SYSTEM AND METHOD FOR USING GLOBAL NAVIGATION SATELLITE SYSTEM (GNSS) NAVIGATION AND VISUAL NAVIGATION TO RECOVER ABSOLUTE POSITION AND ATTITUDE WITHOUT ANY PRIOR ASSOCIATION OF VISUAL FEATURES WITH KNOWN COORDINATES

• US 20150219767A1
• Filed: 01/29/2015
• Published: 08/06/2015
• Est. Priority Date: 02/03/2014
• Status: Abandoned Application

• Current Assignee: Board of Regents of the University of Texas System (University of Texas System)
• Original Assignee: Board of Regents of the University of Texas System (University of Texas System)
• Inventors: Humphreys, Todd E., Shepard, Daniel P., Pesyna, Kenneth Jr., Bhatti, Jahshan
• Application Number:
  US14/608,381
• Publication Number:
  US 20150219767A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01S 19/43 using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry
• CPC Class Codes: G01S 19/485 whereby the further system is an optical system or imaging system
• CPC Class Codes: G01S 19/49 whereby the further system is an inertial position system, e.g. loosely-coupled
• CPC Class Codes: G01S 19/54 using carrier phase measurements; using long or short baseline interferometry

Abstract

An apparatus includes a global navigation satellite system antenna, a global navigation satellite system receiver, a camera, and a processor. The mobile global navigation satellite system receiver produces a set of carrier-phase measurements from a global navigation satellite system. The camera produces an image. The processor determines an absolute position and an absolute attitude of the apparatus solely from three or more sets of data and a rough estimate of the absolute position of the apparatus without any prior association of visual features with known coordinates. Each set of data includes the image and the set of carrier-phase measurements. In addition, the processor uses either a precise orbit and clock data for the global navigation satellite system or another set of carrier-phase measurements from another global navigation satellite system antenna at a known location in each set of data.

Claims

1. An apparatus comprising:

a first global navigation satellite system antenna;

a mobile global navigation satellite system receiver connected to the first global navigation satellite system antenna that produces a first set of carrier-phase measurements from a global navigation satellite system;

an interface that receives a second set of carrier-phase measurements based on a second global navigation satellite system antenna at a known location;

a camera that produces an image; and

a processor communicably coupled to the mobile global navigation satellite system receiver, the interface and the camera, wherein the processor determines an absolute position and an absolute attitude of the apparatus solely from three or more sets of data and a rough estimate of the absolute position of the apparatus without any prior association of visual features with known coordinates, each set of data comprises the image, the first set of carrier-phase measurements and the second set of carrier-phase measurements.

2. The apparatus as recited in claim 1, wherein the global navigation satellite system comprises a global system, a regional system, a national system, a military system, a private system or a combination thereof.

3. The apparatus as recited in claim 1, wherein the processor also uses a prior map of visual features to determine the absolute position and the absolute attitude of the apparatus.

4. The apparatus as recited in claim 1, wherein the rough estimate of the absolute position of the apparatus is obtained using a first set of pseudorange measurements from the mobile global navigation satellite system receiver in each set of data.

5. The apparatus as recited in claim 4, wherein each set of data further comprises a second set of pseudorange measurements from the second global navigation satellite system antenna.

6. The apparatus as recited in claim 1, wherein the rough estimate of the absolute position of the apparatus is obtained using a prior map of visual features, a set of coordinates entered by a user when the apparatus is at a known location, a radio frequency finger-printing, or a cell phone triangulation.

7. The apparatus as recited in claim 1, wherein the first set and second set of carrier-phase measurements are from two or more global navigation satellite systems.

8. The apparatus as recited in claim 1, wherein the first set and second set of carrier-phase measurements are from signals at two or more different frequencies.

9. The apparatus as recited in claim 1, further comprising a visual simultaneous localization and mapping module communicably coupled between the camera and the processor.

10. The apparatus as recited in claim 1, the interface comprising a wireless network interface, a wired network interface, a wireless transceiver or a global navigation satellite system receiver communicably connected to the second global navigation satellite system antenna.

11. The apparatus as recited in claim 1, wherein the processor and the interface are remotely located with respect to the first global navigation satellite system antenna, the mobile global navigation satellite system receiver and the camera.

