Frequency spectral line tracking receiver

• US 5,721,555 A
• Filed: 12/19/1994
• Issued: 02/24/1998
• Est. Priority Date: 12/19/1994
• Status: Expired due to Fees

• Current Assignee: Trimble Navigation Limited (Trimble Inc.)
• Original Assignee: Trimble Navigation Limited (Trimble Inc.)
• Inventors: Lennen, Gary R.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/358,480
• Time in Patent Office: 1,163 Days
• Field of Search: 342/357, 342/352, 455/12.1, 370/70
• US Class Current: 342/357.62
• CPC Class Codes: G01S 19/23 Testing, monitoring, correcting or calibrating of receiver elements
• CPC Class Codes: G01S 19/29 carrier including Doppler, related G01S19/246 takes precedence

Abstract

An improved navigation satellite receiver for tracking individual spread-spectrum frequency spectral lines with a microwave receiver antenna to receive signals from orbiting navigation satellites, a downconverter to produce in-phase and quadrature (I and Q) signals from the received satellite signals, and a digital processing system for frequency and phase locking numeric controlled oscillators (NCO) to the carrier and code of the satellite signals. The improvement comprises at least one spectral line tracker connected to receive the (I and Q) signals and including a spectral line numeric controlled oscillator (NCO) connected to a spectral line mixer that drives a spectral line code correlator. The spectral line NCO is frequency-aided to frequency lock on a spectral line from a value obtained from the carrier NCO.

Claims

1. A method (70) for correcting distortions in spread-spectrum radio transmissions from orbiting navigation satellites, the method comprising the steps of:

receiving (72) radio transmissions from said orbiting navigation satellites with a navigation receiver;

measuring (74) the amplitude and phase of a plurality of individual spectral lines of energy which are constituent to a modulated double-sideband-with-carrier envelope in said radio transmissions;

identifying (76) an individual one of said orbiting navigation satellites by its C/A-code sequence; and

correcting (78) the amplitude and phase of said radio transmissions received according to a comparison of amplitude and phase measurements between measurements obtained in the step of measuring with a template for an ideal distortion-free representation of a radio carrier modulated by said C/A-code sequence for said orbiting navigation satellite identified in the step of identifying.

2. A method (80) for determining ionospheric delays from a single spread-spectrum radio transmission from orbiting navigation satellites, the method comprising the steps of:

receiving (82) radio transmissions from said orbiting navigation satellites with a navigation receiver;

measuring (84) the amplitude and phase of individual spectral lines of energy which are constituent to the modulated double-sideband-with-carrier envelope in said radio transmissions;

identifying (86) an individual one of said orbiting navigation satellites by its C/A-code sequence; and

comparing (88) the phase relation between individual spectral line of energy measurements obtained in the step of measuring and determining therefrom an estimate of an ionospheric delay between said orbiting navigation satellites and said receiver.

3. A method (90) for tracking individual spectral lines of energy in a spread-spectrum modulated radio carrier transmission from orbiting navigation satellites, the method comprising the steps of:

receiving (92) radio transmissions from said orbiting navigation satellites with a navigation receiver;

phase-locking (94) a first local oscillator to said radio carrier transmission at a frequency "F_c " obtained in the step of receiving; and

frequency-aiding (96) a second local oscillator to phase-lock on a single one of said individual spectral lines of energy with a signal derived from said first local oscillator.

4. The method of claim 3, further comprising the step of:

computing (100) ionospheric delays from a difference in phase of separately-measured said spectral lines.

5. An improved navigation satellite receiver (10) for tracking individual spread-spectrum frequency spectral lines with a microwave receiver antenna to receive signals from orbiting navigation satellites, a downconverter to produce in-phase and quadrature (I and Q) signals from said received satellite signals, and a digital processing system for frequency and phase-locking a plurality of numeric controlled oscillators (NCO) (30, 34) to the carrier and code of said satellite signals, the improvement comprising:

at least one spectral line tracker (36) connected to receive said (I and Q) signals and including a spectral line numeric controlled oscillator (NCO) (42) connected to a spectral line mixer (38) that drives a spectral line code correlator (40), wherein the spectral line NCO is frequency-aided to frequency lock on a spectral line from a value obtained from said carrier NCO (30).

6. The receiver of claim 5, wherein:

said carrier NCO (30) is included in a carrier tracking loop with a bandwidth of approximately ten hertz; and

said spectral line NCO (42) is included in a carrier tracking loop with a bandwidth of approximately 0.05 Hz.

7. The receiver of claim 5, further comprising:

a microcomputer (28) connected to a code correlator (26) driven by the carrier and code NCO'"'"'s (30,

     34) and to said spectral line code correlator (40) and including integer ambiguity resolution means for comparing the phases of adjacent spectral lines one kilohertz apart to resolve said receiver'"'"'s position in a three hundred kilometer range from said orbiting navigation satellites.

8. The receiver of claim 7, wherein:

the microcomputer (28) further includes means for comparing the phases of spectral lines two kilohertz apart to resolve said receiver'"'"'s position in a one hundred and fifty kilometer range from said orbiting navigation satellites.

9. The receiver of claim 5, further comprising:

a microcomputer (28) connected to a code correlator (26) driven by the carrier and code NCO'"'"'s (30,

     34) and to said spectral line code correlator (40) and including integer ambiguity resolution means for measuring the phases of a plurality of pairs of spectral lines with varying discrete frequency separations to resolve said receiver'"'"'s position in range from each of said orbiting navigation satellites by simultaneous solution of a plurality of said measurements, wherein carrier phase integer ambiguity is overcome.