SE9001052D0 - PROJECTILE - Google Patents

PROJECTILE

Info

Publication number
SE9001052D0
SE9001052D0 SE9001052A SE9001052A SE9001052D0 SE 9001052 D0 SE9001052 D0 SE 9001052D0 SE 9001052 A SE9001052 A SE 9001052A SE 9001052 A SE9001052 A SE 9001052A SE 9001052 D0 SE9001052 D0 SE 9001052D0
Authority
SE
Sweden
Prior art keywords
cone
sight
symmetry
projectile
line
Prior art date
Application number
SE9001052A
Other languages
Swedish (sv)
Inventor
G Couderc
Original Assignee
Thomson Csf
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 Thomson Csf filed Critical Thomson Csf
Publication of SE9001052D0 publication Critical patent/SE9001052D0/en

Links

Classifications

    • 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
    • G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/48—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
    • G01S7/483—Details of pulse systems
    • G01S7/484—Transmitters
    • 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
    • F41G7/24—Beam riding guidance systems
    • F41G7/26—Optical 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
    • F41G7/24—Beam riding guidance systems
    • F41G7/26—Optical guidance systems
    • F41G7/263—Means for producing guidance beams
    • 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
    • G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
    • G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves
    • G01S1/08—Systems for determining direction or position line
    • G01S1/42—Conical-scan beacons transmitting signals which indicate at a mobile receiver any displacement of the receiver from the conical-scan axis, e.g. for "beam-riding" missile control
    • 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
    • G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
    • G01S17/88—Lidar systems specially adapted for specific applications
    • 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
    • G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/48—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
    • G01S7/481—Constructional features, e.g. arrangements of optical elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Electromagnetism (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Optical Radar Systems And Details Thereof (AREA)

Abstract

In this system the fire-control station) 1 comprises : - means (40 to 45 Fig 4) for tracking a target and defining a line of sight LV ; - means (33 to 39 Fig 4) for scanning with a laser beam (3) a guidance cone 5 whose axis of symmetry AS is locked to said line of sight LV , said cone 5, being made up of elemental cells (e.g. 9, 9' Fig 2) successively illuminated by said beam 3, the beam being deflected by two acousto-optic deflectors (37, 37' Fig 4) in two orthogonal planes; - means for modulating said beam 3 according to a binary sequence (Fig 3) representing said Cartesian coordinates of the cell which is illuminated; and the projectile includes : - means for receiving said laser beam 3 , for demodulating it and for decoding the coordinates; - means for determining a trajectory correction such that said projectile comes closer to the axis of symmetry AS of said guidance cone 5. The beam may carry a message. The effective beam size is controllable in dependence upon range (Fig 5).
SE9001052A 1989-03-24 1990-03-22 PROJECTILE SE9001052D0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8903926 1989-03-24

Publications (1)

Publication Number Publication Date
SE9001052D0 true SE9001052D0 (en) 1990-03-22

Family

ID=9380050

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9001052A SE9001052D0 (en) 1989-03-24 1990-03-22 PROJECTILE

Country Status (4)

Country Link
DE (1) DE4009143A1 (en)
GB (1) GB2459913B (en)
IT (1) IT9047709A1 (en)
SE (1) SE9001052D0 (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1524122A (en) * 1976-01-29 1978-09-06 Elliott Brothers London Ltd Guidance systems for mobile craft
CA1114211A (en) * 1978-10-05 1981-12-15 George W. Stewart, Jr. Prismatic beam rotator for an optical beam projector
US4299360A (en) * 1979-01-30 1981-11-10 Martin Marietta Corporation Beamrider guidance technique using digital FM coding
US4432511A (en) * 1981-05-11 1984-02-21 Northrop Corporation Beam-rider guidance using two overlapping reticle discs
EP0234030B1 (en) * 1986-01-30 1990-11-28 Werkzeugmaschinenfabrik Oerlikon-Bührle AG Guidance system for a missile

Also Published As

Publication number Publication date
GB2459913A (en) 2009-11-18
IT9047709A1 (en) 1990-09-25
DE4009143A1 (en) 2009-12-24
GB9006118D0 (en) 2009-08-12
IT9047709A0 (en) 1990-03-02
GB2459913B (en) 2010-05-19

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