12. The apparatus as recited in claim 1, further comprising a global navigation satellite system positioning module communicably coupled between the processor and the mobile global navigation satellite system receiver and the interface.

13. The apparatus as recited in claim 1, wherein the camera comprises a video camera, a smart-phone camera, a web-camera, a monocular camera, a stereo camera, or a camera integrated into a portable device.

14. The apparatus as recited in claim 1, wherein the camera comprises two or more cameras.

15. The apparatus as recited in claim 1, further comprising an inertial measurement unit communicably coupled to the processor.

16. The apparatus as recited in claim 15, wherein the inertial measurement unit comprises a single-axis accelerometer, a dual-axis accelerometer, a three-axis accelerometer, a three-axis gyro, a dual-axis gyro, a single-axis gyro, a magnetometer or a combination thereof.

17. The apparatus as recited in claim 16, wherein the inertial measurement unit further comprises a thermometer.

18. The apparatus as recited in claim 1, wherein the processor comprises:

a propagation step module;

a global navigation satellite system measurement update module communicably coupled to the mobile global navigation satellite system receiver, the interface and the propagation step module;

a visual navigation system measurement update module communicably coupled to the camera and the propagation step module; and

a filter state to camera state module communicably coupled to the propagation step module that provides the absolute position and the absolute attitude of the apparatus.

19. The apparatus as recited in claim 18, wherein the processor further comprises a visual simultaneous localization and mapping module communicably coupled between the visual navigation system measurement update module and the camera.

20. The apparatus as recited in claim 18, further comprising:

an inertial measurement unit communicably coupled to the propagation step module of the processor; and

the processor further comprises an inertial navigation system update module communicably coupled to the inertial measurement unit, the propagation step module and the global navigation satellite system measurement update module.

21. The apparatus as recited in claim 1, further comprising a power source connected to the mobile global navigation satellite system receiver, the camera and the processor.

22. The apparatus as recited in claim 21, wherein the power source comprises a battery, a solar panel or a combination.

23. The apparatus as recited in claim 1, further comprising a display electrically connected or wirelessly connected to the processor and the camera.

24. The apparatus as recited in claim 23, wherein the display comprises a computer, a display screen, a lens, a pair of glasses, a wrist device, a handheld device, a phone, a personal data assistant, a tablet or a combination thereof.

25. The apparatus as recited in claim 1, wherein the processor provides an output to a remote device.

26. The apparatus as recited in claim 1, further comprising a structure, frame or enclosure rigidly connected to the mobile global navigation satellite system receiver and the camera.

27. The apparatus as recited in claim 1, wherein the mobile global navigation satellite system receiver, the interface, the camera and the processor are integrated together into a single device.

28. The apparatus as recited in claim 1, wherein the processor provides at least centimeter-level position and degree-level attitude accuracy in open outdoor locations.

29. The apparatus as recited in claim 1, wherein the apparatus transitions indoors and maintains highly-accurate global pose for a limited distance of travel without global navigation satellite system availability.

30. The apparatus as recited in claim 1, wherein the processor operates in a post-processing mode or a real-time mode.

31. The apparatus as recited in claim 1, wherein the apparatus comprises a navigation device, an augmented reality device, a 3-Dimensional rendering device or a combination thereof.

32. An apparatus comprising:

a global navigation satellite system antenna;

a mobile global navigation satellite system receiver connected to the global navigation satellite system antenna that produces a set of carrier-phase measurements from a global navigation satellite system with signals at multiple frequencies;

a camera that produces an image; and

a processor communicably coupled to the mobile global navigation satellite system receiver and the camera, wherein the processor determines an absolute position and an absolute attitude of the apparatus solely from three or more sets of data, a rough estimate of the absolute position of the apparatus and a precise orbit and clock data for the global navigation satellite system without any prior association of visual features with known coordinates, each set of data comprises the image and the set of carrier-phase measurements.

33. The apparatus as recited in claim 32, wherein the global navigation satellite system comprises a global system, a regional system, a national system, a military system, a private system or a combination thereof.

