Satellite navigation controller

• US 7,392,134 B2
• Filed: 03/31/2005
• Issued: 06/24/2008
• Est. Priority Date: 04/05/2004
• Status: Active Grant

• Current Assignee: DENSO Corporation
• Original Assignee: DENSO Corporation
• Inventors: Tauchi, Nobutaka, Tanino, Hideki, Mutoh, Katsuhiko
• Primary Examiner(s): Keith; Jack W.
• Assistant Examiner(s): Nguyen; Chuong P
• Application Number:
  US11/093,994
• Publication Number:
  US 20050222768A1
• Time in Patent Office: 1,181 Days
• Field of Search: 701/23, 701207-211, 701213-217, 701/1, 701/200, 340/988, 340/995.1, 342/357.06, 34235712-35715, 342/357.02, 342/357.08
• US Class Current: 701/213
• CPC Class Codes: G01C 21/26 specially adapted for navigation in a road network
• CPC Class Codes: G01S 19/32 Multimode operation in a single same satellite system, e.g. GPS L1/L2
• CPC Class Codes: G01S 19/33 Multimode operation in different systems which transmit time stamped messages, e.g. GPS/GLONASS
• CPC Class Codes: G01S 19/34 Power consumption
• CPC Class Codes: G01S 19/396 Determining accuracy or reliability of position or pseudorange measurements
• CPC Class Codes: G01S 19/49 whereby the further system is an inertial position system, e.g. loosely-coupled

Abstract

A navigation device changes a position determination accuracy of a receiver for satellite navigation to a higher accuracy in the following cases: when the subject vehicle approaches a destination, the subject vehicle runs on a road not described in map information, when the subject vehicle approaches an intersection at which the road is branched at a narrow angle within a predetermined distance, when the subject vehicle is running on a narrow street, when the subject vehicle is running on one of adjacent parallel roads, when self-contained sensors are calibrated, and other like occasions. In the other cases, the navigation device changes the position determination accuracy of the receiver to a low accuracy. When the receiver is caused to execute low-accuracy position determination, power supply to receiver'"'"'s operation required only for high-accuracy position determination is prohibited.

Claims

1. A satellite navigation controller tat controls a receiver for satellite navigation, wherein the receiver is able to receive signals having individual chip rates from satellites to thereby execute position determination with at least two different accuracies including a higher accuracy and a lower accuracy, the chip rate being a speed of spreading code for subjecting the signal to spreading modulation and de-spreading demodulation, the satellite navigation controller comprising:

a chip rate switching unit configured to switch between at least two chip rates including a higher chip rate and a lower chip rate, each chip rate being corresponded to by one of the at least two accuracies, the higher chip rate corresponding to the higher accuracy while needing a processing load and power consumption higher than the lower chip rate;

a determining unit configured to determine a first accuracy, which is one of the at least two accuracies, the first accuracy at which the receiver should be caused to execute position determination; and

a controlling unit configured to cause the chip rate switching unit to switch to a first chip rate of the at least two chip rates, the first chip rate being corresponded to by the first accuracy, to thereby allow the receiver to execute position determination with the first accuracy and prohibit decoding signals from the satellites for executing position determination with a second accuracy, which is different than the first accuracy of the at least two accuracies.

2. The satellite navigation controller of claim 1,

wherein the controlling unit is further configured to interrupt power supply to parts which receive and decode signals from the satellites for executing position determination at the second accuracy to thereby prohibit the receiver from executing position determination with the second accuracy.

3. The satellite navigation controller of claim 1,

wherein the satellite navigation controller is mounted in a vehicle when used, and

wherein the determining unit is further configured to calibrate a position of the vehicle computed by a self-contained navigation, for determining the first accuracy of the at least two accuracies at which the receiver should be caused to execute position determination, wherein the first accuracy determined is not lower than a predetermined accuracy.

4. The satellite navigation controller of claim 1,

wherein the satellite navigation controller is mounted in a vehicle when used, and

wherein the determining unit is further configured for, based on a fact that the vehicle is in a position close to an intersection at which a road is branched at a narrow angle, for displaying a positional relation between the road and the vehicle, determining the first accuracy with which the receiver should be caused to execute position determination, wherein the first accuracy determined is not lower than a predetermined accuracy.

5. The satellite navigation controller of claim 1,

wherein the satellite navigation controller is mounted in a vehicle when used, and

wherein the determining unit is further configured for, based on a fact that the vehicle is running on a narrow street, for displaying a positional relation between the narrow street and the vehicle, determining the first accuracy with which the receiver should be caused to execute position determination, wherein the first accuracy determined is not lower than a predetermined accuracy.

