FR2531231A1 - Procede de guidage passif pour engin - Google Patents

Procede de guidage passif pour engin Download PDF

Info

Publication number
FR2531231A1
FR2531231A1 FR8213188A FR8213188A FR2531231A1 FR 2531231 A1 FR2531231 A1 FR 2531231A1 FR 8213188 A FR8213188 A FR 8213188A FR 8213188 A FR8213188 A FR 8213188A FR 2531231 A1 FR2531231 A1 FR 2531231A1
Authority
FR
France
Prior art keywords
machine
target
guidance
guided
electromagnetic
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
FR8213188A
Other languages
English (en)
French (fr)
Other versions
FR2531231B1 (en, 2012
Inventor
Pierre Levy
Andre Robert
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.)
Societe Anonyme de Telecommunications SAT
Original Assignee
Societe Anonyme de Telecommunications SAT
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 Societe Anonyme de Telecommunications SAT filed Critical Societe Anonyme de Telecommunications SAT
Priority to FR8213188A priority Critical patent/FR2531231A1/fr
Priority to GB08319175A priority patent/GB2126322B/en
Priority to US06/516,120 priority patent/US4540140A/en
Priority to DE19833326499 priority patent/DE3326499A1/de
Publication of FR2531231A1 publication Critical patent/FR2531231A1/fr
Application granted granted Critical
Publication of FR2531231B1 publication Critical patent/FR2531231B1/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
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2286—Homing guidance systems characterised by the type of waves using 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
    • F41G7/22—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

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)
  • Radar Systems Or Details Thereof (AREA)
FR8213188A 1982-07-28 1982-07-28 Procede de guidage passif pour engin Granted FR2531231A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR8213188A FR2531231A1 (fr) 1982-07-28 1982-07-28 Procede de guidage passif pour engin
GB08319175A GB2126322B (en) 1982-07-28 1983-07-15 Passive missile guidance process
US06/516,120 US4540140A (en) 1982-07-28 1983-07-20 Passive missile guidance process
DE19833326499 DE3326499A1 (de) 1982-07-28 1983-07-22 Verfahren zur passiven lenkung von flugkoerpern

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8213188A FR2531231A1 (fr) 1982-07-28 1982-07-28 Procede de guidage passif pour engin

Publications (2)

Publication Number Publication Date
FR2531231A1 true FR2531231A1 (fr) 1984-02-03
FR2531231B1 FR2531231B1 (en, 2012) 1984-12-21

Family

ID=9276410

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8213188A Granted FR2531231A1 (fr) 1982-07-28 1982-07-28 Procede de guidage passif pour engin

Country Status (4)

Country Link
US (1) US4540140A (en, 2012)
DE (1) DE3326499A1 (en, 2012)
FR (1) FR2531231A1 (en, 2012)
GB (1) GB2126322B (en, 2012)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2603695B1 (fr) * 1986-09-09 1990-10-19 Thomson Csf Procede et dispositif de visualisation des cibles et/ou des positions des cibles utilisant des moyens d'acquisition des donnees d'un systeme d'armes
GB9310865D0 (en) * 1992-06-29 1995-11-22 Deutsche Aerospace Method for the independent control of a guidable flying body provided with a warhead and arrangement for the performance of the method
DE4309295A1 (de) * 1992-06-29 1995-10-05 Daimler Benz Aerospace Ag Verfahren zur eigenständigen Steuerung eines lenkbaren und mit einem Gefechtskopf versehenen Flugkörpers und Anordnung zur Durchführung des Verfahrens
RU2124688C1 (ru) * 1997-11-25 1999-01-10 Конструкторское бюро приборостроения Способ комбинированного управления летательным аппаратом
RU2138768C1 (ru) * 1998-08-03 1999-09-27 Конструкторское бюро приборостроения Система наведения управляемого снаряда
RU2187781C2 (ru) * 2000-07-03 2002-08-20 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Система наведения управляемого снаряда
RU2205361C2 (ru) * 2001-04-05 2003-05-27 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Система наведения управляемого снаряда
RU2254543C1 (ru) * 2004-06-21 2005-06-20 Закрытое акционерное общество Научно-технический комплекс "Автоматизация и механизация технологий" Способ наведения баллистической ракеты с отделяемым корректируемым боевым модулем
US10168420B1 (en) * 2014-07-15 2019-01-01 Herbert U. Fluhler Nonlinear interferometric imaging sensor
RU2586399C2 (ru) * 2014-11-05 2016-06-10 Федеральное государственное казенное военное образовательное учреждение высшего профессионального образования "Военная академия войсковой противовоздушной обороны Вооруженных Сил Российской Федерации имени Маршала Советского Союза А.М. Василевского" Министерства Обороны Российской Федерации Способ комбинированного наведения летательного аппарата
US10353064B2 (en) * 2016-05-26 2019-07-16 Decisive Analytics Corporation Method and apparatus for detecting airborne objects

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1201402A (fr) * 1951-02-22 1959-12-30 Dispositif correcteur de trajectoire pour projectiles et engins automatiquement dirigés vers un but
DE1912704A1 (de) * 1969-03-13 1970-10-01 Licentia Gmbh Eigenlenkverfahren eines Flugkoerpers
US4198015A (en) * 1978-05-30 1980-04-15 The United States Of America As Represented By The Secretary Of The Army Ideal trajectory shaping for anti-armor missiles via time optimal controller autopilot
US4277038A (en) * 1979-04-27 1981-07-07 The United States Of America As Represented By The Secretary Of The Army Trajectory shaping of anti-armor missiles via tri-mode guidance

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3181813A (en) * 1956-08-10 1965-05-04 Jr Joseph F Gulick Inter-ferometer homing system
US3740002A (en) * 1966-11-23 1973-06-19 Us Army Interferometer type homing head for guided missiles
US4264907A (en) * 1968-04-17 1981-04-28 General Dynamics Corporation, Pomona Division Rolling dual mode missile
US4108400A (en) * 1976-08-02 1978-08-22 The United States Of America As Represented By The Secretary Of The Navy Dual mode guidance system
US4204655A (en) * 1978-11-29 1980-05-27 The United States Of America As Represented By The Secretary Of The Navy Broadband interferometer and direction finding missile guidance system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1201402A (fr) * 1951-02-22 1959-12-30 Dispositif correcteur de trajectoire pour projectiles et engins automatiquement dirigés vers un but
DE1912704A1 (de) * 1969-03-13 1970-10-01 Licentia Gmbh Eigenlenkverfahren eines Flugkoerpers
US4198015A (en) * 1978-05-30 1980-04-15 The United States Of America As Represented By The Secretary Of The Army Ideal trajectory shaping for anti-armor missiles via time optimal controller autopilot
US4277038A (en) * 1979-04-27 1981-07-07 The United States Of America As Represented By The Secretary Of The Army Trajectory shaping of anti-armor missiles via tri-mode guidance

Also Published As

Publication number Publication date
GB2126322A (en) 1984-03-21
DE3326499C2 (en, 2012) 1987-12-17
FR2531231B1 (en, 2012) 1984-12-21
GB2126322B (en) 1986-02-19
US4540140A (en) 1985-09-10
DE3326499A1 (de) 1984-02-02
GB8319175D0 (en) 1983-08-17

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TP Transmission of property
ST Notification of lapse