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GB1161027A - Improvements to optical systems for the guidance of moving bodies by multiple director beams - Google Patents

Improvements to optical systems for the guidance of moving bodies by multiple director beams

Info

Publication number
GB1161027A
GB1161027A GB32165/67A GB3216567A GB1161027A GB 1161027 A GB1161027 A GB 1161027A GB 32165/67 A GB32165/67 A GB 32165/67A GB 3216567 A GB3216567 A GB 3216567A GB 1161027 A GB1161027 A GB 1161027A
Authority
GB
United Kingdom
Prior art keywords
pulse
interval
circuit
fed
pulses
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
GB32165/67A
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.)
Compagnie Francaise Thomson Houston SA
Original Assignee
Compagnie Francaise Thomson Houston SA
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 Compagnie Francaise Thomson Houston SA filed Critical Compagnie Francaise Thomson Houston SA
Publication of GB1161027A publication Critical patent/GB1161027A/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
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S1/00Beacons 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
    • G01S1/02Beacons 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

Landscapes

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

Abstract

1,161,027. Optical position finding means. COMPAGNIE FRANCAISE THOMSON HOUSTON-HOTCHKISS BRANDT. 12 July, 1967 [21 July, 1966], No. 32165/67. Heading H4D. Specification describes a modification of the optical navigation system described in Specification 1,160,827 wherein the transmission of an omnidirectional reference radio or light beam, is dispensed with, and the position of the mobile craft receiver with respect to a reference line is determined by comparing the interval between successive illuminations g 1 , g 2 , Fig. 11, of the craft by the direction beam, and a predetermined reference time R 1 -R 2 equal to said interval on said reference line. In addition, to reduce the number of moving parts in the beam transmitters, the rotary beam coder/modulators are replaced by fixed multi-slit apertures Fs, Fig. 4, and Fg, Fig. 5, which divide each director beam into a plurality of sub-beams, which, on scanning the mobile craft, give rise to a pulse train comprising a number of sub pulses Ns and Ng characteristic of the bearing or elevation director beam and allowing the identification thereof in decoder R23, Fig. 10. Corresponding pulses g 1 , g 2 are thus produced by the decoder R23 and fed to displacement measurement means R24. The interval g 1 -g 2 is established by a bi-stable circuit 240, triggered by the pulses g 1 , g 2 to give pulse (E1), Fig. 11. A monostable circuit 246 with controllable period is triggered by pulse g 1 (pulse g 2 being blocked by gate 245) to give an output pulse (D) with a duration normally representative of the interval To = R1-R2. A comparator 244 receives the outputs of circuits 240 and 246 and yields pulse (H1) with a duration representing the deviation of the craft from the reference line. To control circuit 246, successive first pulses g 1 , g 11 are fed to a bi-stable circuit 263 to produce a pulse Eg having a duration Tr equal to the repetition period of the scan. A threshold device 264 and integrator 265 produce a D.C. signal at one input of level comparator 266 equal to mTr. Known interval To is expressed as a fraction of Tr, whence Tr = KTo and said input signal is mKTo. The output (D) of circuit 246 of duration (To + #), where # is the error, is fed to a threshold device 260, a " times K " amplitude multiplier 261 and an integrator 262. A D.C. signal is thus produced at the second input of comparator 266 equal to mK(To + #). Comparator 266 thus produces a signal indicating T which is fed to readjust circuit 246. Alternatively reference interval To may be expressed as a multiple K of the period #r of the plurality Ng, Ns of sub-pulses. Thus a controlled pulse generator 270, Fig. 12 (not shown), may be synchronized with the subpulses, and feed its output via " times K " multiplier means 276 and integrator means 277, to control circuit 246. As another alternative, circuit 246 may be dispensed with, Fig. 13 (not shown), and the output of integrator 277 fed to one input of a level comparator 283 receiving at its other input a D.C. signal representing the interval g 1 -g 2 .
GB32165/67A 1966-07-21 1967-07-12 Improvements to optical systems for the guidance of moving bodies by multiple director beams Expired GB1161027A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR70230A FR1525902A (en) 1966-07-21 1966-07-21 Improvements to optical systems for simultaneous guidance of a plurality of mobile units by multiple guiding beams

Publications (1)

Publication Number Publication Date
GB1161027A true GB1161027A (en) 1969-08-13

Family

ID=8613744

Family Applications (1)

Application Number Title Priority Date Filing Date
GB32165/67A Expired GB1161027A (en) 1966-07-21 1967-07-12 Improvements to optical systems for the guidance of moving bodies by multiple director beams

Country Status (5)

Country Link
DE (1) DE1531499A1 (en)
FR (1) FR1525902A (en)
GB (1) GB1161027A (en)
IL (1) IL28305A (en)
SE (1) SE350339B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2907589A1 (en) * 1978-03-02 1979-09-06 Saab Scania Ab PROCESS AND DEVICE FOR TRANSFERRING INFORMATION BY MEANS OF SWIVELING COMPARTMENT BEAMS
US4218138A (en) * 1978-03-02 1980-08-19 Saab-Scania Aktiebolag Method and means for determining positions of reflectors with fan-shaped beams
US4218834A (en) * 1978-03-02 1980-08-26 Saab-Scania Ab Scoring of simulated weapons fire with sweeping fan-shaped beams
GB2350248A (en) * 1982-07-09 2000-11-22 Short Brothers Ltd Furnishing information to determine the position of a body
RU2815295C1 (en) * 2023-10-02 2024-03-13 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Tracking guidance system

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2441145A1 (en) * 1978-11-09 1980-06-06 Aerospatiale GUIDANCE SYSTEM FOR BURST SHOT OF REMOTE CONTROLLED MISSILES
FR2503857B1 (en) * 1981-04-10 1986-02-14 Cilas DEVICE FOR GUIDING A MOBILE MACHINE
GB2113939B (en) * 1981-11-19 1985-07-10 British Aerospace Angular position determination

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2907589A1 (en) * 1978-03-02 1979-09-06 Saab Scania Ab PROCESS AND DEVICE FOR TRANSFERRING INFORMATION BY MEANS OF SWIVELING COMPARTMENT BEAMS
US4218138A (en) * 1978-03-02 1980-08-19 Saab-Scania Aktiebolag Method and means for determining positions of reflectors with fan-shaped beams
US4218834A (en) * 1978-03-02 1980-08-26 Saab-Scania Ab Scoring of simulated weapons fire with sweeping fan-shaped beams
US4227261A (en) * 1978-03-02 1980-10-07 Saab-Scania Ab Transmission of information by sweeping fan-shaped beams
GB2350248A (en) * 1982-07-09 2000-11-22 Short Brothers Ltd Furnishing information to determine the position of a body
GB2350248B (en) * 1982-07-09 2001-04-04 Short Brothers Ltd A method of, and apparatus for. furnishing information to determine the position of a body
RU2815295C1 (en) * 2023-10-02 2024-03-13 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Tracking guidance system

Also Published As

Publication number Publication date
FR1525902A (en) 1968-05-24
SE350339B (en) 1972-10-23
IL28305A (en) 1971-05-26
DE1531499A1 (en) 1969-08-28

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee