METHOD AND APPARATUS FOR POSITIONING

• US 20120188120A1
• Filed: 04/08/2011
• Published: 07/26/2012
• Est. Priority Date: 01/26/2011
• Status: Abandoned Application

• Current Assignee: Industrial Technology Research Institute
• Original Assignee: Industrial Technology Research Institute
• Inventors: Kiang, Jean-Fu, Tsai, Shuan-Chi
• Application Number:
  US13/082,424
• Publication Number:
  US 20120188120A1
• Time in Patent Office: Days
• US Class Current: 342/357.24
• CPC Class Codes: G01S 19/41 Differential correction, e.g. DGPS [differential GPS]

Abstract

A positioning method and a positioning apparatus are provided. In this positioning method, a differential global positioning system is used to calculate a double difference of satellite distance in connection with a reference station and a receiver station. A baseline vector pointing from the reference station to the receiver station is calculated according to the double difference of satellite distance and the cosine law. The baseline vector and the position of the reference station are used to calculate the position of the receiver station. Correction coefficients are obtained according to the position of the reference station, the position of the receiver station, and the current time. The position of the receiver station is corrected according to the correction coefficients and the length of the baseline vector.

Claims

1. A positioning method, comprising:

using a differential global positioning system to calculate a double difference of a satellite distance in connection with a reference station and a receiver station;

calculating a baseline vector pointing from the reference station to the receiver station according to the double difference of satellite distance and cosine law;

using the baseline vector and a position of the reference station to calculate a position of the receiver station;

obtaining a plurality of correction coefficients according to the position of the reference station, the position of the receiver station, and a current time; and

correcting the position of the receiver station according to the correction coefficients and a length of the baseline vector.

2. The positioning method according to claim 1, wherein the step of calculating the double difference of satellite distance comprises:

using the differential global positioning system to calculate a double difference of pseudo-range and a double difference of carrier phase in connection with the reference station and the receiver station;

calculating a double difference of integer ambiguity in the double difference of carrier phase according to the double difference of pseudo-range, the double difference of carrier phase, and a plurality of transmitting signal frequencies of the differential global positioning system; and

calculating the double difference of satellite distance according to the double difference of carrier phase and the double difference of integer ambiguity.

3. The positioning method according to claim 1, wherein the double difference of satellite distance is calculated from four distances between the reference station/the receiver station and two satellites of the differential global positioning system according to a first equation, and the step of calculating the baseline vector comprises:

with respect to two triangles defined by the reference station, the receiver station and each of the two satellites, applying the cosine law to the four distances respectively and applying resultant equations into the first equation to obtain a second equation; and

calculating the baseline vector according to the second equation.

4. The positioning method according to claim 3, wherein the second equation comprises a primary term and a secondary term, and the step of calculating the baseline vector according to the second equation comprises:

setting the secondary term to be zero and calculating an estimate of the baseline vector according to the second equation;

applying the estimate into the secondary term, and calculating a next estimate of the baseline vector according to the second equation; and

repeating the previous step until the estimate satisfies a convergent criterion, and then taking the estimate satisfying the convergent criterion as the baseline vector.

5. The positioning method according to claim 1, wherein the step of obtaining the correction coefficients comprises:

using the current time, a latitude and a longitude of the receiver station, and an azimuth angle between the baseline vector and a north direction as indices to obtain the correction coefficients from a lookup table.

6. The positioning method according to claim 1, wherein the number of the correction coefficients is three and the three correction coefficients are respectively corresponding to three coordinate axes of a position at which the receiver station is located.

7. The positioning method according to claim 6, wherein the step of correcting the position of the receiver station comprises:

using each of the correction coefficients and a cube of the length of the baseline vector to calculate a correction amount corresponding to each of the correction coefficients; and

using each of the correction amounts to correct a corresponding coordinate of the position of the receiver station.

15. A positioning apparatus employing the differential global positioning system according to claim 1, in which the positioning apparatus is the receiver station, the positioning apparatus comprising:

a balloon;

a payload disposed below the balloon and comprising;

a receiver receiving satellite signals of the differential global positioning system or receiving the satellite signals as well as signals from the reference station;

a processor calculating based on the signals received by the receiver; and

a transmitter wirelessly transmitting a calculation result of the processor, wherein the processor executes the positioning method according to claim 1, or a monitoring station executes the positioning method, or the processor executes some steps of the positioning method and the monitoring station executes the remaining steps of the positioning method.

8. A positioning method, comprising:

using a differential global positioning system to calculate a double difference of satellite distance in connection with a reference station and a receiver station;

calculating a baseline vector pointing from the reference station to the receiver station according to the double difference of satellite distance and cosine law; and

using the baseline vector and a position of the reference station to calculate a position of the receiver station.

9. The positioning method according to claim 8, wherein the double difference of satellite distance is calculated from four distances between the reference station/the receiver station and two satellites of the differential global positioning system according to a first equation, and the step of calculating the baseline vector comprises:

with respect to two triangles defined by the reference station, the receiver station and each of the two satellites, applying the cosine law to the four distances respectively and applying resultant equations into the first equation to obtain a second equation; and

calculating the baseline vector according to the second equation.

10. The positioning method according to claim 9, wherein the second equation comprises a primary term and a secondary term, and the step of calculating the baseline vector according to the second equation comprises:

setting the secondary term to be zero and calculating an estimate of the baseline vector according to the second equation;

applying the estimate into the secondary term, and calculating a next estimate of the baseline vector according to the second equation; and

repeating the previous step until the estimate satisfies a convergent criterion, and then taking the estimate satisfying the convergent criterion as the baseline vector.

16. A positioning apparatus employing the differential global positioning system according to claim 8, in which the positioning apparatus is the receiver station, the positioning apparatus comprising:

a balloon;

a payload disposed below the balloon and comprising;

a receiver receiving satellite signals of the differential global positioning system or receiving the satellite signals as well as signals from the reference station;

a processor calculating according to the signals received by the receiver; and

a transmitter wirelessly transmitting a calculation result of the processor, wherein the processor executes the positioning method according to claim 8, or a monitoring station executes the positioning method, or the processor executes some steps of the positioning method and the monitoring station executes the remaining steps of the positioning method.

11. A positioning method, comprising:

using a differential global positioning system to calculate a baseline vector pointing from a reference station to a receiver station;

using the baseline vector and a position of the reference station to calculate a position of the receiver station;

obtaining a plurality of correction coefficients according to the position of the reference station, the position of the receiver station, and a current time; and

correcting the position of the receiver station according to the correction coefficients and a length of the baseline vector.

12. The positioning method according to claim 11, wherein the step of obtaining the correction coefficients comprises:

using the current time, a latitude and a longitude of the receiver station, and an azimuth angle between the baseline vector and a north direction as indices to obtain the correction coefficients from a lookup table.

13. The positioning method according to claim 11, wherein the number of the correction coefficients is three and the three correction coefficients are respectively corresponding to three coordinate axes of a position at which the receiver station is located.

14. The positioning method according to claim 13, wherein the step of correcting the position of the receiver station comprises:

using each of the correction coefficients and a cube of the length of the baseline vector to calculate a correction amount corresponding to each of the correction coefficients; and

using each of the correction amounts to correct a corresponding coordinate of the position of the receiver station.

17. A positioning apparatus employing the differential global positioning system according to claim 11, in which the positioning apparatus is the receiver station, the positioning apparatus comprising:

a balloon;

a payload disposed below the balloon and comprising;

a receiver receiving satellite signals of the differential global positioning system or receiving the satellite signals as well as signals from the reference station;

a processor calculating according to the signals received by the receiver; and

a transmitter wirelessly transmitting a calculation result of the processor, wherein the processor executes the positioning method according to claim 11, or a monitoring station executes the positioning method, or the processor executes some steps of the positioning method and the monitoring station executes the remaining steps of the positioning method.