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DE59913732D1 - missile - Google Patents

missile

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
German (de)
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/en
Application granted granted Critical
Publication of DE59913732D1 publication Critical patent/DE59913732D1/en
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 missile Expired - Lifetime DE59913732D1 (en)

Priority Applications (1)

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

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE1998157894 DE19857894A1 (en) 1998-12-15 1998-12-15 Aircraft launched missile system that has built in controller for reconfiguration and allows function monitoring and error detection
DE59913732T DE59913732D1 (en) 1998-12-15 1999-12-13 missile

Publications (1)

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

Family

ID=7891186

Family Applications (2)

Application Number Title Priority Date Filing Date
DE1998157894 Withdrawn DE19857894A1 (en) 1998-12-15 1998-12-15 Aircraft launched missile system that has built in controller for reconfiguration and allows function monitoring and error detection
DE59913732T Expired - Lifetime DE59913732D1 (en) 1998-12-15 1999-12-13 missile

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE1998157894 Withdrawn DE19857894A1 (en) 1998-12-15 1998-12-15 Aircraft launched missile system that has built in controller for reconfiguration and allows function monitoring and error detection

Country Status (2)

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

Families Citing this family (12)

* 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 (en) * 2001-07-03 2004-07-08 Peter Zahner Devices and methods for the self-sufficient and thus safer departure of steerable external loads from carrier aircraft
DE10158666A1 (en) * 2001-11-28 2003-06-18 Lfk Gmbh Missile independent guide device and method for guiding a missile independently uses orientation features lying outside a target point by means an optical homing head and an image processor
DE102004042990B4 (en) * 2004-09-06 2008-11-20 Michael Grabmeier Method and device for testing an operational cruise missile in various test scenarios by means of maintenance mode
DE102007022672C5 (en) * 2007-05-15 2010-09-09 Lfk-Lenkflugkörpersysteme Gmbh Procedure for condition monitoring of an intelligent weapon and intelligent weapon
DE102008041571B4 (en) 2008-08-26 2019-12-05 Robert Bosch Gmbh Method and device for error handling during operation of an internal combustion engine
US20150205271A1 (en) * 2012-07-17 2015-07-23 Siemens Aktiengesellschaft Automated reconfiguration of a discrete event control loop
DE102014213171A1 (en) * 2014-04-09 2015-10-15 Continental Automotive Gmbh System for autonomous vehicle guidance and motor vehicle
DE102017210151A1 (en) * 2017-06-19 2018-12-20 Zf Friedrichshafen Ag Device and method for controlling a vehicle module in response to a state signal
DE102017006612A1 (en) * 2017-07-12 2019-01-17 Mbda Deutschland Gmbh Inertial sensor system for missiles
CN113360841B (en) * 2021-05-19 2022-05-03 电子科技大学 A Distributed MIMO Radar Target Localization Performance Calculation Method Based on Supervised Learning
IT202100013952A1 (en) * 2021-05-28 2022-11-28 Mbda italia spa Method and system for electronically controlling the movement of a power-assisted device for receiving and/or transmitting and/or reflecting electromagnetic radiation

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 (en) * 1984-08-31 1986-03-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn DEVICE FOR AUTOMATIC RECONFIGURATION OF AN INTACT DEVICE COMBINATION
DE3634023A1 (en) * 1986-10-07 1988-04-21 Bodenseewerk Geraetetech INTEGRATED, REDUNDANT REFERENCE SYSTEM FOR FLIGHT CONTROL AND FOR GENERATING COURSE AND LOCATION INFORMATION
DE3923432C2 (en) * 1989-07-15 1997-07-17 Bodenseewerk Geraetetech Device for generating measurement signals with a plurality of sensors
DE3929404A1 (en) * 1989-09-05 1991-03-07 Bodenseewerk Geraetetech METHOD AND DEVICE FOR DETECTING AND IDENTIFYING ERRORS ON SENSORS
US5742609A (en) * 1993-06-29 1998-04-21 Kondrak; Mark R. Smart canister systems
DE4419925A1 (en) 1994-06-08 1995-12-14 Bodenseewerk Geraetetech Inertial sensor unit
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 (en) * 1996-04-02 1997-10-30 Bodenseewerk Geraetetech Steering signal generating device for target tracking of e.g. military missile

Also Published As

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

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition