Method and apparatus for improving the accuracy of position estimates in a satellite based navigation system

• US 5,430,654 A
• Filed: 12/01/1992
• Issued: 07/04/1995
• Est. Priority Date: 12/01/1992
• Status: Expired due to Fees

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: Gudat, Adam, Kyrtsos, Christos T.
• Primary Examiner(s): Chin, Gary
• Application Number:
  US07/984,108
• Time in Patent Office: 945 Days
• Field of Search: 364/443, 364/449, 364/455, 364/459, 73/178 R, 342/357, 342/358, 342/450, 342/451, 342/457, 342/463, 342/465
• US Class Current: 701/215
• CPC Class Codes: G01S 19/41 Differential correction, e.g. DGPS [differential GPS]

Abstract

An apparatus and method are disclosed for determining the position of a vehicle at or near the surface of the Earth using navigation signals from a satellite-based navigation system. Precise position estimates are achieved by reducing effective receiver noise. A plurality of receiver means each compute a pseudorange for each satellite. A signal optimizer then uses the pseudoranges from each receiver means to compute an optimal pseudorange for each satellite. A processor means computes a vehicle position from the optimal pseudoranges.

Claims

1. An apparatus for determining the position of a vehicle at or near the surface of the Earth using navigation signals from a satellite-based navigation system having a plurality of navigation satellites, the apparatus comprising:

first means mounted on the vehicle for receiving the navigation signals from the plurality of satellites and for computing, from the navigation signals, a first pseudorange for each of the plurality of satellites, each said first pseudorange representing the distance between said first means and a corresponding one of the plurality of satellites;

second means mounted on the vehicle for receiving the navigation signals from the plurality of satellites and for computing a second pseudorange for each of the plurality of satellites from the navigation signals, each said second pseudorange representing the distance between said second means and a corresponding one of the plurality of satellites;

third means for receiving said first and second pseudoranges and for computing, for each one of the plurality of satellites, an optimal pseudorange;

fourth means for computing a satellite position for each of the plurality of satellites from the navigation signals received by said first means; and

fifth means for computing the position of the vehicle from said satellite positions and said optimal pseudoranges.

2. The apparatus of claim 1, wherein said third means comprises means for averaging said first and second pseudoranges to compute said optimal pseudorange.

3. An apparatus for determining the position of a vehicle at or near the surface of the Earth using navigation signals from a Global Positioning System which includes a plurality of satellites orbiting the Earth, the apparatus comprising:

first means mounted on the vehicle for receiving the, navigation signals from the plurality of satellites;

second means mounted on the vehicle for receiving the navigation signals from the plurality of satellites;

third means, electrically connected to said first and second means, for computing a satellite position for each satellite based on the navigation signals received by said first and second means, a first pseudorange from the navigation signals received by said first means, and a second pseudorange based on the navigation signals received by said second means;

fourth means for receiving said first and second pseudoranges and for computing an optimal pseudorange for each satellite; and

fifth means for computing the position of the vehicle from said satellite positions and said optimal pseudoranges.

4. The apparatus of claim 3, wherein said fourth means comprises means for averaging said first and second pseudoranges to compute said optimal pseudorange.

5. A method for determining the position of a vehicle at or near the surface of the Earth using navigation signals from a satellite-based navigation system having a plurality of satellites, the method comprising the steps of:

(a) receiving the navigation signals from each of the plurality of satellites at a plurality of antennas mounted on the vehicle;

(b) computing from the navigation signals, for each antenna, a pseudorange to each satellite;

(c) computing an optimal pseudorange for each satellite by averaging said pseudoranges across said plurality of antennas;

(d) computing a satellite position for each of the plurality of satellites from the navigation signals; and

(e) determining the position of the vehicle from said satellite positions and said optimal pseudoranges.

6. The method of claim 5, wherein step (b) of computing is performed using a plurality of receivers, each of said plurality of receivers being connected to a corresponding one of said plurality of antennas.

7. The method of claim 5, wherein step (b) of computing is performed using a single receiver connected to each of said plurality of antennas.