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 beamsInfo
- 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
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
- F41G7/24—Beam riding guidance systems
- F41G7/26—Optical guidance systems
-
- 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
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 .
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)
| 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)
| 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 |
-
1966
- 1966-07-21 FR FR70230A patent/FR1525902A/en not_active Expired
-
1967
- 1967-07-12 IL IL28305A patent/IL28305A/en unknown
- 1967-07-12 GB GB32165/67A patent/GB1161027A/en not_active Expired
- 1967-07-20 SE SE10723/67*A patent/SE350339B/xx unknown
- 1967-07-21 DE DE19671531499 patent/DE1531499A1/en not_active Withdrawn
Cited By (7)
| 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 |