GUIDING POSITIONING METHOD, POSITIONING DEVICE AND COMPUTER PROGRAM PRODUCT

• US 20100131200A1
• Filed: 04/18/2008
• Published: 05/27/2010
• Est. Priority Date: 04/24/2007
• Status: Abandoned Application

• Current Assignee: Tracker Software Oy
• Original Assignee: Tracker Oy (Open Air Group AB)
• Inventors: Lohi, Hannu
• Application Number:
  US12/594,603
• Publication Number:
  US 20100131200A1
• Time in Patent Office: Days
• US Class Current: 701/213
• CPC Class Codes: G01C 17/00 Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes using gyroscopic effect G01C19/00
• CPC Class Codes: G01S 19/53 Determining attitude

Abstract

A method in which location information and bearing of the user of a positioning device are determined based on signals sent by positioning satellites. The user is instructed to act in a suitable way when the bearing is being determined. The method further determines a confidence parameter that indicates the reliability of the communicated bearing and is communicated to the user simultaneously with the bearing. The confidence parameter enables the user to estimate whether or not the communicated bearing information can be trusted. The confidence parameter can be determined from the number of positioning satellites connected to the satellite receiver and the determined traveling speed of the user of the positioning device, or from the dilution of precision provided by the GPS system. The confidence parameter gets a value “good”, when an equation is true, and a value “bad”, when the equation is false.

Claims

1. A guiding positioning method, in which with a positioning device, that includes a satellite receiver, a positioning signal from several positioning satellites is received, a bearing of the user of the positioning device is determined using the received positioning signals, and the defined bearing is communicated to the user of the positioning device, characterized in that in the method a confidence parameter representing the reliability of the bearing is determined based on the received positioning signals, which confidence parameter is communicated to the user of the positioning device.

2. The method according to claim 1, characterized in that the confidence parameter is communicated to the user of the positioning device simultaneously with the bearing.

3. The method according to claim 1, characterized in that in the method the number of positioning satellites connected to the satellite receiver and the travelling speed of the user of the positioning device are determined, and the confidence parameter of the positioning signal is determined based on this information.

4. The method according to claim 3, characterized in that the confidence parameter is determined with the equation:

v·

(nmb−

2)≧

9, 

 

(1)

where

v=determined travelling speed of the user, km/h

nmb=number of satellites connected to the satellite receiver,

whereby the confidence parameter gets a value “

good”

when equation (1) is true, and a value “

bad”

when equation (1) is false.

5. The method according to claim 1, characterized in that the positioning method is the GPS positioning method and the confidence parameter is determined using the dilution of precision defined in that method.

6. The method according to claim 1, characterized in that in the method satellite reception is first ascertained.

7. The method according to claim 6, characterized in that the user of the positioning device is asked to stop moving if the satellite reception is not sufficient.

8. A positioning device that comprises an electronic terminal, having a display, a memory, a processor, a satellite receiver for receiving positioning signals, and means for determining a bearing of the user of the positioning device, characterized in that the device further comprises means for determining, based on the received positioning signals, a confidence parameter that represents the reliability of the determined bearing, and for communicating the confidence parameter to the user.

9. The positioning device of claim 8, characterized in that the confidence parameter is arranged to be communicated to the user simultaneously with the bearing.

10. The positioning device according to claim 8, characterized in that the display of the terminal includes a data field for communicating the confidence parameter value to the user using text, symbols, and/or colours.

11. The positioning device according to claim 8, characterized in that the said means for determining the confidence parameter comprise a software program loaded in the memory of the terminal.

12. A computer program product that comprises computer program means, stored on computer readable medium, for determining a bearing of the user of a positioning device using positioning signals sent from positioning satellites, and for communicating the bearing to the user of the positioning device, characterized in that the computer program product further comprises computer program means for determining, based on the received positioning signals, a confidence parameter that represents the reliability of the determined bearing, and for communicating the confidence parameter to the user.

13. The computer program product of claim 12, characterized in that the said computer program means are configured to communicate the confidence parameter to the user simultaneously with the bearing.

14. The computer program product of claim 12, characterized in that the said computer program means are configured to determine the number of positioning satellites connected to the satellite receiver and the travelling speed of the user of the positioning device, and to determine the confidence parameter based on this information.

15. The computer program product of claim 14, characterized in that the said computer program means are configured to determine the confidence parameter using the following equation:

v·

(nmb−

2)≧

9, 

 

(1)

where

v=determined travelling speed of the user, km/h

nmb=number of satellites connected to the satellite receiver,

whereby the confidence parameter gets a value “

good”

when equation (1) is true, and a value “

bad”

when equation (1) is false.

16. The computer program product of claim 12, characterized in that the said computer program means are configured to determine the confidence parameter using a dilution of precision determined in the GPS positioning method.

17. The computer program product of claim 12, characterized in that it further comprises computer program means for ascertaining satellite reception.

18. The computer program means of claim 17, characterized in that the said computer program means are configured to provide a stop request to the user if the satellite reception is not sufficient.