34. The apparatus as recited in claim 32, wherein the processor also uses a prior map of visual features to determine the absolute position and the absolute attitude of the apparatus.

35. The apparatus as recited in claim 32, wherein the rough estimate of the absolute position of the apparatus is obtained using a set of pseudorange measurements from the mobile global navigation satellite system receiver in each set of data.

36. The apparatus as recited in claim 32, wherein the rough estimate of the absolute position of the apparatus is obtained using a prior map of visual features, a set of coordinates entered by a user when the apparatus is at a known location, a radio frequency finger-printing, or a cell phone triangulation.

37. The apparatus as recited in claim 32, further comprising a visual simultaneous localization and mapping module communicably coupled between the camera and the processor.

38. The apparatus as recited in claim 32, wherein the precise orbit and clock data provide decimeter-level or better positioning and nano-second or better timing for the satellites.

39. The apparatus as recited in claim 32, wherein the processor is remotely located with respect to the global navigation satellite system antenna, the mobile global navigation satellite system receiver and the camera.

40. The apparatus as recited in claim 32, further comprising a global navigation satellite system positioning module communicably coupled between the processor and the mobile global navigation satellite system receiver.

41. The apparatus as recited in claim 32, wherein the camera comprises a video camera, a smart-phone camera, a web-camera, a monocular camera, a stereo camera, or a camera integrated into a portable device.

42. The apparatus as recited in claim 32, wherein the camera comprises two or more cameras.

43. The apparatus as recited in claim 32, further comprising an inertial measurement unit communicably coupled to the processor.

44. The apparatus as recited in claim 43, wherein the inertial measurement unit comprises a single-axis accelerometer, a dual-axis accelerometer, a three-axis accelerometer, a three-axis gyro, a dual-axis gyro, a single-axis gyro, a magnetometer or a combination thereof.

45. The apparatus as recited in claim 43, wherein the inertial measurement unit further comprises a thermometer.

46. The apparatus as recited in claim 32, wherein the processor comprises:

a propagation step module;

a global navigation satellite system measurement update module communicably coupled to the mobile global navigation satellite system receiver and the propagation step module;

a visual navigation system measurement update module communicably coupled to the camera and the propagation step module; and

a filter state to camera state module communicably coupled to the propagation step module that provides the absolute position and the absolute attitude of the apparatus.

47. The apparatus as recited in claim 46, wherein the processor further comprises a visual simultaneous localization and mapping module communicably coupled between the visual navigation system measurement update module and the camera.

48. The apparatus as recited in claim 46, further comprising:

an inertial measurement unit communicably coupled to the propagation step module of the processor; and

the processor further comprises an inertial navigation system update module communicably coupled to the inertial measurement unit, the propagation step module and the global navigation satellite system measurement update module.

49. The apparatus as recited in claim 32, further comprising a power source connected to the mobile global navigation satellite system receiver, the camera and the processor.

50. The apparatus as recited in claim 49, wherein the power source comprises a battery, a solar panel or a combination.

51. The apparatus as recited in claim 32, further comprising a display electrically connected or wirelessly connected to the processor and the camera.

52. The apparatus as recited in claim 51, wherein the display comprises a computer, a display screen, a lens, a pair of glasses, a wrist device, a handheld device, a phone, a personal data assistant, a tablet or a combination thereof.

53. The apparatus as recited in claim 32, wherein the processor provides an output to a remote device.

54. The apparatus as recited in claim 32, further comprising a structure, frame or enclosure rigidly connected to the mobile global navigation satellite system receiver and the camera.

55. The apparatus as recited in claim 32, wherein the mobile global navigation satellite system receiver, the camera and the processor are integrated together into a single device.

56. The apparatus as recited in claim 32, wherein the processor provides at least centimeter-level position and degree-level attitude accuracy in open outdoor locations.

57. The apparatus as recited in claim 32, wherein the apparatus transitions indoors and maintains highly-accurate global pose for a limited distance of travel without global navigation satellite system availability.

58. The apparatus as recited in claim 32, wherein the processor operates in a post-processing mode or a real-time mode.

59. The apparatus as recited in claim 32, wherein the apparatus comprises a navigation device, an augmented reality device, a 3-Dimensional rendering device or a combination thereof.

