DE3326499A1 - Verfahren zur passiven lenkung von flugkoerpern - Google Patents

Verfahren zur passiven lenkung von flugkoerpern

Info

Publication number
DE3326499A1
DE3326499A1 DE19833326499 DE3326499A DE3326499A1 DE 3326499 A1 DE3326499 A1 DE 3326499A1 DE 19833326499 DE19833326499 DE 19833326499 DE 3326499 A DE3326499 A DE 3326499A DE 3326499 A1 DE3326499 A1 DE 3326499A1
Authority
DE
Germany
Prior art keywords
missile
steering
target object
electromagnetic
passive
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
DE19833326499
Other languages
German (de)
English (en)
Other versions
DE3326499C2 (en, 2012
Inventor
Pierre 92100 Boulogne Billancourt Levy
André 95600 Eaubonne 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
Publication of DE3326499A1 publication Critical patent/DE3326499A1/de
Application granted granted Critical
Publication of DE3326499C2 publication Critical patent/DE3326499C2/de
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2273Homing guidance systems characterised by the type of waves
    • F41G7/2286Homing guidance systems characterised by the type of waves using radio waves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2253Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22Homing guidance systems
    • F41G7/2273Homing guidance systems characterised by the type of waves
    • F41G7/2293Homing 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)
DE19833326499 1982-07-28 1983-07-22 Verfahren zur passiven lenkung von flugkoerpern Granted DE3326499A1 (de)

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
DE3326499A1 true DE3326499A1 (de) 1984-02-02
DE3326499C2 DE3326499C2 (en, 2012) 1987-12-17

Family

ID=9276410

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19833326499 Granted DE3326499A1 (de) 1982-07-28 1983-07-22 Verfahren zur passiven lenkung von flugkoerpern

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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1912704B2 (de) * 1969-03-13 1977-04-14 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt Eigenlenkverfahren fuer flugkoerper

Family Cites Families (8)

* 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
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
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
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
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

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1912704B2 (de) * 1969-03-13 1977-04-14 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt Eigenlenkverfahren fuer flugkoerper

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
FR2531231A1 (fr) 1984-02-03
GB8319175D0 (en) 1983-08-17

Similar Documents

Publication Publication Date Title
EP0406877B1 (de) Verfahren zur Extraktion von Bewegungsfehlern eines ein kohärentes Abbildungsradarsystem mit führenden Trägers aus Radar-Rohdaten und Einrichtung zur Durchführung des Verfahrens
EP0406879B1 (de) Verfahren zur Extraktion von Bewegungsfehlern eines ein kohärentes Abbildungsradarsystem mitführenden Trägers aus Radar-Rohdaten und Einrichtung zur Durchführung des Verfahrens
DE2628379A1 (de) Seitensicht-radargeraet
DE3424775A1 (de) Abtaster fuer ein kanonengestartetes projektil
DE3326499A1 (de) Verfahren zur passiven lenkung von flugkoerpern
DE2836292C3 (de) Anordnung zur Winkelmessungsverbesserung bei einem Summen-Differenz-Folgeradar im Zweizielfall
DE3442598C2 (de) Leitsystem für Flugkörper
DE3326243C2 (en, 2012)
DE19627218B4 (de) Radarvorrichtung
DE2505697C1 (de) Stroerschutzverfahren fuer eine Antenne mit elektronischer Strahlschwenkung und Antenne zur Anwendung des Verfahrens
DE3529277C2 (en, 2012)
DE1766149A1 (de) Radarverfahren zur fruehzeitigen Mehrfachziel-Aufloesung
DE4002063C2 (de) Navigationssystem sowie Verfahren zur Bestimmung der relativen Lage zweier Objekte, insbesondere Projektleitsystem
DE3642767B3 (de) Winkelverfolgungsradarsystem
DE2215745A1 (de) Bahnverfolgungsantennengerät
DE3131494A1 (de) Ueberwachungseinrichtung fuer den landekurssender eines instrumentenlandesystems
DE4341295C2 (de) Vorrichtung und Verfahren zur elektronischen Strahlschwenkung mit mehreren bündelnden Antennen
DE1623399B1 (de) System zur automatischen zielverfolgung bei direkter sicht des zieles
DE2828648C2 (de) Bordgeschwindigkeitssensor für Luftfahrzeuge
DE10255634A1 (de) Radiointerferometrische Führungseinrichtung für die automatischen Steuerung unbemannter Fluggeräte insbesondere während der Endphase der Landung
DE2717997C2 (de) Monopulspeiler zur Azimut- und/oder Elevationsmessung
DE3537759C2 (en, 2012)
DE1110702B (de) Impulsradargeraet zur Verfolgung bewegter Ziele mit Schaltungsanordnung zur Unterdrueckung von Echos fester Gegenstaende
DE102018206670B3 (de) Synthetik-Apertur-Radarverfahren zur Fernerkundung der Erdoberfläche und Synthetik-Apertur-Radarvorrichtung
DE2734635A1 (de) Verfahren zum betreiben eines am flugzeugbord eingesetzten doppler-navigationsradarsystems

Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee