Differential phase measurement through antenna multiplexing

• US 5,268,695 A
• Filed: 10/06/1992
• Issued: 12/07/1993
• Est. Priority Date: 10/06/1992
• Status: Expired due to Term

• Current Assignee: Trimble Navigation Limited (Trimble Inc.)
• Original Assignee: Trimble Navigation Limited (Trimble Inc.)
• Inventors: Dentinger, Michael P., Cohen, Clark E.
• Primary Examiner(s): Hellner, Mark
• Application Number:
  US07/957,271
• Time in Patent Office: 427 Days
• Field of Search: 342/352, 342/357, 342/386, 342/407, 342/417, 342/432, 342/433, 342/442, 342/445
• US Class Current: 342/357.27
• CPC Class Codes: G01S 19/37 Hardware or software details of the signal processing chain
• CPC Class Codes: G01S 19/54 using carrier phase measurements; using long or short baseline interferometry

Abstract

An embodiment of the present invention is a system for time multiplexing a carrier signal received by two or more GPS antennas through a single hardware path, using a single receiver'"'"'s oscillator in that hardware path as a reference to compare the phase from each antenna. One of the antennas is designated as a reference antenna and a carrier signal received by it is used to phase lock in numerically controlled oscillator. The same carrier signal received by the other antennas is periodically compared in phase to the output of the numerically controlled oscillator. Each comparison results in a phase angle measurement for the respective antennas compared to the master antenna.

Claims

1. A direction angle measurement system, comprising:

at least two GPS antennas for producing a plurality of respective output signals for a GPS carrier signal that differ in phase according to the geometry of the relative positions of the GPS antennas and a GPS satellite transmitting said GPS carrier signal;

input multiplexing means for selecting one of said output signals from the GPS antennas and having a selected-antenna output signal;

a radio frequency amplification stage for producing an amplified RF signal from said selected-antenna output signal;

a correlator for mixing said amplified RF signal with a reference frequency signal to produce a phase detector signal output;

output multiplexing means synchronized to the input multiplexing means for distributing said phase detector signal output to respective differential phase output signal ports;

a variable frequency oscillator for generating said reference frequency signal;

a phase locked loop for controlling the variable frequency oscillator to lock in phase to said selected-antenna output signal during a first time period when a first of said GPS antennas is selected and to substantially not drift from said phase lock at time periods other than said first time period; and

a phase differencer for measuring a phase difference between said reference frequency signal and said selected-antenna output signal at a second time when a second of said GPS antennas is selected, wherein said phase difference is proportional to a differential range between the GPS antennas and said GPS satellite.

2. The system of claim 1, wherein:

the input multiplexing means comprises at least two high-speed GaAs FET switches that sequentially feed the output of each GPS antenna into the correlator.

3. The system of claim 1, wherein:

the input multiplexing means comprises at least two high-speed PIN diodes that sequentially feed the output of each GPS antenna into the correlator.

4. A measurement system, comprising:

a single GPS hardware channel having a correlator output;

multiplex means for high-speed electronic sequential feeding of the output of more than one GPS antenna into the single GPS hardware channel;

means for designating a signal from one of said GPS antennas as a master to serve as a GPS carrier phase reference;

loop means for tracking a GPS carrier when said master signal passes through said GPS hardware channel and locking said correlator output of the single GPS hardware channel to the master signal;

isolation means for running the loop means open-loop when any of the signals from GPS antennas not said master signal runs through said GPS hardware channel; and

measurement means for reading a carrier phase angle at said correlator output of the single GPS hardware channel.

5. The system of claim 4, further comprising:

transfer function means for filtering raw differential phase measurements from said correlator output of the single GPS hardware channel with H(z); and

clocking means for advancing the multiplex means at a rate sufficient to allow the system to track differential phase dynamics.

6. A method of attitude determination, the method comprising the steps of:

time multiplexing at least a first and a second antenna signal having independent phase relationships that are respectively received by two or more corresponding GPS antennas;

phase locking a variable frequency oscillator to one of said antenna signals during a first time period when said one antenna signal is being time multiplexed; and

comparing the phase of another than said one antenna signal to a reference frequency signal output of said variable frequency oscillator at a second time period that is sufficiently proximate to said first time period wherein said variable frequency oscillator does not substantially drift from said phase lock and said phase comparison will result in a difference that is proportional to a differential range between said GPS antennas and a GPS satellite.

7. The method of claim 6, further comprising the steps of:

defining one of said GPS antennas as a reference position wherein the step of phase locking comprises phase locking said variable frequency oscillator to said particular one GPS antenna.

8. A process for antenna phase angle measurement wherein a plurality of GPS antennas are multiplexed into a common correlator and one of the antennas is arbitrary selected to act as a master reference for an oscillator, the process comprising the steps of:

selecting an antenna from a group of slave antennas and a master antenna to be used for a next set of measurements;

setting an input multiplexer according to said antenna selected;

determining if said input multiplexer is on a master antenna or a slave antennas;

updating a numerically controlled oscillator based on any measured carrier phase tracking error obtained from a correlator at the output of said input multiplexer;

closing a slave antenna differential phase loop, if a slave antenna has been selected;

updating a code phase based on a measured code tracking error from an early-minus-late accumulator;

concurrently demodulating GPS data transmitted from a GPS satellite with antenna selecting

storing the sign of modulated data that has been integrated over a fraction of the data bit period together with a record of the time that antenna switches occur, wherein a detecting of bit transitions in said GPS data permits ranging and said recording the time of bit transitions allows a receiver to resolve how many integer C/A code epochs lie between a particular GPS satellite and receiver;

drifting antenna selection timing such that the switching edges will drift with respect to said data bit transition edges such that bit transitions are possible to detect on all GPS satellites being tracked;

accessing a stored history of signs of said received data to detect bit transitions wherein each transition is not observed across an antenna switching event;

observing carrier phase errors from a correlator while dwelling on said master antenna to determine if an aliasing condition exists, wherein such a determination is made on the basis of measurements averaged over several antenna switch periods to overcome receiver noise;

correcting signal tracking if aliasing is detected in the step of observing;

scheduling antenna switching such that said master antenna always catches at least some part of each data bit received from all the GPS satellites being tracked; and

integrating said parts of each data bit received and storing each received data bit in a buffer.