IL213743A - Method for controlling a guided missile which is driven by a motor - Google Patents

Method for controlling a guided missile which is driven by a motor

Info

Publication number
IL213743A
IL213743A IL213743A IL21374311A IL213743A IL 213743 A IL213743 A IL 213743A IL 213743 A IL213743 A IL 213743A IL 21374311 A IL21374311 A IL 21374311A IL 213743 A IL213743 A IL 213743A
Authority
IL
Israel
Prior art keywords
driven
controlling
motor
guided missile
missile
Prior art date
Application number
IL213743A
Other languages
Hebrew (he)
Other versions
IL213743A0 (en
Original Assignee
Diehl Bgt Defence Gmbh & 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 & Co Kg filed Critical Diehl Bgt Defence Gmbh & Co Kg
Publication of IL213743A0 publication Critical patent/IL213743A0/en
Publication of IL213743A publication Critical patent/IL213743A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/008—Combinations of different guidance systems
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/12—Target-seeking control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
IL213743A 2010-07-26 2011-06-23 Method for controlling a guided missile which is driven by a motor IL213743A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102010032281A DE102010032281A1 (en) 2010-07-26 2010-07-26 A method of controlling an engine driven missile

Publications (2)

Publication Number Publication Date
IL213743A0 IL213743A0 (en) 2011-12-01
IL213743A true IL213743A (en) 2015-05-31

Family

ID=44971162

Family Applications (1)

Application Number Title Priority Date Filing Date
IL213743A IL213743A (en) 2010-07-26 2011-06-23 Method for controlling a guided missile which is driven by a motor

Country Status (3)

Country Link
EP (1) EP2413086A3 (en)
DE (1) DE102010032281A1 (en)
IL (1) IL213743A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112824820A (en) * 2019-11-21 2021-05-21 北京恒星箭翔科技有限公司 Reverse-low small slow target air defense missile system for 40 mm rocket launcher and intercepting method
DE102020006465B4 (en) 2020-10-21 2022-06-30 Diehl Defence Gmbh & Co. Kg Interceptor missile and method of guiding it
CN113835447B (en) * 2021-09-08 2024-04-05 中国人民解放军91776部队 Bezier curve-based two-dimensional collaborative guidance method for controlling attack angle and time
DE102022001286A1 (en) * 2022-04-13 2023-10-19 Diehl Defence Gmbh & Co. Kg Method for midcourse steering of a thrust-steerable missile
DE102022001287A1 (en) 2022-04-13 2023-10-19 Diehl Defence Gmbh & Co. Kg Method for guiding an interceptor missile
DE102022001285B4 (en) 2022-04-13 2024-08-22 Diehl Defence Gmbh & Co. Kg Method for guiding a missile

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3995792A (en) * 1974-10-15 1976-12-07 The United States Of America As Represented By The Secretary Of The Army Laser missile guidance system
DE3918701A1 (en) * 1989-06-08 1990-12-13 Diehl Gmbh & Co METHOD FOR IMPROVING THE ACCURACY OF A PROGRAMMED FLYING BODY
US6069584A (en) * 1997-12-10 2000-05-30 Rockwell Collins, Inc. Competent munitions using range correction with auto-registration
DE19950669A1 (en) * 1999-10-21 2001-04-26 Bodenseewerk Geraetetech Missile guidance method uses calculated target intersection point for determining flight path and missile velocity characteristic

Also Published As

Publication number Publication date
EP2413086A3 (en) 2012-11-21
DE102010032281A1 (en) 2012-01-26
EP2413086A2 (en) 2012-02-01
IL213743A0 (en) 2011-12-01

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Legal Events

Date Code Title Description
FF Patent granted
KB Patent renewed
KB Patent renewed