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DE59913732D1 - Flugkörper - Google Patents

Flugkörper

Info

Publication number
DE59913732D1
DE59913732D1 DE59913732T DE59913732T DE59913732D1 DE 59913732 D1 DE59913732 D1 DE 59913732D1 DE 59913732 T DE59913732 T DE 59913732T DE 59913732 T DE59913732 T DE 59913732T DE 59913732 D1 DE59913732 D1 DE 59913732D1
Authority
DE
Germany
Prior art keywords
missile
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 - Lifetime
Application number
DE59913732T
Other languages
English (en)
Inventor
Uwe Dr Krogmann
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.)
Diehl Defence GmbH and Co KG
Original Assignee
Diehl BGT Defence GmbH and Co KG
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 Diehl BGT Defence GmbH and Co KG filed Critical Diehl BGT Defence GmbH and Co KG
Priority to DE59913732T priority Critical patent/DE59913732D1/de
Application granted granted Critical
Publication of DE59913732D1 publication Critical patent/DE59913732D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/055Umbilical connecting means
    • 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
    • F41G7/2246Active homing systems, i.e. comprising both a transmitter and a receiver
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01Arrangements thereon for guidance or control
    • F42B15/04Arrangements thereon for guidance or control using wire, e.g. for guiding ground-to-ground rockets

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Feedback Control In General (AREA)
DE59913732T 1998-12-15 1999-12-13 Flugkörper Expired - Lifetime DE59913732D1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE59913732T DE59913732D1 (de) 1998-12-15 1999-12-13 Flugkörper

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE1998157894 DE19857894A1 (de) 1998-12-15 1998-12-15 Flugkörper
DE59913732T DE59913732D1 (de) 1998-12-15 1999-12-13 Flugkörper

Publications (1)

Publication Number Publication Date
DE59913732D1 true DE59913732D1 (de) 2006-09-14

Family

ID=7891186

Family Applications (2)

Application Number Title Priority Date Filing Date
DE1998157894 Withdrawn DE19857894A1 (de) 1998-12-15 1998-12-15 Flugkörper
DE59913732T Expired - Lifetime DE59913732D1 (de) 1998-12-15 1999-12-13 Flugkörper

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE1998157894 Withdrawn DE19857894A1 (de) 1998-12-15 1998-12-15 Flugkörper

Country Status (2)

Country Link
EP (1) EP1020699B1 (de)
DE (2) DE19857894A1 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9827358D0 (en) * 1998-12-12 2000-01-19 British Aerospace Combat aid system
DE10132184B4 (de) * 2001-07-03 2004-07-08 Peter Zahner Vorrichtungen und Verfahren für den autarken und damit sichereren Abgang von lenkbaren Außenlasten von Trägerflugzeugen
DE10158666A1 (de) * 2001-11-28 2003-06-18 Lfk Gmbh Vorrichtung und Verfahren zur autarken Zielführung eines Flugkörpers mit Hilfe außerhalb des Zielpunktes liegender Orientierungsmerkmale
RU2218550C2 (ru) * 2002-01-09 2003-12-10 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Способ определения аэродинамических характеристик управляемого снаряда в полете, способ определения угла атаки управляемого снаряда в полете, способ стабилизации углового положения управляемого снаряда и устройства для их осуществления
DE102004042990B4 (de) * 2004-09-06 2008-11-20 Michael Grabmeier Verfahren und Vorrichtung zum Test eines operationellen Marschflugkörpers in verschiedenen Prüfzenarien mittels Betriebsart Wartung
DE102007022672C5 (de) * 2007-05-15 2010-09-09 Lfk-Lenkflugkörpersysteme Gmbh Verfahren zur Zustandsüberwachung einer intelligenten Waffe und intelligente Waffe
DE102008041571B4 (de) 2008-08-26 2019-12-05 Robert Bosch Gmbh Verfahren und Vorrichtung zur Fehlerbehandlung beim Betrieb eines Verbrennungsmotors
US20150205271A1 (en) * 2012-07-17 2015-07-23 Siemens Aktiengesellschaft Automated reconfiguration of a discrete event control loop
DE102014213171A1 (de) * 2014-04-09 2015-10-15 Continental Automotive Gmbh System zur autonomen Fahrzeugführung und Kraftfahrzeug
DE102017210151A1 (de) * 2017-06-19 2018-12-20 Zf Friedrichshafen Ag Vorrichtung und Verfahren zur Ansteuerung eines Fahrzeugmoduls in Abhängigkeit eines Zustandssignals
DE102017006612A1 (de) * 2017-07-12 2019-01-17 Mbda Deutschland Gmbh Inertialsensorsystem für Flugkörper
CN113360841B (zh) * 2021-05-19 2022-05-03 电子科技大学 一种基于监督学习的分布式mimo雷达目标定位性能计算方法
IT202100013952A1 (it) * 2021-05-28 2022-11-28 Mbda italia spa Metodo e sistema per controllare elettronicamente il movimento di un dispositivo servoassistito di ricezione e/o trasmissione e/o riflessione di radiazioni elettromagnetiche

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4413327A (en) * 1970-06-09 1983-11-01 The United States Of America As Represented By The Secretary Of The Navy Radiation circumvention technique
US4260942A (en) * 1978-04-17 1981-04-07 Trw Inc. Failure detection and correction system for redundant control elements
DE3432165A1 (de) * 1984-08-31 1986-03-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Einrichtung zur automatischen rekonfiguration einer intakten geraetekombination
DE3634023A1 (de) * 1986-10-07 1988-04-21 Bodenseewerk Geraetetech Integriertes, redundantes referenzsystem fuer die flugregelung und zur erzeugung von kurs- und lageinformationen
DE3923432C2 (de) * 1989-07-15 1997-07-17 Bodenseewerk Geraetetech Einrichtung zur Erzeugung von Meßsignalen mit einer Mehrzahl von Sensoren
DE3929404A1 (de) 1989-09-05 1991-03-07 Bodenseewerk Geraetetech Verfahren und vorrichtung zum erkennen und identifizieren von fehlern an sensoren
US5742609A (en) * 1993-06-29 1998-04-21 Kondrak; Mark R. Smart canister systems
DE4419925A1 (de) 1994-06-08 1995-12-14 Bodenseewerk Geraetetech Inertialsensor-Einheit
US5721680A (en) * 1995-06-07 1998-02-24 Hughes Missile Systems Company Missile test method for testing the operability of a missile from a launch site
US5719764A (en) * 1995-07-19 1998-02-17 Honeywell Inc. Fault tolerant inertial reference system
DE19645556A1 (de) * 1996-04-02 1997-10-30 Bodenseewerk Geraetetech Vorrichtung zur Erzeugung von Lenksignalen für zielverfolgende Flugkörper

Also Published As

Publication number Publication date
DE19857894A1 (de) 2000-06-21
EP1020699A1 (de) 2000-07-19
EP1020699B1 (de) 2006-08-02

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition