SYSTEM AND METHOD FOR DETECTING AMBIGUITIES IN SATELLITE SIGNALS FOR GPS TRACKING OF VESSELS

• US 20150153459A1
• Filed: 11/15/2012
• Published: 06/04/2015
• Est. Priority Date: 05/11/2012
• Status: Active Grant

• Current Assignee: Korea Institute Of Ocean Science & Technology
• Original Assignee: Korea Institute Of Ocean Science & Technology
• Inventors: Cho, Deuk Jae, Shim, Woo-Seong
• Granted Patent: US 9,638,806 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01S 19/40 Correcting position, velocity or attitude

Abstract

The present invention relates to a system for detecting ambiguities in a satellite signal for the GPS tracking of vessels, which includes: a GNSS receiving unit obtaining a vessel position using a plurality of satellites; a vessel position calculating unit calculating a second vessel position from a first vessel position after a specific amount of time elapses using dead-reckoning; a distance calculating unit calculating prediction distances between each of the satellites and the vessel and an error monitoring unit comparing the calculated prediction distances between the satellites and the vessel, and pseudoranges between the satellites and the GNSS receiving unit at the second vessel position, and monitoring for the occurrence of errors at the satellites on the basis of the existence of an increase in errors at each of the satellites.

Claims

1. A system for detecting ambiguities in satellite signals for vessel positioning, comprising:

a Global Navigation Satellite System (GNSS) reception unit for acquiring a position of a vessel using a plurality of satellites;

a vessel position calculation unit for calculating a second vessel position of the vessel after a specific time (t) has elapsed from a first vessel position of the vessel, using dead-reckoning;

a distance calculation unit for calculating predicted distances between the respective satellites and the vessel, using position values of the respective satellites at the second vessel position, calculated using ephemeris information of the satellites, and a position value of the second vessel position; and

an error monitoring unit for individually comparing the predicted distances between the respective satellites and the vessel calculated by the distance calculation unit, with pseudoranges between the respective satellites and the GNSS reception unit at the second vessel position, and then monitoring whether errors have occurred in the satellites depending on whether an error in each satellite has increased.

2. The system of claim 1, wherein the vessel position calculation unit calculates the second vessel position using a bow azimuth angle and a ground speed of the vessel from the first vessel position.

3. The system of claim 2, wherein the vessel comprises:

a direction sensor for measuring the bow azimuth angle; and

a speed sensor for measuring the ground speed.

4. The system of claim 2, wherein the first vessel position is a GNSS position previously acquired using the position values of the respective satellites when the GNSS reception unit is located at a point corresponding to the first vessel position.

5. The system of claim 1, wherein the position values of the satellites at the second vessel position are acquired by the GNSS reception unit calculating distance values of respective satellites that have moved from the first vessel position during the specific time (t) using the ephemeris information of the satellites.

6. The system of claim 1, wherein the pseudoranges are values calculated by the GNSS reception unit using signal measurement values.

7. A method for detecting ambiguities in satellite signals for vessel positioning, comprising:

acquiring a first vessel position of a vessel using a plurality of satellites;

calculating a second vessel position of the vessel after a specific time (t) has elapsed from the first vessel position, using dead-reckoning;

calculating predicted distances between the respective satellites and the vessel at the second vessel position using ephemeris information of the satellites; and

monitoring whether errors have occurred in satellite signals depending on whether an error in each satellite has increased by individually comparing the predicted distances between the respective satellites and the vessel with pseudoranges between the respective satellites and a Global Navigation Satellite System (GNSS) reception unit at the second vessel position.

8. The method of claim 7, wherein acquiring the first vessel position is configured to acquire the first vessel position using the following equation:

VP_a(T)=TA(ρ

_1a,ρ

_2a,ρ

_3a,ρ

_4a)

where VP_a(T) denotes the position of the vessel at point ‘

a’

, T denotes a time axis, TA denotes an abbreviated form of triangulation, meaning a function of receiving four pseudorange parameters and obtaining the position of the vessel from known satellite positions, and (ρ

_1a, ρ

_2a, ρ

_3a, ρ

_4a) denotes pseudoranges from point ‘

a’

to the respective satellites.

9. The method of claim 7, wherein calculating the second vessel position is configured to calculate the second vessel position using the following equation:

VP_DR(T+t)=DR{VP_a(T),HDG_a,SOG_a}

where VP_DR(T+t) denotes the position of the vessel at point ‘

b’

to which the vessel has moved for the time t, via dead-reckoning, T denotes a time axis, DR denotes an abbreviated form of dead-reckoning, meaning a function of calculating the position of the vessel after time t has elapsed, using input parameter values, VP_a(T) denotes the position of the vessel at point ‘

a’

, HDG_a denotes a bow azimuth angle at point ‘

a’

, and SOG_a denotes a ground speed at point ‘

a’

.

10. The method of claim 7, wherein calculating the distance comprises:

a satellite position value calculation operation of calculating position values of respective satellites at the second vessel position using the ephemeris information of the satellites; and

a predicted distance calculation operation of calculating predicted distances between the respective satellites and the vessel using the position values of the respective satellites at the second vessel position and a position value of the second vessel position.

11. The method of claim 10, wherein the predicted distance calculation operation is configured to calculate the predicted distances using the following equation:

Cal<sub>ρ

1,2,3,4b</sub>=√

{square root over (|VP_DR(T+t)−

S_1,2,3,4b|²)}

where Cal<sub>ρ

1,2,3,4b</sub> denotes distances from the vessel to the respective satellites at point ‘

b’

, VP_DR(T+t) denotes the position of the vessel at point ‘

b’

to which the vessel has moved for the time t, using dead-reckoning, T denotes a time axis, and S_1,2,3,4b denotes the calculated position values of the respective satellites at point ‘

b’

.

12. The method of claim 7, wherein monitoring whether errors have occurred comprises:

a pseudorange acquisition operation of acquiring pseudoranges between the respective satellites and the vessel at the second vessel position;

a distance comparison operation of individually comparing the predicted distances between the respective satellites and the vessel with the pseudoranges; and

an error monitoring operation of monitoring whether errors have occurred in satellite signals depending on whether an error in each satellite has increased.

13. The method of claim 12, wherein the pseudorange acquisition operation is configured to acquire the pseudoranges using the following equation that represents a vessel position (VP_b(T+t)) corresponding to the second vessel position by a formula of distances between the vessel and the satellites:

VP_b(T+t)=TA(ρ

_1b,ρ

_2b,ρ

_3b,ρ

_4b)

where VP_b(T+t) denotes the position of the vessel at point ‘

b’

, T denotes a time axis, TA denotes an abbreviated form of triangulation, meaning a function of receiving four pseudorange parameters and obtaining the position of the vessel from known satellite positions, and (ρ

_1b, ρ

_2b, ρ

_3b, ρ

_4b) denotes pseudoranges from point ‘

b’

to the respective satellites.