60. A computerized method for determining an absolute position and an absolute attitude of an apparatus comprising the steps of:

providing the apparatus comprising a first global navigation satellite system antenna, a mobile global navigation satellite system receiver connected to the first global navigation satellite system antenna, an interface, a camera, and a processor communicably coupled to the mobile global navigation satellite system receiver, the interface and the camera;

receiving a first set of carrier-phase measurements produced by the mobile global navigation satellite system receiver from a global navigation satellite system;

receiving a second set of carrier-phase measurements from the interface based on a second global navigation satellite system antenna at a known location receiving an image from the camera; and

determining the absolute position and the absolute attitude of the apparatus using the processor based solely from three or more sets of data and a rough estimate of the absolute position of the apparatus without any prior association of visual features with known coordinates, each set of data comprises the image, the first set of carrier-phase measurements and the second set of carrier-phase measurements.

61. The method as recited in claim 60, wherein the processor also uses a prior map of visual features to determine the absolute position and the absolute attitude of the apparatus.

62. The method as recited in claim 60, wherein the rough estimate of the absolute position of the apparatus is obtained using a first set of pseudorange measurements from the mobile global navigation satellite system receiver in each set of data.

63. The method as recited in claim 62, wherein each set of data further comprises a second set of pseudorange measurements from the second global navigation satellite system antenna.

64. The method as recited in claim 60, wherein the rough estimate of the absolute position of the apparatus is obtained using a prior map of visual features, a set of coordinates entered by a user when the apparatus is at a known location, a radio frequency finger-printing, or a cell phone triangulation.

65. The method as recited in claim 60, wherein the first set and second set of carrier-phase measurements are from two or more global navigation satellite systems.

66. The method as recited in claim 60, wherein the first set and second set of carrier-phase measurements are from signals at two or more different frequencies.

67. The method as recited in claim 60, wherein the processor provides an output to a remote device.

68. The method as recited in claim 60, wherein the processor provides at least centimeter-level position and degree-level attitude accuracy in open outdoor locations.

69. The method as recited in claim 60, wherein the processor operates in a post-processing mode or a real-time mode.

70. The method as recited in claim 60, wherein the apparatus comprises a navigation device, an augmented reality device, a 3-Dimensional rendering device or a combination thereof.

71. A computerized method for determining an absolute position and an attitude of an apparatus comprising the steps of:

providing the apparatus comprising a global navigation satellite system antenna, a mobile global navigation satellite system receiver connected to the global navigation satellite system antenna, a camera, and a processor communicably coupled to the mobile global navigation satellite system receiver and the camera;

receiving a set of carrier-phase measurements produced by the mobile global navigation satellite system receiver from a global navigation satellite system with signals at multiple frequencies;

receiving an image from the camera; and

determining the absolute position and the attitude using the processor based solely from three or more sets of data, a rough estimate of the absolute position of the apparatus and a precise orbit and clock data for the global navigation satellite system without any prior association of visual features with known coordinates, each set of data comprises the image, and the set of carrier-phase measurements.

72. The method as recited in claim 71, wherein the processor also uses a prior map of visual features to determine the absolute position and the absolute attitude of the apparatus.

73. The method as recited in claim 71, wherein the rough estimate of the absolute position of the apparatus is obtained using a first set of pseudorange measurements from the mobile global navigation satellite system receiver in each set of data.

74. The method as recited in claim 71, wherein the rough estimate of the absolute position of the apparatus is obtained using a prior map of visual features, a set of coordinates entered by a user when the apparatus is at a known location, a radio frequency finger-printing, or a cell phone triangulation.

75. The method as recited in claim 71, wherein the precise orbit and clock data provide decimeter-level or better positioning and nano-second or better timing for the satellites.

76. The method as recited in claim 71, wherein the processor provides an output to a remote device.

77. The method as recited in claim 71, wherein the processor provides at least centimeter-level position and degree-level attitude accuracy in open outdoor locations.

78. The method as recited in claim 71, wherein the processor operates in a post-processing mode or a real-time mode.

79. The method as recited in claim 71, wherein the apparatus comprises a navigation device, an augmented reality device, a 3-Dimensional rendering device or a combination thereof.