GB2459914B - Guidance system for a missile provided with a photosensitive detector - Google Patents

Guidance system for a missile provided with a photosensitive detector

Info

Publication number
GB2459914B
GB2459914B GB9022378A GB9022378A GB2459914B GB 2459914 B GB2459914 B GB 2459914B GB 9022378 A GB9022378 A GB 9022378A GB 9022378 A GB9022378 A GB 9022378A GB 2459914 B GB2459914 B GB 2459914B
Authority
GB
United Kingdom
Prior art keywords
guidance system
photosensitive detector
missile provided
missile
photosensitive
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
GB9022378A
Other languages
English (en)
Other versions
GB2459914A (en
GB9022378D0 (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
Publication of GB9022378D0 publication Critical patent/GB9022378D0/en
Publication of GB2459914A publication Critical patent/GB2459914A/en
Application granted granted Critical
Publication of GB2459914B publication Critical patent/GB2459914B/en
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)
GB9022378A 1989-10-17 1990-10-16 Guidance system for a missile provided with a photosensitive detector Expired - Fee Related GB2459914B (en)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
GB9022378D0 GB9022378D0 (en) 2009-08-12
GB2459914A GB2459914A (en) 2009-11-18
GB2459914B true GB2459914B (en) 2010-05-19

Family

ID=41008793

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9022378A Expired - Fee Related GB2459914B (en) 1989-10-17 1990-10-16 Guidance system for a missile provided with a photosensitive detector

Country Status (3)

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

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014115722B4 (de) * 2014-10-29 2022-08-11 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Integriertes Flugkörperantriebssystem
US10837745B2 (en) 2018-07-13 2020-11-17 Simmonds Precision Products, Inc. Short-exposure imaging-seeker for spin-stabilized projectiles

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0081421A1 (fr) * 1981-12-09 1983-06-15 Thomson-Brandt Armements Méthode de guidage terminal et missile guidé opérant selon cette méthode
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

Family Cites Families (9)

* 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
FR2420144A1 (fr) * 1978-03-14 1979-10-12 Thomson Csf Systeme de detection optoelectrique et de localisation angulaire d'un objet lumineux
FR2469345A1 (fr) * 1979-11-09 1981-05-22 Thomson Brandt Procede de pilotage et de guidage de projectiles en phase terminale et projectiles comportant les moyens de mise en oeuvre de ce procede
SE423451B (sv) * 1980-09-15 1982-05-03 Philips Svenska Ab Sett for samarbete mellan projektiler och malfoljande projektil for genomforande av settet vid bekempning av mal
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
FR2578665B1 (fr) * 1981-06-04 1988-02-12 Aerospatiale Procede de pilotage d'un missile a faible vitesse, systeme d'arme et missile pour la mise en oeuvre du procede
DE3300709C2 (de) * 1983-01-11 1985-12-19 Friedrich Dr. 8890 Aichach Schäff Rotierender Flugkörper zum Bekämpfen von Luftzielen

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0081421A1 (fr) * 1981-12-09 1983-06-15 Thomson-Brandt Armements Méthode de guidage terminal et missile guidé opérant selon cette méthode
US4568040A (en) * 1981-12-09 1986-02-04 Thomson-Brandt Terminal guidance method and a guided missile operating according to this method
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

Also Published As

Publication number Publication date
DE4032982B3 (de) 2010-05-20
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
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20100819