GB9310865D0 - Method for the independent control of a guidable flying body provided with a warhead and arrangement for the performance of the method - Google Patents

Method for the independent control of a guidable flying body provided with a warhead and arrangement for the performance of the method

Info

Publication number
GB9310865D0
GB9310865D0 GBGB9310865.2A GB9310865A GB9310865D0 GB 9310865 D0 GB9310865 D0 GB 9310865D0 GB 9310865 A GB9310865 A GB 9310865A GB 9310865 D0 GB9310865 D0 GB 9310865D0
Authority
GB
United Kingdom
Prior art keywords
guidable
warhead
performance
arrangement
body provided
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.)
Pending
Application number
GBGB9310865.2A
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.)
Airbus Defence and Space GmbH
Original Assignee
Deutsche Aerospace AG
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
Priority claimed from DE4309295A external-priority patent/DE4309295A1/en
Application filed by Deutsche Aerospace AG filed Critical Deutsche Aerospace AG
Publication of GB9310865D0 publication Critical patent/GB9310865D0/en
Pending 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
    • F41G7/2246—Active homing systems, i.e. comprising both a transmitter and a receiver
    • 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
    • F41G7/2273—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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/883—Radar or analogous systems specially adapted for specific applications for missile homing, autodirectors
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/89—Radar or analogous systems specially adapted for specific applications for mapping or imaging
    • G01S13/90—Radar or analogous systems specially adapted for specific applications for mapping or imaging using synthetic aperture techniques, e.g. synthetic aperture radar [SAR] techniques
    • G01S13/904—SAR modes
    • G01S13/9043—Forward-looking SAR
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00—Details of, or arrangements associated with, antennas
    • H01Q1/27—Adaptation for use in or on movable bodies
    • H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00—Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/02—Antennas or antenna systems providing at least two radiating patterns providing sum and difference patterns

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Astronomy & Astrophysics (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GBGB9310865.2A 1992-06-29 1993-05-26 Method for the independent control of a guidable flying body provided with a warhead and arrangement for the performance of the method Pending GB9310865D0 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE4220748 1992-06-29
DE4309295A DE4309295A1 (en) 1992-06-29 1993-03-23 Guided missile control system

Publications (1)

Publication Number Publication Date
GB9310865D0 true GB9310865D0 (en) 1995-11-22

Family

ID=25915990

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB9310865.2A Pending GB9310865D0 (en) 1992-06-29 1993-05-26 Method for the independent control of a guidable flying body provided with a warhead and arrangement for the performance of the method
GB9312560A Expired - Fee Related GB2290671B (en) 1992-06-29 1993-06-18 Guidance of an armed flying body

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB9312560A Expired - Fee Related GB2290671B (en) 1992-06-29 1993-06-18 Guidance of an armed flying body

Country Status (2)

Country Link
FR (1) FR2723191B1 (en)
GB (2) GB9310865D0 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102150569B1 (en) * 2019-02-28 2020-09-01 국방과학연구소 Method and apparatus for estimating position of guided missile

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2226066A5 (en) * 1970-10-13 1974-11-08 Bodenseewerk Geraetetech
IT1074498B (en) * 1976-09-16 1985-04-20 Selenia Ind Elettroniche IMPROVEMENT IN ELEVATION ERROR REDUCTION SYSTEMS FOR LOW ALTITUDE TARGET TRACKING RADAR
DE2830502C3 (en) * 1978-07-12 1981-10-08 Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen Missile control device
US4665401A (en) * 1980-10-10 1987-05-12 Sperry Corporation Millimeter wave length guidance system
DE3145374C2 (en) * 1981-11-14 1984-12-20 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Method and device for combating ground targets by means of missiles
FR2531231A1 (en) * 1982-07-28 1984-02-03 Telecommunications Sa PASSIVE GUIDANCE METHOD FOR MACHINE
US5061930A (en) * 1990-06-12 1991-10-29 Westinghouse Electric Corp. Multi-mode missile seeker system

Also Published As

Publication number Publication date
FR2723191A1 (en) 1996-02-02
GB2290671A (en) 1996-01-03
FR2723191B1 (en) 1997-11-21
GB2290671B (en) 1996-06-26
GB9312560D0 (en) 1995-11-08

Similar Documents

Publication Publication Date Title
GB2272783B (en) Aircraft engine control system
GB2271791B (en) Well orienting tool and/or thruster
KR0133373B1 (en) Magnetic head assembly the manufacturing method and
EP0586932A3 (en) Crash-helmet with a morphologically head fitted lining and method for manufacturing the same
EP0489712A3 (en) Missile steering arrangement using thrust control
GB2194838B (en) A flying body
IL107844A0 (en) Flight control device for missiles
AR244181A1 (en) Method for the control of mollusks
GB2256622B (en) A flying body having rudder or control blades
DE3665204D1 (en) Method for controlling and/or regulating the operating caracteristics of a combustion engine
AU4197489A (en) Process and device for controlling the longitudinal and transverse motion of a vehicle
EP0357526A3 (en) Print head assembly acceleration control method
EP0403658A4 (en) Method of controlling the speed of a servomotor
AR243483A1 (en) Method for the control of mollusks
GB9310865D0 (en) Method for the independent control of a guidable flying body provided with a warhead and arrangement for the performance of the method
EP0332119A3 (en) Electronic-type engine control method
GB8905631D0 (en) Jettisonable aerodynamic control surface
GB2328497B (en) Method for guiding a missile and missiles
AU670280B2 (en) A detonator harness unit and a method of making the same
AU3696493A (en) Multilayered structural body
GB2231942B (en) A submunition flying body
AU4491689A (en) Method for guiding a moving body, and moving body guided according to the method
EP0600549A3 (en) Thin-film magnetic head and method of manufacturing the magnetic head.
IL91224A0 (en) Flying body for the setting-down of a load
EP0368256A3 (en) Serial printer and a method of assembling the same