System for simultaneously deriving position information from a plurality of satellite transmissions

• US 5,014,066 A
• Filed: 07/20/1989
• Issued: 05/07/1991
• Est. Priority Date: 03/01/1982
• Status: Expired due to Term

• Current Assignee: Western Atlas International Incorporated (Northrop Grumman Corporation)
• Original Assignee: Western Atlas International Incorporated (Northrop Grumman Corporation)
• Inventors: Counselman, III, Charles C.
• Primary Examiner(s): Barron, Jr., Gilberto
• Assistant Examiner(s): Sotomayor, John B.
• Application Number:
  US07/382,291
• Time in Patent Office: 656 Days
• Field of Search: 342/352, 342/357, 342/450, 342/451, 342/453, 342/463, 342/464, 342/465, 342/417, 342/442, 342/444
• US Class Current: 342/352
• CPC Class Codes: G01C 15/00 Surveying instruments or accessories not provided for in groups G01C1/00 - G01C13/00
• CPC Class Codes: G01S 19/35 Constructional details or hardware or software details of the signal processing chain
• CPC Class Codes: G01S 19/44 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method

Abstract

A method and a system are disclosed for measuring the baseline vector b between a pair of survey marks on the ground by radio interferometry using radio signals broadcast from the earth orbiting satellites of the NAVSTAR Global Positioning System (GPS), the radio signals broadcast by the satellites being double-sideband modulated with their carriers suppressed. The signals received by one antenna during a predetermined time span are separated into upper and lower sideband components. These separate components are filtered, converted to digital form, and then multiplied together. Differences in Doppler shift are utilized to distinguish the carriers of different satellites. Thus, the powers and carrier phases of the signals from a plurality of satellites are measured simultaneously and numerical data representing the measurement results are obtained at each survey mark. The measurements are performed in real time at each mark without reference to signals that are received at any other place and without knowledge of any of the coded signals that modulate the GPS carriers.

Claims

1. A method of determining position information from a composite of spread spectrum, suppressed carrier signals transmitted simultaneously at the same frequencies by a plurality of orbiting satellites and received simultaneously from different directions by an antenna, comprising:

(a) forming a digital representation of said composite;

(b) applying said digital representation to a plurality of logic circuits, each said logic circuit being responsive to the signal transmitted by a different selected satellite and operating synchronously in response to a common clock;

(c) deriving simultaneously, in each said logic circuit, data representing the signal transmitted by the satellite to which each said logic circuit is responsive; and

(d) combining the simultaneously derived data from a plurality of said logic circuits to determined position information.

2. The method of claim 1 wherein the simultaneously derived data are related to the phases of carrier waves implicit in the signals received from the satellites.

3. The method of claim 2 wherein the digital representation of the composite is derived by sampling an analog representation of the composite.

4. The method of claim 3 wherein the analog representation is a spread spectrum signal received from a plurality of satellites.

5. The method of claim 4 wherein the analog representation is a baseband signal.

6. The method of claim 5 wherein the signal received from each said satellite is a double sideband signal and the baseband signal represents a selected sideband thereof.

7. Apparatus for determining position information from a composite of spread spectrum, suppressed carrier signals transmitted simultaneously at the same frequencies by a plurality of orbiting satellites and received simultaneously from different directions by an antenna, comprising:

(a) means for forming a digital representation of said composite;

(b) a plurality of logic circuits operating synchronously in response to a common clock, each said logic circuit being responsive to a signal transmitted by a different selected satellite included in said digital representation;

(c) means in each said logic circuit for deriving simultaneously data representing the signal transmitted by the satellite to which each said logic circuit is responsive; and

(d) means for combining the simultaneously derived data from a plurality of said logic circuits to determine position information.

8. The apparatus of claim 7 wherein the means in each logic circuit for simultaneously deriving data includes means for simultaneously deriving data related to the phase of a carrier wave implicit in the signal received from the selected satellite.

9. The apparatus of claim 8 wherein the means for forming a digital representation of the composite includes means for sampling an analog representation of the composite.

10. The apparatus of claim 9 wherein the analog representation is a spread spectrum signal received from a plurality of satellites.

11. The apparatus of claim 10 wherein the analog representation is a baseband signal.

12. The apparatus of claim 11 wherein the signal received from each said satellite is a double sideband signal and the baseband signal represents a selected sideband thereof.