IT9021755A1 - Sistema di guida per missile dotato di un rivelatore fotosensibile. - Google Patents

Sistema di guida per missile dotato di un rivelatore fotosensibile.

Info

Publication number
IT9021755A1
IT9021755A1 IT021755A IT2175590A IT9021755A1 IT 9021755 A1 IT9021755 A1 IT 9021755A1 IT 021755 A IT021755 A IT 021755A IT 2175590 A IT2175590 A IT 2175590A IT 9021755 A1 IT9021755 A1 IT 9021755A1
Authority
IT
Italy
Prior art keywords
guide system
system equipped
photosensitive detector
missile guide
missile
Prior art date
Application number
IT021755A
Other languages
English (en)
Other versions
IT9021755A0 (it
Inventor
Gilles Grenier
Des Ordons Jacques Roze
Original Assignee
Aerospatiale Soc Nat Indus Trielle
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 Aerospatiale Soc Nat Indus Trielle filed Critical Aerospatiale Soc Nat Indus Trielle
Publication of IT9021755A0 publication Critical patent/IT9021755A0/it
Publication of IT9021755A1 publication Critical patent/IT9021755A1/it

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
    • F41G7/2206—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
    • F41G7/2213—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
    • F41G7/222—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
IT021755A 1989-10-17 1990-10-16 Sistema di guida per missile dotato di un rivelatore fotosensibile. IT9021755A1 (it)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
IT9021755A0 IT9021755A0 (it) 1990-10-16
IT9021755A1 true IT9021755A1 (it) 1991-04-18

Family

ID=41008793

Family Applications (1)

Application Number Title Priority Date Filing Date
IT021755A IT9021755A1 (it) 1989-10-17 1990-10-16 Sistema di guida per missile dotato di un rivelatore fotosensibile.

Country Status (3)

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

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

Family Cites Families (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
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
FR2517818A1 (fr) * 1981-12-09 1983-06-10 Thomson Brandt Methode de guidage terminal et missile guide operant selon cette methode
DE3300709C2 (de) * 1983-01-11 1985-12-19 Friedrich Dr. 8890 Aichach Schäff Rotierender Flugkörper zum Bekämpfen von Luftzielen
FR2583523B1 (fr) * 1985-06-17 1988-07-15 Aerospatiale Systeme pour la localisation d'un mobile.
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
GB2459914A (en) 2009-11-18
GB2459914B (en) 2010-05-19
IT9021755A0 (it) 1990-10-16
GB9022378D0 (en) 2009-08-12

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