Time-relative positioning for static applications

• US 5,999,123 A
• Filed: 09/13/1995
• Issued: 12/07/1999
• Est. Priority Date: 09/13/1995
• Status: Expired due to Term

• Current Assignee: Rockwell International Corporation
• Original Assignee: Rockwell International Corporation
• Inventors: Ulmer, Karl, Disselkoen, Brent, Hwang, Patrick
• Primary Examiner(s): Issing, Gregory C.
• Application Number:
  US08/527,605
• Time in Patent Office: 1,546 Days
• Field of Search: 342/357, 342/442, 342/443, 364/449.7, 364/449.8, 364/449.9
• US Class Current: 342/357.26
• CPC Class Codes: G01S 19/43 using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry
• CPC Class Codes: G01S 5/0226 Transmitters

Abstract

A system of utilizing a single radio receiver with continuously broadcast GPS signals in order to determine precise relative positioning between two arbitrary positions or to determine current position. The invention includes utilizing changes in the carrier signal as detected by the GPS receiver occurring as a result of the movement from a first position to a second position.

Claims

1. A method of determining a time-relative positioning measurement between an initial position and a second position utilizing a single radio receiver having processing means, comprising the following steps:

signaling the start of the measurement after acquiring a given constellation of GPS satellites, the start of the measurement corresponding to an initial position;

recording carrier phase observations for each of the GPS satellites in the given constellation;

signaling the end of the measurement interval, the end of the measurement corresponding to a second position;

said second position not required to be known upon signaling the start of the measurement;

computationally processing the carrier phase observations from the given constellation to produce a solution vector between the initial position and the second position; and

computationally estimating the quality of the solution vector produced by taking into consideration known error sources and the effects of satellite geometry for the given constellation.

2. The method of claim 1, wherein the recording of signals from the constellation of GPS satellites is comprised of recording the signals of four GPS satellites.

3. The method of claim 1, wherein at least one of the known error sources is a multi-path error assigned to each of the satellites in the GPS constellation.

4. The method of claim 1, wherein at least one of the known error sources is an ionosphere delay change assigned a value of zero based on a short time interval approximation.

5. A method of determining a time-relative positioning measurement utilizing a single GPS radio receiver, comprising the following steps:

signaling the start of the measurement after acquiring a given constellation of GPS satellite, the start of the measurement corresponding to an initial position;

recording the carrier phase observations for each of the GPS satellites in the given constellation;

signaling the end of the measurement interval, the end of the measurement corresponding to a second position;

performing a calibration determination by temporarily remaining stationary at one of the initial or second positions for the purpose of reducing assumed position error;

computationally processing the carrier phase observations from the given constellation to produce a solution vector; and

computationally estimating the quality of the solution vector produced by taking into consideration known error sources and the effects of satellite geometry for the given constellation;

wherein the vector information represents a straight line between the initial position and the second position.

6. The method of claim 5, wherein the recording of signals from the constellation of GPS satellites is comprised of recording the signals of four GPS satellites.

7. The method of claim 5, further comprising the step of determining an intermediate vector while traversing between the initial position and the second position in order to provide a real time update of position with respect to previous positions.

8. The method of claim 5, wherein at least one of the known error sources is a multi-path error assigned to each of the satellites in the GPS constellation.

9. The method of claim 5, wherein at least one of the known error sources is an troposphere delay change assigned a value of zero.