Classifications

• • G—PHYSICS
  • G05—CONTROLLING; REGULATING
  • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
  • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
  • G05D1/02—Control of position or course in two dimensions
  • G05D1/021—Control of position or course in two dimensions specially adapted to land vehicles
  • G05D1/0231—Control of position or course in two dimensions specially adapted to land vehicles using optical position detecting means
  • G05D1/0234—Control of position or course in two dimensions specially adapted to land vehicles using optical position detecting means using optical markers or beacons
• • 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
  • G01S3/783—Systems for determining direction or deviation from predetermined direction using amplitude comparison of signals derived from static detectors or detector 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
  • G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
  • G01S5/16—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using electromagnetic waves other than radio waves
• • G—PHYSICS
  • G05—CONTROLLING; REGULATING
  • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
  • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
  • G05D1/02—Control of position or course in two dimensions
  • G05D1/021—Control of position or course in two dimensions specially adapted to land vehicles
  • G05D1/0268—Control of position or course in two dimensions specially adapted to land vehicles using internal positioning means
  • G05D1/027—Control of position or course in two dimensions specially adapted to land vehicles using internal positioning means comprising intertial navigation means, e.g. azimuth detector

Definitions

• the present invention relates to devices for use in automatic vehicle guidance systems.
• a 5 simple example is the system used for the transfer of coal waste to slag heaps. More complicated systems are used in the movement of materials within factories and warehouses. However, these systems usually rely on rails or on fixed paths defined by, for example, buried guide wires, and are governed by inter alia, signals received from trip 10 switches, photo-electric cells, or similar position sensors. The uses of such systems are therefore very inflexible, and are suitable only for the most routine type of task.
• Patent GB 2129161B There is a requirement for more flexible systems, and one such system is described in Patent GB 2129161B. This Patent describes a
• the vehicles and transmitters may also, in some instance, be desirable to have camerasmounted on the vehicles and transmitters mounted at fixed positions.
• the vehicles can only be used on very flat 30 surfaces so that pitch and roll of a vehicle does not prevent reception of signals.
• an automatic vehicle guidance system includes a lens having almost a full 360° view in azimuth and a substantial angle of view in elevation, afocusingdevice for focusing a beam of light from the lens on to a substantially annular photo detector, and means for relating a focusing point on the photo detector to a reference axis.
• the device is used, for example, in an automatic vehicle guidance system having a plurality of light emitting sources, henceforth referred to as beacons, and a plurality of bearing sensing devices.
• the beacons may be fixed, with the bearing sensing devices mounted on vehicles, in which case there will be a reference axis fixed relative to each vehicle; alternatively the bearing sensing devices can be fixed with the beacons mounted on vehicles, in which case the reference axis will be fixed relative to-the bearing sensing devices.
• the beacons can advantageously be used in a sequentially pulsed fashion.
• a preferred photo detector is formed from a continuous P-N junc- tion together with a highly uniform resistive sheet. Suitable material is commercially available. Material is formed into an annulus with electrodes deposited at each-end, forming a one-dimensional lateral effect photo-diode. When a point on the surface of this detector is exposed to light a photo-electric curren is generated at the point. ⁇ h e current divides and flows through the resistive layer to the electrodes, which are normally tied to a ground potential.
• the means for relating the focusing point to the reference axis preferably use a ratiometric converter which compares the ratio of currents flowing from the focusing point to each of the electrodes to define the position of the point on the annulus.
• the known fixed relationship of the detector relative to the axis then allows a relation to be made between focusing point and axis.
• a "fish-eye" type of lens is used, positioned to give a field of view from approximately horizontal to almost vertical throughout almost a full 360° in azimuth, beams entering the fish eye lens being focused by a focusing lens onto the photo detector.
• a spherical reflecting lens is used, light reflected therefrom being focused onto the photo detector.
• Figure 2(a) and (b) show 2 environments in which the vehicle of Figure 1 can operate.
• Figure 3 and Figure 4 are block diagrams of guidance systems for vehicles operating in the environments of Figure 2(a), Figure 2(b) respectively.
• Figure 5(a) is detail of one embodiment of the invention.
• Figure 5(b) is a section through a field of view of the device illustrated in Figure 5(a).
• Figure 6(a) is a detail of a second embodiment of the invention.
• Figure 6(b) is a section through a field of view of the device of Figure 6(a) .
• Figure 7(a) is a plan view of a photo detector as used in the invention.
• Figure 7(b) shows a potentiometric equivalent circuit for- the photo dectector of Figure 7(a).
• a vehicle with which a device according to the invention can be used (Figure 1) has a body 10 mounted on wheels 11 driven and steered according to commands from a control box 12.
• the vehicle 10 can operate in an environment (2) (a) in which a bearing sensing device according to the invention, 13, mounted on the vehicle receives signals from a plurality .of fixed beacons 14; or in an environment (2(b)) in which beacons 24 (shown indittedlines in Figure 1) mounted as far apart as possible on vehicle 10 send signals, to fixed bearing sensing devices 23.
• control unit 12 When operating in the environment illustrated in 2(a) the control unit 12 will typically contain ( Figure 3) the bearing sensing device 13 which sends signals to a beacon check unit 30 and to a ratiometric converter 31.
• the beacon check unit 30 sends a signal to a timer controller 32 which passes signals to the ratiometric converter 31 and to a computer 33 whi ⁇ h also receives a signal from the ratiometric converter 31.
• the computer then ' signals a pilot unit 34 which controls the steering and driving of the wheels 11.
• the fixed beacons 14 send sequentially pulsed signals according to the control of a flash timer 15.
• the control unit 12 When operating in the environment of Figure 2(b) the control unit 12 will typically contain ( Figure 4) a radio receiver 40 which receives signals from a transmitter 45 in a control unit 41 and which controls sequential flashing of beacons 24 and operation of a pilot unit 34.
• the ground control units contain a series of bearing sensing devices 23 each of which sends signals to an associated beacon check 30 and ratio metric converter 31.
• a signal from the beacon check 30 passes to a master timer 42 which sends signals to each ratiometric converter 31, to a master computer 43 and to a flash timer 44.
• the master computer 43 receives signals from each ratiometric converter 31 and sends command signals ' to a transmitter 45 which also receives signals from the flash timer 44, and which sends command signals to the receiver 40.
• a bearing sensing device 13, 23, ( Figure 5) (a) has anultra-wideangle (fish eye) lens 50 directingabeam of light 51 from a beacon 14, 24 through a field stop 52 to a lens 53 which focuses the beam onto an annular photo detector 54.
• a bearing sensing device of this type has a field of view ( Figure 5(b)) 55 extending from horizontal to within about 20° of the vertical.
• a beam of light 61 from a beacon 14, 24 passes through a cylindrical window 62 and is reflected by a spherical mirror 60 through a field stop 52 to be focused by a lens 53 onto an annular photo detector 54.
• the cylind ⁇ rical window 62 must be robust as well as of good optical quality as it must support the field stop 52, lens 53, and photo detector 54 and associated structure (not shown in this figure) which must be situated above the spherical mirror 60.
• the field of view of this type of bearing sensing device (Figure 6(b)) extends from slightly below the horizontal to slightly less than vertical.
• the annular photo detector 54 ( Figure 7(a)) is in the form of an annulus extending over almost 360° and is formed from a continous P-N junction together with a highly uniform resistance sheet. Electrodes 70, 71 are deposited on the ends of the annulus. In use, when a beam of light falls on a point 72 of the annulus 54 current passes to both electrodes 70 and 71, and by comparing these currents, in a manner analogous to that illustrated in 7(b), the position 72 along theannulus can be identified.
• the beacons 14 sequentially emit flashes of light under the control of the flash timer 15.
• the bearing sensing device 13 on the vehicle 10 senses the flash of light and signals the beacon check 30 which checks (in a manner which forms no part of the current invention) which beacon sent the signal, and passes this information to the timer 32.
• a signal corresponding to the currents passing alongthepaths 72-70and71-70 is alsopassedto the radiometric converter 31 which calculates the position of the point 72 on the annulus 53 andcompares thiswiththe known position of an axis 16 of the vehicle 10 to give the bearing of the beacon 14 which is identified from the timer 32.
• This information is fed to the' computer 33 and stored.
• beacon bearings are being stored by the computer it calculates the position of the vehicle 10 and signals the pilot unit 34 to make any necessary adjustments to the steering and speed of the vehicle 10.
• each oftheenvironments 2(a), (b) will have its own advantages and disadvantages.
• the blind spot due to the electrodes 70, 71 on the photo detector 53 may be a disadvantage, but this environment does not require the use of a radio transmitter such as required in environment 2(b).
• the arrangement of environment 2(b) enables the computer 43 to store the positions and vector velocities of all vehicles 10 and arrange for collisions to be avoided.
• Figures 5, 6 has its own advantages.
• the lens 50 might be expected to be more accurate than the spherical lens 60, but does tend to be much more expensive.

Landscapes

• Physics & Mathematics (AREA)
• Engineering & Computer Science (AREA)
• Radar, Positioning & Navigation (AREA)
• Remote Sensing (AREA)
• General Physics & Mathematics (AREA)
• Electromagnetism (AREA)
• Aviation & Aerospace Engineering (AREA)
• Automation & Control Theory (AREA)
• Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
• Traffic Control Systems (AREA)
• Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Applications Claiming Priority (2)

Publications (1)

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ID=10624262

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• 1987
  • 1987-09-23 GB GB878722403A patent/GB8722403D0/en active Pending
• 1988
  • 1988-09-19 AU AU24277/88A patent/AU2427788A/en not_active Abandoned
  • 1988-09-19 KR KR1019890700895A patent/KR890702099A/ko not_active Application Discontinuation
  • 1988-09-19 EP EP88908279A patent/EP0383783A1/de not_active Withdrawn
  • 1988-09-19 WO PCT/GB1988/000768 patent/WO1989003076A1/en not_active Application Discontinuation
  • 1988-09-22 ES ES8802885A patent/ES2010803A6/es not_active Expired
  • 1988-09-22 PT PT88573A patent/PT88573A/pt not_active Application Discontinuation
• 1990
  • 1990-03-07 GB GB9005253A patent/GB2231741B/en not_active Expired - Lifetime

Non-Patent Citations (1)

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