FR2326676A1 - Procede et dispositif pour augmenter la portee utile des projectiles tires contre des objectifs ponctuels - Google Patents

Procede et dispositif pour augmenter la portee utile des projectiles tires contre des objectifs ponctuels

Info

Publication number
FR2326676A1
FR2326676A1 FR7628602A FR7628602A FR2326676A1 FR 2326676 A1 FR2326676 A1 FR 2326676A1 FR 7628602 A FR7628602 A FR 7628602A FR 7628602 A FR7628602 A FR 7628602A FR 2326676 A1 FR2326676 A1 FR 2326676A1
Authority
FR
France
Prior art keywords
projectile
trajectory
guides
pulse
target area
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.)
Granted
Application number
FR7628602A
Other languages
English (en)
Other versions
FR2326676B1 (fr
Inventor
H Molitz
V Fleck
J Biele
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.)
Institut Franco Allemand de Recherches de Saint Louis ISL
Original Assignee
Institut Franco Allemand de Recherches de Saint Louis ISL
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 Institut Franco Allemand de Recherches de Saint Louis ISL filed Critical Institut Franco Allemand de Recherches de Saint Louis ISL
Publication of FR2326676A1 publication Critical patent/FR2326676A1/fr
Application granted granted Critical
Publication of FR2326676B1 publication Critical patent/FR2326676B1/fr
Granted 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
    • F41G7/305—Details for spin-stabilized missiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/06—Aiming or laying means with rangefinder

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
FR7628602A 1975-09-30 1976-09-23 Procede et dispositif pour augmenter la portee utile des projectiles tires contre des objectifs ponctuels Granted FR2326676A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19752543606 DE2543606C2 (de) 1975-09-30 1975-09-30 Anordnung zur Flugbahnkorrektur eines rotierenden Geschosses

Publications (2)

Publication Number Publication Date
FR2326676A1 true FR2326676A1 (fr) 1977-04-29
FR2326676B1 FR2326676B1 (fr) 1982-04-09

Family

ID=5957845

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7628602A Granted FR2326676A1 (fr) 1975-09-30 1976-09-23 Procede et dispositif pour augmenter la portee utile des projectiles tires contre des objectifs ponctuels

Country Status (2)

Country Link
DE (1) DE2543606C2 (fr)
FR (1) FR2326676A1 (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1982002765A1 (fr) * 1979-02-21 1982-08-19 Geoffrey Martin Spence Systeme de guidage de projectile
EP0058258A1 (fr) * 1981-02-13 1982-08-25 Geoffrey Martin Spence Système de guidage pour projectile
WO1983003894A1 (fr) * 1982-04-21 1983-11-10 Hughes Aircraft Company Systeme de guidage de projectiles en fin de trajectoire
FR2722579A1 (fr) * 1994-07-16 1996-01-19 Rheinmetall Ind Gmbh Dispositif de correction de trajectoire de missiles

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2658167C2 (de) * 1976-10-30 1983-01-20 Eltro GmbH, Gesellschaft für Strahlungstechnik, 6900 Heidelberg Verfahren und Vorrichtung zur Korrektur der Flugbahn eines Geschosses
DE3827764A1 (de) * 1988-08-16 1990-02-22 Rheinmetall Gmbh Verfahren zur ermittlung von richtkorrekturwerten
DE3904684A1 (de) * 1989-02-16 1990-09-20 Asea Brown Boveri Verfahren zur korrektur der flugbahn aus einer rohrwaffe abgefeuerten oder selbststangetriebenen explosivgeschosses sowie geschoss, auf das das verfahren angewendet wird
DE3918701A1 (de) * 1989-06-08 1990-12-13 Diehl Gmbh & Co Verfahren zur verbesserung der treffgenauigkeit eines programmiert fliegenden flugkoerpers
DE4410326C2 (de) * 1994-03-25 1998-07-02 Rheinmetall Ind Ag Geschoß mit einer Vorrichtung zur Flugbahnkorrektur
DE4416211C2 (de) * 1994-05-07 1996-09-26 Rheinmetall Ind Gmbh Verfahren und Vorrichtung zur Flugbahnkorrektur von Geschossen
FR3035205B1 (fr) * 2015-04-20 2018-10-05 Roxel France Dispositif de correction de trajectoire d'un projectile et procede de correction de trajectoire

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB524876A (en) * 1938-02-15 1940-08-16 Sperry Gyrosocope Company Inc Improvements in or relating to explosive projectiles (such as bombs or aerial torpedoes), and electrical apparatus for controlling their movement during flight
US2414103A (en) * 1941-07-08 1947-01-14 Sperry Gyroscope Co Inc Apparatus for controlling missiles in flight
US2629289A (en) * 1945-05-03 1953-02-24 Sperry Corp Fire control apparatus for controlling the flight of missiles
US3028807A (en) * 1959-08-24 1962-04-10 Mcdonnell Aircraft Corp Guidance system
FR2167608A1 (fr) * 1972-01-03 1973-08-24 Ship Systems Inc
US3868883A (en) * 1964-02-20 1975-03-04 Mc Donnell Douglas Corp Guidance system

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3374967A (en) * 1949-12-06 1968-03-26 Navy Usa Course-changing gun-launched missile

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB524876A (en) * 1938-02-15 1940-08-16 Sperry Gyrosocope Company Inc Improvements in or relating to explosive projectiles (such as bombs or aerial torpedoes), and electrical apparatus for controlling their movement during flight
US2414103A (en) * 1941-07-08 1947-01-14 Sperry Gyroscope Co Inc Apparatus for controlling missiles in flight
US2629289A (en) * 1945-05-03 1953-02-24 Sperry Corp Fire control apparatus for controlling the flight of missiles
US3028807A (en) * 1959-08-24 1962-04-10 Mcdonnell Aircraft Corp Guidance system
US3868883A (en) * 1964-02-20 1975-03-04 Mc Donnell Douglas Corp Guidance system
FR2167608A1 (fr) * 1972-01-03 1973-08-24 Ship Systems Inc

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1982002765A1 (fr) * 1979-02-21 1982-08-19 Geoffrey Martin Spence Systeme de guidage de projectile
EP0058258A1 (fr) * 1981-02-13 1982-08-25 Geoffrey Martin Spence Système de guidage pour projectile
WO1983003894A1 (fr) * 1982-04-21 1983-11-10 Hughes Aircraft Company Systeme de guidage de projectiles en fin de trajectoire
FR2722579A1 (fr) * 1994-07-16 1996-01-19 Rheinmetall Ind Gmbh Dispositif de correction de trajectoire de missiles
US5647559A (en) * 1994-07-16 1997-07-15 Rheinmetall Industrie Gmbh Apparatus for flight path correction of flying bodies

Also Published As

Publication number Publication date
DE2543606A1 (de) 1977-04-07
FR2326676B1 (fr) 1982-04-09
DE2543606C2 (de) 1986-11-06

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Legal Events

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