GB1359581A - Optical trackers - Google Patents
Optical trackersInfo
- Publication number
- GB1359581A GB1359581A GB49872A GB49872A GB1359581A GB 1359581 A GB1359581 A GB 1359581A GB 49872 A GB49872 A GB 49872A GB 49872 A GB49872 A GB 49872A GB 1359581 A GB1359581 A GB 1359581A
- Authority
- GB
- United Kingdom
- Prior art keywords
- light
- detector
- screen
- areas
- line
- 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
-
- 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
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/78—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
- G01S3/782—Systems for determining direction or deviation from predetermined direction
- G01S3/785—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system
- G01S3/786—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system the desired condition being maintained automatically
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
1359581 Phuto-electric detector BRITISH AIRCRAFT CORP Ltd 5 Jan 1973 [5 Jan 1972] 498/72 Heading G1A [Also in Division H4] An optical tracker for tracking a distant light source, such as a flare carried by a missile, comprises a cylindrical lens which projects an image of the source, in the form of a focused line of light, upon the screen of a photo-electric detector. The screen has at least one pair of distinct light-sensitive areas, which are so arranged that their respective electrical outputs vary continuously and differentially as the line of light moves transversely to the direction of its length. Sum and difference signals are obtained from the detector outputs, and are used to derive error signals for tracking. The arrangement enables false error signals due to atmospheric shimmer to be reduced. In one form of screen a rectangular light-sensitive area 12, Fig. 2, is split by a diagonal line 13 to provide two triangular areas 12A, 12B. The focused line of light 11 normally lies centrally between the longer edges of the rectangle, producing equal outputs from the two areas. When it moves transversely, the output from one area is reduced, and the output from the other area is correspondingly increased. In another form of screen a rectangular light-sensitive area is divided into two areas each comprising a plurality of triangles, as shown in Fig.4. A form of screen is also described Fig.8 (not shown) in which a rectangular light-sensitive area is split into two by a single diagonal line as in Fig.2 and has a narrow central strip removed, in which is provided a multi-diagonal arrangement similar to that of Fig.4. An azimuthal tracker unit comprises a cylindrical lens 10, Fig.7, with a vertical axis 21 about which a support 20, in the form of a sector of a cylinder, may be rotated by a servomotor through a shaft 22 and worm gearing 23. A potentiometer pick-off 24 enables the position of the support 20 to be monitored. A detector 12, of the kind described with reference to Fig. 8, is symmetrically mounted within the support 20, and two infrared sources 25 are provided which are used intermittently during a tracking operation to illuminate the detector 12, to enable overall balance to be maintained. A similar orthogonally disposed unit may be provided for tracking in elevation. Circuitry for a tracker unit is described with reference to Fig.9 (not shown). This includes provision for switching to the inner areas of the detector 12 as the tracker nears the line of sight to the source, normalizing the difference signal by division by the sum signal, and periodic balancing making use of the pilot sources. In another embodiment, the detectors are fixed relative to their respective cylindrical lenses Fig.10 (not shown).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB49872A GB1359581A (en) | 1973-01-05 | 1973-01-05 | Optical trackers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB49872A GB1359581A (en) | 1973-01-05 | 1973-01-05 | Optical trackers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1359581A true GB1359581A (en) | 1974-07-10 |
Family
ID=9705407
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB49872A Expired GB1359581A (en) | 1973-01-05 | 1973-01-05 | Optical trackers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1359581A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4039825A (en) * | 1974-12-16 | 1977-08-02 | Zed Instruments Limited | Position indicating system |
FR2484097A1 (en) * | 1980-06-06 | 1981-12-11 | Sfim | Aircraft optical displacement sensor for helmet sighting system - uses dihedral prisms to form images of source for linear photo detector to indicate movement of head of pilot |
GB2129245A (en) * | 1982-10-29 | 1984-05-10 | Perkin Elmer Corp | Illumination angle detector |
GB2258576A (en) * | 1991-08-03 | 1993-02-10 | British Aerospace Space & Comm | A visible light detector assembly |
-
1973
- 1973-01-05 GB GB49872A patent/GB1359581A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4039825A (en) * | 1974-12-16 | 1977-08-02 | Zed Instruments Limited | Position indicating system |
FR2484097A1 (en) * | 1980-06-06 | 1981-12-11 | Sfim | Aircraft optical displacement sensor for helmet sighting system - uses dihedral prisms to form images of source for linear photo detector to indicate movement of head of pilot |
GB2129245A (en) * | 1982-10-29 | 1984-05-10 | Perkin Elmer Corp | Illumination angle detector |
GB2258576A (en) * | 1991-08-03 | 1993-02-10 | British Aerospace Space & Comm | A visible light detector assembly |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |