MULTI-DIMENSIONAL IMAGING METHOD AND APPARATUS

• US 20070109177A1
• Filed: 11/06/2006
• Published: 05/17/2007
• Est. Priority Date: 11/04/2005
• Status: Abandoned Application

• Current Assignee: Agellis Group AB (RHI Magnesita NV)
• Original Assignee: Agellis Group AB (RHI Magnesita NV)
• Inventors: Nilsson, Emil, Baath, Lars
• Application Number:
  US11/556,716
• Publication Number:
  US 20070109177A1
• Time in Patent Office: Days
• US Class Current: 342/124
• CPC Class Codes: G01S 13/38 wherein more than one modulation frequency is used
• CPC Class Codes: G01S 13/4454 phase comparisons monopulse, i.e. comparing the echo signals received by an interferometric antenna arrangement
• CPC Class Codes: G01S 13/88 Radar or analogous systems specially adapted for specific applications electromagnetic prospecting or detecting of objects, e.g. near-field detection, G01V3/00
• CPC Class Codes: G01S 13/885 for ground probing prospecting or detecting using electromagnetic waves G01V3/12
• CPC Class Codes: G01S 13/89 for mapping or imaging
• CPC Class Codes: G01S 3/48 the waves arriving at the antennas being continuous or intermittent and the phase difference of signals derived therefrom being measured
• CPC Class Codes: G01V 3/12 operating with electromagnetic waves operating with millimetre waves G01V8/005
• CPC Class Codes: G01V 3/15 specially adapted for use during transport, e.g. by a person, vehicle or boat

Abstract

A method, an antenna, and a system for determining positions for reflection points using microwaves. An electromagnetic wave signal is generated at a defined frequency, and transmitted by an antenna unit the antenna unit includes a transmitter antenna and a plurality of receiver antennas, separated by a known spacing perpendicular to a main line of sight and devised to receive reflected portions of the transmitted wave. Phase comparator means are connected to the transmitter antenna and the receiver antennas, and a control unit connected to the phase comparator means is operable to calculate an angle to a reflection point from detected phase difference between at least two receiver antennas and the spacing between said at least two receiver antennas, and to calculate a distance to the reflection point from detected phase difference between the transmitter antenna and a receiver antenna dependent on the frequency.

Claims

1. Method for determining a position in space for a reflection point, using a transmitter antenna and a plurality of receiver antennas spaced apart perpendicular to a main line of sight, comprising the steps of:

transmitting a coherent electromagnetic wave signal towards the reflection point;

detecting a phase difference between the transmitted signal and a reflected signal from the reflection point received in a receiver antenna;

repeating the steps of transmitting and receiving in a plurality of frequency steps over a frequency band;

determining a distance (r) to the reflection point by measuring variation in phase difference dependent on signal frequency; and

identifying an angle (φ

,θ

) between a line of sight from the receivers to the reflection point, and the main line of sight, dependent on a delay between reception of reflected signals from the reflection point in at least two receiver antennas and a known spacing between said at least two receiver antennas.

2. The method of claim 1, comprising the steps of:

combining the transmitted signal and received signals;

performing a Fourier transformation of the combined signal; and

performing the steps of detecting phase difference and determining delay in the frequency domain.

3. The method of claim 1, wherein the step of identifying an angle comprises the steps of:

combining the signals received in the at least two receiver antennas to an aggregate receiver signal;

determining the delay between reception of reflected signals from the reflection point in the at least two receiver antennas from the aggregate receiver signal; and

calculating the angle based on the determined delay and the known spacing.

4. The method of claim 3, wherein the step of determining the delay between receptions of reflected signals comprises the step of:

determining the phase difference between the received signals.

5. The method of claim 1, comprising the steps of:

detecting amplitude variations in a signal received in at least one receiver antenna;

comparing the amplitude variations with a threshold criterion; and

identifying existence of a reflection point based on the comparison.

6. The method of claim 1, comprising the steps of:

using an isotropic transmitter antenna to simultaneously expose a solid angle;

determining the distance and angle to a plurality of reflection points within an overlap of said solid angle and a field of view of the receivers.

7. The method of claim 1, wherein the step of identifying an angle comprises the steps of:

combining reflected signals received in the at least two receiver antennas to an aggregate receiver signal;

selecting a delay between the at least two receiver antennas, representative of a certain angle of incidence of the reflected signals to the receivers dependent on the known spacing;

detecting amplitude variations in the aggregate receiver signal as a function of the delay between the at least two receiver antennas;

comparing the amplitude variations with a threshold criterion; and

identifying existence of a reflection point based on the comparison.

8. The method of claim 7, comprising the step of:

identifying the angle of incidence to the identified reflection point dependent on the delay of reception and the known spacing between the at least two receiver antennas.

9. The method of claim 6, comprising the step of:

producing a three-dimensional representation of the positions of said plurality of reflection points.

10. The method of claim 6, comprising the step of:

producing a three-dimensional representation of a surface adapted to the determined positions of said plurality of reflection points.

11. The method of claim 10, comprising the step of:

integrating the three-dimensional representation of the surface to determine a volume defined by the surface.

12. The method of claim 6, comprising the steps of

directing the transmitted signal towards an object;

detecting received signals reflected in reflection points of an outer surface of the object;

detecting received signals, which have penetrated the outer surface and reflected in a lower reflection point beneath the outer surface of the object;

determining the position of the lower reflection point.

13. The method of claim 12, comprising the steps of

detecting received signals, which have penetrated the outer surface and reflected in a plurality of lower reflection points beneath the outer surface of the object;

determining the positions of the plurality lower reflection points;

producing a three-dimensional representation of a lower surface adapted to the positions of the plurality of lower reflection points.

14. The method of claim 13, comprising the steps of

integrating the three-dimensional representation of the lower surface to determine a volume defined by the lower surface.

15. The method of claim 1, comprising the step of:

using the transmitter antenna also as one of said receiver antennas.

16. The method of claim 1, used in a cargo supervision application, comprising the steps of:

arranging the transmitter antenna and receiver antennas in a cargo space of a freight vessel;

determining positions for a plurality of reflection points in a surface of a cargo present in the cargo space;

producing a three-dimensional representation of a surface adapted to the determined positions of said plurality of reflection points;

providing the three-dimensional representation to a cargo supervision system.

17. The method of claim 16, comprising the step of:

integrating the three-dimensional representation of a surface against walls of the cargo space to provide a volume representation of the cargo.

18. The method of claim 17, comprising the step of:

determining the mass of the cargo using the volume representation and a density value for the cargo.

19. The method of claim 18, comprising the steps of:

calculating a position of the centre of gravity for the volume representation; and

calculating a heeling parameter representing a tilting force provided by the mass of the cargo.

20. The method of claim 19, comprising the steps of:

comparing the heeling parameter with a preset value; and

triggering an alarm or information output when the heeling parameter exceeds the preset value.

21. The method of claim 1, used in a ground penetrating application, comprising the steps of:

arranging the transmitter antenna and receiver antennas on a support structure;

elevating the support structure over, and aiming the transmitter antenna towards, a ground surface area;

determining positions for a plurality of reflection points present underneath said ground surface;

producing a three-dimensional representation of the points of reflection.

22. The method of claim 1, used in a robot guiding application, comprising the steps of:

providing an industrial robot having a stationary base connected to a movable manoeuvre mechanism;

arranging the transmitter antenna and receiver antennas connected to the robot;

determining positions for a plurality of reflection points on an object to be operated by the robot;

controlling the movement of a robot head of the manoeuvre mechanism dependent on the determined positions.

23. The method of claim 22, comprising the step of:

arranging the transmitter antenna and receiver antennas in a fixed relation to the robot head.

24. The method of claim 22, comprising the step of:

arranging the transmitter antenna and receiver antennas in a fixed relation to the stationary base;

monitoring the movement of the manoeuvre mechanism to determine the relative position of the robot head in relation to the stationary base; and

controlling the movement of a robot head dependent on the determined positions and the movement of the manoeuvre mechanism.

25. The method of claim 1, used in a vehicle positioning application, comprising the steps of:

providing a vehicle comprising driving and steering means;

arranging the transmitter antenna and receiver antennas connected to the vehicle;

determining positions for a plurality of reflection points in an environment of the vehicle;

controlling the driving and steering means of the vehicle dependent on the determined positions.

26. The method of claim 25, comprising the steps of:

determining a distance between the positions of the points of reflection;

identifying a point of reflection based on the distance to an adjacent point of reflection;

retrieving true position data for the identified point of reflection; and

determining the position for the vehicle dependent on the true position of the point of reflection and the determined position of the point of reflection relative to the antenna transmitter.

27. The method of claim 1, used in an application for monitoring a slag surface in a furnace, comprising the steps of:

providing a furnace, containing a melt covered by a slag layer having a slag surface;

arranging the transmitter antenna and receiver antennas at a known position relative the furnace;

determining positions for a plurality of reflection points in the slag surface;

providing a three-dimensional representation of the slag surface;

monitoring the shape or position of the slag surface based on the three-dimensional representation.

28. The method of claim 27, comprising the step of:

presenting an image of the three-dimensional representation on a display.

29. The method of claim 27, comprising the steps of:

comparing position data of the three-dimensional representation with a preset level value;

triggering a warning signal if the position data exceeds the level value.

34. The apparatus as recited in claim 30, further comprising a computer system and computer program code means, which when executed causes the computer system to carry out the steps of claim 1.

30. Apparatus for determining a position in space for a reflection point, comprising:

a signal generator, devised to generate a electromagnetic wave signal at a defined frequency,

an antenna unit, including a transmitter antenna devised to transmit a generated coherent electromagnetic wave, and a plurality of receiver antennas separated by a known spacing perpendicular to a main line of sight and devised to receive reflected portions of the transmitted wave,

phase comparator means connected to the transmitter antenna and the receiver antennas,

a control unit connected to the phase comparator means, operable to calculate an angle to a reflection point from detected phase difference between at least two receiver antennas and the spacing between said at least two receiver antennas, and to calculate a distance to the reflection point from detected phase difference between the transmitter antenna and a receiver antenna dependent on the frequency.

31. The apparatus as recited in claim 30, further comprising a frequency stepping function connected to the signal generator, devised to generate the wave signal at a plurality of frequency steps over a frequency band, wherein the control unit is devised to calculate a distance to the reflection point from a detected variation in the phase difference between the transmitter antenna and a receiver antenna over said frequency steps.

32. The apparatus as recited in claim 30, wherein the transmitter antenna and receiver antennas have a large beam width pattern such that the generated coherent electromagnetic wave is transmitted to cover an entire field or object.

33. The apparatus as recited in claim 32, wherein the beam width pattern represents a full angle field of view of 0-120°

.

35. System for determining the volume of a body, comprising an apparatus as recited in claim 32, wherein the antenna unit is arranged at a distance from the body so as to simultaneously illuminate the whole body from the position of the antenna, wherein the control unit is devised to determine the positions for a plurality of reflection points in a surface of the object, and further comprises means for producing a three-dimensional representation of a surface adapted to the determined positions of said plurality of reflection points, and means for integrating the three-dimensional representation of the surface to determine a volume defined by the surface.

36. System for producing an image of underground features, comprising an apparatus as recited in claim 32, wherein the antenna unit is arranged is held at an elevated position by means of a lifting device so as to simultaneously illuminate an area of a ground surface, wherein the control unit is devised to determine the position for a reflection point located under the ground surface.

37. The system producing an image of underground features as recited in claim 36, wherein the control unit is devised to determine the positions for a plurality of reflection points under the ground surface, and further comprises means for producing a three-dimensional representation of the positions of said plurality of reflection points.

38. System for monitoring a cargo space of a freight vessel, comprising an apparatus as recited in claim 32, wherein the antenna unit is aimed at the cargo space devised for holding a cargo, and wherein the control unit is devised to determine the positions for a plurality of reflection points in a surface of a cargo placed in the cargo space and further comprises means for producing a three-dimensional representation of a surface adapted to the determined positions of said plurality of reflection points arranged, the control unit being communicatively connected to provide the three-dimensional representation to a cargo supervision system.

