Ultra short baseline GNSS receiver

• US 8,638,257 B2
• Filed: 10/15/2009
• Issued: 01/28/2014
• Est. Priority Date: 10/15/2009
• Status: Active Grant

• Current Assignee: Novatel Incorporated (Hexagon AB)
• Original Assignee: Novatel Incorporated (Hexagon AB)
• Inventors: Fenton, Patrick C.
• Primary Examiner(s): GALT, CASSI J
• Application Number:
  US12/579,460
• Publication Number:
  US 20110090114A1
• Time in Patent Office: 1,566 Days
• Field of Search: 342/357.36, 342/357.37
• US Class Current: 342/357.37
• CPC Class Codes: G01S 19/54 using carrier phase measurements; using long or short baseline interferometry

Abstract

A GNSS receiver utilizes an antenna structure that two or more antennas that are spaced apart from their neighboring antennas by less than 1 wavelength of a GNSS satellite carrier signal of interest. The receiver calculates the orientation of the antennas directly from differences in the carrier phase angles measured at the two antennas, without resolving integer carrier cycle ambiguity.

Claims

1. A GNSS receiver comprising:

an antenna structure consisting of two or more antennas with each antenna spaced apart from neighboring antennas by less than one wavelength of a carrier signal in GNSS satellite signals;

a phase map that contains carrier phase difference error values associated with angles of incidence of the GNSS satellite signals at the antenna structure and line biases associated with operation of the GNSS receiver and calculated for respective pairs of antennas based on phase difference values;

one or more processors configured to process the GNSS satellite signals received by the antennas and calculate estimated orientation of the antenna structure directly from differences in carrier phase angle measurements of incoming GNSS carrier signals at the antennas, determine the angles of incidence of the respective GNSS satellite signals based on positions of respective satellites and the estimated orientation of the antenna structure, enter the phase map using the angles of incidence and retrieve associated carrier phase difference error values, and utilize the associated carrier phase difference error values to correct the estimated orientation to produce an updated orientation; and

the one or more processors further configured to re-enter the phase map to calculate a new updated orientation, utilizing updated angles of incidence, until a change in the new updated orientation is less than an error gradient associated with the phase map.

2. The GNSS receiver of claim 1 wherein the one or more processors are configured to calculate the estimated orientation of the antenna structure without resolving an integer carrier cycle ambiguity of the incoming GNSS carrier signals, and perform cycle roll over compensation as needed.

3. The GNSS receiver of claim 2 further including:

one or more inertial sensors that are initialized with the estimated calculated orientation, the sensors providing sensor values to the one or more processors, and

the one or more processors are configured to include the sensor values in calculations that determine direction of movement.

4. The receiver of claim 3 wherein the one or more inertial sensors are gyroscopes.

5. The receiver of claim 4 wherein the one or more processors are configured to utilize the calculated estimated orientation to calibrate the one or more gyroscopes.

6. The receiver of claim 1 wherein the one or more processors are configured to calculate the estimated orientation in two dimensions if the antenna structure includes two antennas and in three dimensions if the antenna structure includes more than two antennas.

7. A method of operating a GNSS receiver comprising:

receiving incoming GNSS signals at two or more antennas on an antenna structure, each antenna being spaced apart from at least one neighboring antenna by an ultra short baseline that is less than one wavelength of a carrier of the GNSS signals,

measuring carrier phase angles of the GNSS signals at the antennas and calculating one or more carrier phase differences directly from the carrier phase angle measurements,

calculating estimated orientation of the antennas from the carrier phase differences,

using the calculated estimated orientation and a position of a satellite to determine angles of incidence of incoming GNSS signals,

using the angles of incidence to enter a phase map or table to retrieve associated carrier phase difference error values that include line biases associated with operation of the GNSS receiver and calculated for respective pairs of antennas based on phase difference values,

correcting the calculated carrier phase differences based on the carrier phase difference error values,

correcting the estimated orientation based on the corrected phase differences to produce an updated orientation, and

re-entering the phase map, utilizing updated angles of incidence, to retrieve the associated carrier phase difference error values to calculate a new updated orientation until a change in the new updated orientation is less than an error gradient associated with the phase map.

8. The method of claim 7 wherein calculating the estimated orientation is performed without resolving integer carrier cycle ambiguity and with roll over compensation as needed.

9. The method of claim 7 further comprising:

collecting carrier phase angle measurement data over a period of time,

batch processing the carrier phase angle measurement data to determine which carrier phase angle measurement data are valid, and

calculating the estimated orientation of the antennas using the valid carrier phase measurement data.

10. The method in claim 7 further comprising:

collecting sets of carrier phase angle measurement data over a period of time, and

computing the estimated orientation of the antenna with each set of collected phase angle measurement data to determine direction.

11. The method of claim 7 further including utilizing the calculated estimated orientation to initialize one or more inertial sensors.

12. The method of claim 11 further including utilizing the estimated calculated orientation to calibrate the inertial sensors.

13. The method of claim 11 further including utilizing the estimated calculated orientation to re-initialize GNSS phase difference tracking processes after signal lock to the GNSS carrier signal is lost and reacquired.

14. The method of claim 7 wherein re-entering the phase map further includes

a) calculating the updated angles of incidence using a latest calculated updated orientation,

b) entering the phase map or table to extract improved estimates of the carrier phase difference error values,

c) using the improved estimates of the phase difference error values to correct the phase difference measurements,

d) calculating the new updated orientation based on the corrected phase difference measurements,

e) repeating steps a through d until the new updated orientation for the iteration is sufficiently close to a previous updated orientation for a previous iteration based on the error gradient of the phase map.

15. The method of claim 7 further including using the estimated orientation calculated for one or more ultra short baselines to initialize the carrier cycle ambiguity resolution of one or more corresponding longer base line pairs of GNSS antennas.

16. The method of claim 15 wherein one endpoint of at least one of the longer base lines is an end point of the corresponding ultra short base line.

17. The method of claim 7 wherein the estimated orientation is determined in two dimensions if the antenna structure includes two antennas and in three dimensions if the antenna structure includes more than two antennas.