GNSS line bias measurement system and method

• US 7,489,270 B2
• Filed: 04/15/2005
• Issued: 02/10/2009
• Est. Priority Date: 04/15/2005
• Status: Active Grant

• Current Assignee: Novariant Incorporated (Kubota Corporation)
• Original Assignee: Novariant Incorporated (Kubota Corporation)
• Inventors: Zimmerman, Kurt, Cobb, Henry Stewart, Montgomery, Paul Yalden, Lawrence, David Gary
• Primary Examiner(s): Tarcza; Thomas H
• Assistant Examiner(s): LIU, HARRY K
• Application Number:
  US11/106,962
• Publication Number:
  US 20060244656A1
• Time in Patent Office: 1,397 Days
• Field of Search: 342/417, 342/411, 342/442, 342/357.06, 701/215
• US Class Current: 342/357.29
• CPC Class Codes: G01S 19/04 providing carrier phase data
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method

Abstract

A number of solutions for deriving the line bias are disclosed. Some of these solutions utilize signal processing and judicious selection of the frequency plan used in the position detection systems to either enable the derivation of the line bias, or make the measurements insensitive to line bias. In other examples, the present invention utilizes measurement schemes for deriving the line bias and enabling a position detection system to process line bias information in order to find a position solution.

Claims

1. A method for determining the relative position of a first antenna and a second antenna, the first antenna being connected to a receiver via a first communication path and the second antenna connected to the receiver via a second communication path, the method comprising:

a. generating differential carrier phase measurements between the first and second antennas by

i. transmitting signal information bi-directionally between the receiver and at least one of the first and second antennas over the first communication path and/or the second communication path;

ii. measuring phases of at least some of said signal information for the first and second antennas; and

iii. using differences between the phases for the second antenna and phases for the first antenna to correct for differences in transmission delay over the first communication path and the second communication path;

b. calculating the relative position of the first and second antennas from the differential carrier phase measurements generated in step a.

2. The method of claim 1, wherein the first and second antennas are configured to receive GNSS signals.

3. The method of claim 1, wherein the step of transmitting signal information comprises:

transmitting a clock signal from the receiver to the first and second antennas; and

transmitting an intermediate frequency from the antennas to the receiver.

4. The method of claim 1, wherein the step of transmitting signal information comprises:

transmitting a clock signal from the receiver to the first and second antennas; and

transmitting a down-converted GNSS signal from the antennas to the receiver.

5. The method of claim 4, wherein the step of transmitting the down-converted GNSS signal comprises down-converting a received GNSS signal to substantially half the frequency at which it was received at the first and second antennas.

6. The method of claim 1, wherein the step of transmitting signal information farther comprises transmitting a first compensation signal from the first antenna to the receiver and a second compensation signal from the second antenna to the receiver.

7. The method of claim 6 wherein the first compensation signal and the second compensation signal are a harmonic of the clock signal.

8. A system for determining the relative position of a first antenna and a second antenna, comprising:

a receiver;

a first communication path connecting the first antenna to the receiver; and

a second communication path connecting the second antenna to the receiver;

wherein the receiver generates differential carrier phase measurements between the first and second antennas using signal information transmitted bi-directionally between the receiver and at least one of the first and second antennas over the first communication path and the second communication path and generating a difference between the phases for the second antenna relative to the phases for the first antenna to correct for differences in transmission delay over the first communication path and the second communications path and calculates the relative position of the first and second antennas from the differential carrier phase measurements.

9. The system of claim 8, wherein the first and second antennas are configured to receive GNSS signals.

10. The system of claim 8, wherein the receiver transmits a clock signal to the first and second antennas and receives an intermediate frequency from the antennas.

11. The system of claim 8, wherein the receiver transmits a clock signal to the first and second antennas and receives a down-converted GNSS signal from the antennas.

12. The system of claim 11, wherein the down-converted GNSS signal is at substantially half the frequency at which it was received at the first and second antennas.

13. The system of claim 8, wherein the receiver receives a first compensation signal from the first antenna and a second compensation signal from the second antenna.

14. The system of claim 13 wherein the first compensation signal and the second compensation signal are a harmonic of a clock signal.