39. The system for monitoring a cargo space of a freight vessel as recited in claim 38, comprising means for integrating the three-dimensional representation of the surface against walls of the cargo space to provide a volume representation of the cargo.

40. The system for monitoring a cargo space of a freight vessel as recited in claim 39, comprising means for determining the mass of the cargo using the volume representation and a density value for the cargo.

41. The system for monitoring a cargo space of a freight vessel as recited in claim 40, comprising means for calculating a position of the centre of gravity for the volume representation, and means for calculating a heeling parameter representing a tilting force provided by the mass of the cargo on the freight vessel.

42. The system for monitoring a cargo space of a freight vessel as recited in claim 41, comprising means for comparing the heeling parameter with a preset value, and means for triggering an alarm or information output when the heeling parameter exceeds the preset value.

43. System for monitoring a slag surface in a furnace, comprising an apparatus as recited in claim 32, wherein the antenna unit is arranged at a known position relative the furnace and aimed at an interior portion of the furnace, devised to contain a melt covered by a slag layer having a slag surface, wherein the control unit is devised to determine the positions for a plurality of reflection points in the slag surface and further comprises means for providing a three-dimensional representation of the slag surface.

44. The system for monitoring a slag surface in a furnace as recited in claim 43, comprising a display for presenting an image of the three-dimensional representation.

45. The system for monitoring a slag surface in a furnace as recited in claim 43, comprising means for comparing position data of the three-dimensional representation with a preset level value, and means for triggering a warning signal if the position data exceeds the level value.

46. System for guiding a robot having a stationary base connected to a movable manoeuvre mechanism with a robot head, comprising an apparatus as recited in claim 32 with the antenna unit connected to the robot, wherein the control unit is devised to determine the positions for a plurality of reflection points on an object to be operated by the robot, and devised to control the movement of the manoeuvre mechanism dependent on the determined positions.

47. The system for guiding a robot as recited in claim 46, wherein the antenna unit is arranged in a fixed relation to the robot head.

48. The system for guiding a robot as recited in claim 46, wherein the antenna unit is arranged in a fixed relation to the stationary base, and the control unit is devised to monitoring the movement of the manoeuvre mechanism to determine the relative position of the robot head in relation to the stationary base, and to control the movement of the robot head dependent on the determined positions and the movement of the manoeuvre mechanism.

49. System for positioning a vehicle, comprising an apparatus as recited in claim 32, wherein the antenna unit is carried on the vehicle and a number of reflection points are fixed at predetermined positions in an environment of the vehicle, said control unit being devised to determine the relative position of at least two of said number of reflection points with regard to the antenna unit, and to calculate a position for the vehicle dependent on the predetermined position and the relative position for the at least two points of reflection.

50. The system for positioning a vehicle as recited in claim 49, said vehicle comprising driving and steering means, wherein the control unit is further devised to control the driving and steering means of the vehicle dependent on the determined position of the vehicle.

51. The system for positioning a vehicle as recited in claim 49, wherein the control unit is devised to determine a distance between the positions of the at least two points of reflection, and to identify a point of reflection based on the distance to an adjacent point of reflection, the control unit further being devised to retrieve predetermined position data for the identified point of reflection from a memory.

52. Antenna unit, devised for transmission of a coherent electromagnetic wave signal at a defined frequency and reception of a reflected signal from a point of reflection at a position in space, comprising a support structure carrying a transmitter antenna and a plurality of receiver antennas spaced apart perpendicular to a main line of sight of the antenna unit.

53. The antenna unit as recited in claim 52, wherein the receiver antennas are distributed in a plane on said support structure, the normal direction of that plane defining the main line of sight.

54. The antenna unit as recited in claim 52, wherein one of the receiver antennas is also the transmitter antenna.

55. The antenna unit as recited in claim 52, wherein the transmitter antenna and receiver antennas have a large beam width pattern such that the generated coherent electromagnetic wave is transmitted to cover an entire field or object.

56. The antenna unit as recited in claim 55, wherein the beam width pattern represents a full angle field of view of 0-120°

.