder
EP0028966A1 (fr) * 1979-11-09 1981-05-20 Thomson-Brandt Armements Procédé de pilotage et de guidage de projectiles en phase terminale de vol
US4796834A (en) * 1980-09-15 1989-01-10 U.S. Philips Corporation Method for combatting of targets and projectile or missile for carrying out the method
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
US4645139A (en) * 1981-06-04 1987-02-24 Societe Nationale Industrielle Aeropatiale Procedure for steering a low-speed missile, weapon system and missile for implementation of the procedure
US4568040A (en) * 1981-12-09 1986-02-04 Thomson-Brandt Terminal guidance method and a guided missile operating according to this method
EP0081421B1 (fr) * 1981-12-09 1989-01-25 Thomson-Brandt Armements Méthode de guidage terminal et missile guidé opérant selon cette méthode
DE3300709C2 (de) * 1983-01-11 1985-12-19 Friedrich Dr. 8890 Aichach Schäff Rotierender Flugkörper zum Bekämpfen von Luftzielen
US4710028A (en) * 1985-06-17 1987-12-01 Aerospatiale Societe Nationale Industrielle System for locating a body in motion
US4860968A (en) * 1988-04-15 1989-08-29 The Boeing Company Communication link between moving bodies

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014115722A1 (de) * 2014-10-29 2016-05-04 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Integriertes Flugkörperantriebssystem
EP3015697A1 (de) * 2014-10-29 2016-05-04 Bayern-Chemie Gesellschaft für flugchemische Antriebe mbH Integriertes flugkörperantriebssystem
DE102014115722B4 (de) 2014-10-29 2022-08-11 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Integriertes Flugkörperantriebssystem

Also Published As

Publication number Publication date
GB2459914B (en) 2010-05-19
IT9021755A1 (it) 1991-04-18
IT9021755A0 (enExample) 1990-10-16
GB2459914A (en) 2009-11-18
GB9022378D0 (en) 2009-08-12

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Legal Events

Date Code Title Description
8339 Ceased/non-payment of the annual fee