6. The satellite navigation controller of claim 1,

wherein the satellite navigation controller is mounted in a vehicle when used, and

wherein the determining unit is further configured for, based on a fact that the vehicle is running on any adjacent parallel road of a plurality of adjacent parallel roads, for displaying a positional relation between the any adjacent parallel road and the vehicle, determining the first accuracy with which the receiver should be caused to execute position determination, wherein the first accuracy determined is not lower than a predetermined accuracy.

7. The satellite navigation controller of claim 1,

wherein the satellite navigation control let is mounted in a vehicle when used, and

wherein the determining unit is further configured for, based on a fact that a key switch for the vehicle is in one of an ACC position and an off position, determining the higher accuracy as the first accuracy with which the receiver should be caused to execute position determination.

8. The satellite navigation controller of claim 1,

wherein, the satellite navigation controller is mounted in a vehicle when used, and

wherein, the determining unit is further configured so that when it determines the first accuracy with which the receiver should be caused to execute position determination, wherein the first accuracy determined is not lower than a predetermined accuracy, a maximum extraction range for map matching is narrowed.

9. The satellite navigation controller of claim 1, further comprising:

a display unit configured to display a position of a vehicle where the satellite navigation controller is mounted,

wherein the determining unit is further configured for, based on a fact that the display unit does not display the position of the vehicle on a map, determining the lower accuracy as the first accuracy with which the receiver should be caused to execute position determination.

10. The satellite navigation controller of claim 1, mounted in a vehicle when used and further comprising:

a display unit configured to display a position of the vehicle on a map; and

a detecting unit configured to detect whether the satellite navigation controller is connected to equipment in the vehicle or not,

wherein the determining unit is further configured for, based on a fact that the detecting unit detects that the satellite navigation controller is not connected, for causing the display unit to display the position of the vehicle on a map, determining the lower accuracy as the first accuracy with which the receiver should be caused to execute position determination when the vehicle stop.

11. The satellite navigation controller of claim 1,

wherein the satellite navigation control is mounted in a vehicle when used,

wherein the determining unit is further configured for, based on a fact that the vehicle approaches a preset destination within a predetermined distance, for computing a positional relation between the destination and the vehicle, determining the first accuracy with which the receiver should be caused to execute position wherein the first accuracy determined is not lower than a predetermined accuracy.

12. The satellite navigation controller of claim 1,

wherein the satellite navigation controller is mounted in a vehicle when used,

wherein the determining unit is further configured for, based on a fact that the vehicle is running on a certain road that is not described in map information, for generating position information of the certain road, determining the first accuracy with which the receiver should be caused to execute position determination, wherein the first accuracy determined is not lower than a predetermined accuracy.

13. The satellite navigation controller of claim 1,

wherein the satellite navigation controller is mounted in a vehicle when used,

wherein the determining unit is further configured for, based on a fact that the vehicle is running on a given road described on a map based on position determination with an accuracy that is not higher than a predetermined accuracy, for generating position information of the given road, determining the first accuracy with which the receiver is caused to execute position determination, wherein the first accuracy determined is not lower than the predetermined accuracy.

14. The satellite navigation controller of claim 1, wherein the higher accuracy corresponds to a measurement error of not more than 10 centimeters, wherein the lower accuracy corresponds to a measurement error of not less than 10 meters.

15. The satellite navigation controller of claim 1, wherein the higher accuracy is obtained using real time kinematic positioning.

16. A positioning system used in a navigation device for a vehicle, the system comprising:

a receiver for satellite navigation to receive signals having individual chip rates from satellites to thereby execute position determination, the chip rate being a speed of spreading code for subjecting the signal to spreading modulation and de-spreading demodulation, the receiver including;

a chip rate switching unit configured to facilitate switching at least two chip rates therebetween, each chip rate being corresponded to by one of the at least two accuracies;

a first positioning unit configured to facilitate determining a position of the vehicle with a first chip rate corresponded to by a first accuracy having a first measurement error, the second chip rate needing a processing load and power consumption higher than the first chip rate; and

a second positioning unit configured to facilitate determining a position of the vehicle with a second chip rate corresponded to by a second accuracy having a second measurement error lower than the first measurement error; and

a satellite navigation controller configured to control the receiver based on signals from satellites for satellite navigation, the satellite navigation controller including;

a chip rate switching unit configured to switch the first chip rate and the second chip rate therebetween;

a determining unit configured to determine one of the two accuracies for executing position determination; and

a controlling unit configured to cause the chip rate switching unit to switch to one of the two chip rates corresponded to by the one of the two accuracies determined, to thereby allow the receiver to execute position determination with the one of the two accuracies determined and prohibit decoding signals from the satellites for executing position determination with, of the two accuracies, another accuracy different from the one of the two accuracies determined.

17. The positioning system of claim 16, wherein the first measurement error is not less than 10 meters, wherein the second measurement error is not more than 10 centimeters.