Single global positioning system receiver capable of attitude determination

• US 5,943,008 A
• Filed: 09/23/1997
• Issued: 08/24/1999
• Est. Priority Date: 09/23/1997
• Status: Expired due to Term

• Current Assignee: Teledyne Scientific & Imaging, LLC (Teledyne Technologies Incorporated)
• Original Assignee: Rockwell Science Center, Inc.
• Inventors: Van Dusseldorp, David L.
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US08/935,943
• Time in Patent Office: 700 Days
• Field of Search: 342/357, 342/423, 342/445, 701/213
• US Class Current: 701/213
• CPC Class Codes: G01S 19/54 using carrier phase measurements; using long or short baseline interferometry

Abstract

A platform attitude determination can be made with a single receiver in a global positioning system (GPS). The receiver receives at least three sets of GPS signals from three antennas. Two of the GPS signals are delayed so that the receiver receives each GPS signal in separate time domain slots. In this way, the synchronization of separate GPS receivers does not have to be accomplished.

Claims

1. A global positioning system capable of determining an attitude factor, the system comprising:

a receiver having an antenna interface;

a first antenna electrically coupled to the antenna interface;

a second antenna disposed in a first fixed relationship to the first antenna and electrically coupled to the antenna interface through a first delay circuit;

a third antenna disposed in a fixed second relationship to the first antenna and electrically coupled to the antenna interface through a second delay circuit; and

wherein the receiver compares a first signal received by the first antenna, a second signal received by the second antenna, and a third signal received by the third antenna to determine the attitude factor.

2. The system of claim 1, wherein the attitude factor includes an azimuth angle.

3. The system of claim 1, wherein the attitude factor includes an elevation angle.

4. The system of claim 1, wherein the second signal is adjusted in accordance with a first delay associated with the first delay circuit.

5. The system of claim 4, wherein the third signal is adjusted in accordance with a second delay associated with the second delay circuit.

6. The system of claim 5, wherein the first signal, the second signal, and the third signal include carrier phase information.

7. The system of claim 5, wherein the receiver synchronously receives the first signal, the second signal, and the third signal on a group of channels.

8. A positioning receiver, comprising:

at least three antennas disposed in a fixed relationship to each other to receive a first set of satellite signals, a second set of satellite signals, and a third set of satellite signals, the second set and the third set being delayed with respect to the first set; and

receiving means for processing the first set, the second set, and the third set, and determining an attitude factor in accordance with the first set, the second set, and the third set and the fixed relationship.

9. The receiver of claim 8, wherein the attitude factor includes an azimuth angle.

10. The receiver of claim 9, wherein the attitude factor includes an elevation angle.

11. The receiver of claim 8, wherein the third set is delayed with respect to the second set.

12. The receiver of claim 11, wherein the receiver means calculates a first relative position in response to the first set, a second relative position in response to the second set, and a third relative position in response to the third set, the first set, the second set, and the third set are in different time domain slots to prevent the first set from affecting determination of the second relative position and the third relative position.

13. The receiver of claim 8, wherein the first set, the second set, and the third set include satellite code and carrier phase information.

14. The receiver of claim 12, wherein the attitude factor is determined by adjusting the second set and the third set in accordance with a first delay and a second delay.

15. The receiver of claim 8, wherein the receiver means simultaneously receives the first set, the second set, and the third set on three separate groups of channels.

16. The receiver of claim 8, wherein the receiver means sequentially receives the first set, the second set, and the third set on a group of channels.

17. A method of determining an attitude factor for a vehicle, the vehicle including a positioning system having a first antenna, a second antenna, and a third antenna, the first antenna, the second antenna, and the third antenna being disposed in a positional relationship, the method comprising:

receiving a first set of satellite signals on the first antenna;

receiving a second set of satellite signals on the second antenna;

delaying the second set of satellite signals for a first time with respect to the first set;

receiving a third set of satellite signals on the third antenna;

delaying the third set of satellite signals for a second time with respect to the first set; and

determining the attitude factor by processing with the first set, the second set, and the third set and the fixed relationship.

18. The method of claim 17, wherein the delaying steps utilize a length of cable.

19. The method of claim 18, wherein the first time is approximately 200 nanoseconds.

20. The method of claim 17, wherein the attitude factor includes an azimuth angle and an elevation angle.