GB1071268A - Guidance systems for vehicles and the like - Google Patents

Guidance systems for vehicles and the like

Info

Publication number
GB1071268A
GB1071268A GB4739863A GB4739863A GB1071268A GB 1071268 A GB1071268 A GB 1071268A GB 4739863 A GB4739863 A GB 4739863A GB 4739863 A GB4739863 A GB 4739863A GB 1071268 A GB1071268 A GB 1071268A
Authority
GB
United Kingdom
Prior art keywords
frequency
frequencies
receiver
vehicle
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
Application number
GB4739863A
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.)
GALILEO OFF SpA
Officine Galileo SpA
Original Assignee
GALILEO OFF SpA
Officine Galileo SpA
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 GALILEO OFF SpA, Officine Galileo SpA filed Critical GALILEO OFF SpA
Publication of GB1071268A publication Critical patent/GB1071268A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F41G7/24Beam riding guidance systems
    • F41G7/26Optical guidance systems
    • 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
    • F41G7/2253Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • 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
    • F41G7/2273Homing guidance systems characterised by the type of waves
    • F41G7/2293Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves

Abstract

1,071,268. Photo-electric guidance systems. OFFICINE GALILEO S.p.A. Dec. 2, 1963 [Dec. 11, 1962], No. 47398/63. Heading H4D. A vehicle is guided by directing an optical radiator beam to a receiver in the vehicle, part of the beam is modulated alternately at a frequency F 1 and a frequency F 2 , the whole beam is amplitude modulated at a reference frequency # 0 and the receiver compares outputs at frequencies F 1 and F 2 and at frequencies F 1 and # 0 to afford control signals which tend to maintain the vehicle on a fixed path with respect to the beam. The embodiment relates to the guidance of a missile by a beam from the ground, frequency F 2 being F 1/2 hereafter termed f. The modulation at frequencies f, 2f is effected by a rotating reticle carrying two series of radial slits one series having twice the number of slits as the other (Fig. 2, not shown); at the receiver the outputs at the two frequencies are compared after amplitude equalization and rectification to give a radial-error signal. The reference signal is produced by a disc which is half transparent and half attenvating, the disc being rotated at a predetermined rate with respect to that of the reticle; at the receiver the reference signal phase is compared with that of the signal of frequency 2f after rectification of the latter to give an angular-error signal. The missile is stabilized against rotation about its own longitudinal axis. Optical and electric frequency filters may be added.
GB4739863A 1962-12-11 1963-12-02 Guidance systems for vehicles and the like Expired GB1071268A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT2443862 1962-12-11

Publications (1)

Publication Number Publication Date
GB1071268A true GB1071268A (en) 1967-06-07

Family

ID=11213517

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4739863A Expired GB1071268A (en) 1962-12-11 1963-12-02 Guidance systems for vehicles and the like

Country Status (4)

Country Link
CH (1) CH403503A (en)
DE (1) DE1292509B (en)
GB (1) GB1071268A (en)
NL (1) NL301272A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2185870A (en) * 1986-01-28 1987-07-29 Diehl Gmbh & Co Missile guidance

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2474681A1 (en) * 1980-01-29 1981-07-31 Telecommunications Sa LIGHT BEAM GUIDING SYSTEM
US4399961A (en) * 1981-04-27 1983-08-23 The United States Of America As Represented By The Secretary Of The Army Tone burst reticle beamrider missile guidance
US4432511A (en) * 1981-05-11 1984-02-21 Northrop Corporation Beam-rider guidance using two overlapping reticle discs

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2403983A (en) * 1945-04-03 1946-07-16 Bell Telephone Labor Inc Representation of complex waves
US2826378A (en) * 1950-12-15 1958-03-11 Jr John Norris Childs Apparatus for radio control of guided missiles
GB793868A (en) * 1955-01-12 1958-04-23 Gen Electric Co Ltd Improvements in or relating to visual position-indicating arrangements

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2185870A (en) * 1986-01-28 1987-07-29 Diehl Gmbh & Co Missile guidance
GB2185870B (en) * 1986-01-28 1990-03-28 Diehl Gmbh & Co A target-tracking mechanism

Also Published As

Publication number Publication date
CH403503A (en) 1965-11-30
DE1292509B (en) 1969-04-10
NL301272A (en) 1965-12-27

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