System for determining direction or attitude using GPS satellite signals

• US 5,021,792 A
• Filed: 01/12/1990
• Issued: 06/04/1991
• Est. Priority Date: 01/12/1990
• Status: Expired due to Fees

• Current Assignee: Rockwell International Corporation
• Original Assignee: Rockwell International Corporation
• Inventors: Hwang, Patrick Y.
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US07/464,271
• Time in Patent Office: 508 Days
• Field of Search: 342/357, 342/394, 342/356, 342/445, 342/446
• US Class Current: 342/357.31
• CPC Class Codes: G01S 19/55 Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method
• CPC Class Codes: H01Q 3/02 using mechanical movement of antenna or antenna system as a whole

Abstract

A system for determining spatial orientation based on the carrier phase of signals received from a set of GPS satellites. The system comprises an antenna array including a number of antennas coupled to GPS radio receivers, a mechanism for reconfiguring the positions of the antennas within the array and a signal processing module for processing the data collected by the antennas and the receivers. The mechanism for reconfiguring the antenna array is adapted for exchanging the positions of one pair of antennas and for rearranging the antennas from collinear into non-collinear patterns. Phase measurements are taken by the antennas and their associated receivers, both before and after antenna exchange and after antenna rearrangement in order to provide the data necessary to determine direction or attitude.

Claims

1. A method for determining attitude using GPS satellites and an antenna array including a plurality of antennas in which the positions of the antennas within the array may be selectively reconfigured, comprising the steps of:

arranging said antennas in a collinear pattern in which said antennas are spaced apart by known distances;

receiving and phase sampling signals from a plurality of GPS satellites with each of said antennas;

exchanging the positions of a pair of said antennas within said array while maintaining continuous phase tracking;

receiving and phase sampling signals from said plurality of GPS satellites with each of said antennas;

rearranging said antennas in a non-collinear pattern in which said antennas are spaced apart by known distances while maintaining continuous phase tracking;

receiving and phase sampling signals from said plurality of GPS satellites with each of said antennas; and

calculating the attitude of said antenna array based on the phase of said GPS signals received and sampled in the previous steps.

2. The method of claim 1 in which said plurality of GPS satellites includes four separate satellites and wherein receiver clock timing errors are eliminated from the attitude calculations by double differencing phase measurements between separate antennas and separate satellites.

3. The method of claim 1 in which said antenna array includes three separate antennas which are equally spaced apart in said collinear pattern and one of which is orthogonally positioned with respect to the others in said non-collinear pattern.

4. The method of claim 1, in which the step of calculating the attitude of said antenna array includes the steps of computing a set of double difference phase integer ambiguities between separate antennas and computing the coordinates of baseline and orthogonal vectors using further phase measurements and said phase integer ambiguities.

5. An apparatus for determining attitude using signals from a set of GPS satellites, comprising:

a plurality of antennas configurable into an array for receiving said signals at spaced apart locations;

means for exchanging the positions of a pair of said antennas within said array and also rearranging the positions of said antennas within said array from collinear to non-collinear patterns;

means for sampling the phase of said signals received by said antennas from said GPS satellites at the positions of each of said antennas before an antenna exchange, after an antenna exchange and after an antenna rearrangement and for tracking the phase of said signals from said GPS antennas during antenna exchange and rearrangement; and

means for calculating the attitude of said antenna array based on the measured phase of said signals.

6. The apparatus of claim 5 in which said set of GPS satellites includes four separate satellites and wherein receiver clock timing errors are eliminated from attitude calculations performed by said means for calculating by double differencing phase measurements between separate antennas and separate satellites.

7. The apparatus of claim 5 in which said antenna array includes three separate antennas which are equally spaced apart when arranged in said collinear pattern and one of which is orthogonally positioned with respect to the others when arranged in said non-collinear pattern.

8. The apparatus of claim 5, in which said set of GPS satellites includes three separate satellites and wherein one set of receiver clock timing errors are eliminated by synchronizing the receiver functions associated with the antennas to a common clock signal.

9. A method for determining direction and attitude using a set of GPS satellites and a system including an array of three or more antennas, one or more GPS radio receivers coupled to said antennas, and a computing means for processing the information acquired by said antennas and receivers, said method comprising the steps of:

configuring said array of antennas in a first predetermined pattern in which said antennas are spaced-apart by known distances;

sampling the phase of the GPS signals from said GPS satellites using said antennas and receivers;

exchanging the positions of a pair of said antennas while continuously tracking the phase of the GPS signals;

sampling the phase of the GPS signals from said GPS satellites using said antennas and receivers; and

reconfiguring said array of antennas in a second different predetermined pattern in which said antennas are spaced apart by known distances while continuously tracking the phase of said signals;

sampling the phase of said GPS signals from said GPS satellites using said antennas and receivers; and

computing the direction and attitude of said antenna array using said computing means.

10. The method of claim 9, wherein the antennas within said first predetermined pattern are collinear.

11. The method of claim 9 in which said set of GPS satellites includes four separate satellites and wherein receiver clock timing errors are eliminated from the directional computations by double differencing phase measurements between separate antennas and separate satellites.

12. The method of claim 9 in which said set of GPS satellites includes three separate satellites and wherein one set of receiver clock timing errors are eliminated by synchronizing the receiver functions associated with the antennas to a common clock signal.

13. An apparatus for determining direction using phase information derived from the signals provided by a set of GPS satellites, said apparatus comprising:

a plurality of antennas configurable into an antenna array in which the antennas are spaced apart by known distances;

one or more radio receivers coupled to said antennas which are adapted for sampling and continuously tracking the phase of said GPS signals as received by said antennas at their individual locations;

means for exchanging the positions of a pair of said antennas and rearranging said array into collinear and non-collinear patterns; and

means for processing data from said receivers and calculating the direction and attitude of said array based on the measured phase of said GPS signals from said satellites.

14. The apparatus of claim 13 in which said set of GPS satellites includes four separate satellites and wherein receiver clock timing errors are eliminated from attitude calculations performed by said microprocessor means by double differencing phase measurements between separate antennas and separate satellites.

15. The apparatus of claim 13 in which said antenna array includes three separate antennas which are equally spaced apart when arranged in said collinear pattern and one of which is orthogonally positioned with respect to the others when arranged in said non-collinear pattern.