Receiver calibration technique for global orbiting navigation satellite system (GLONASS)

• US 6,363,123 B1
• Filed: 02/23/1999
• Issued: 03/26/2002
• Est. Priority Date: 02/23/1999
• Status: Expired due to Term

• Current Assignee: Leica Geosystems Inc (Hexagon AB)
• Original Assignee: Leica Geosystems Inc (Hexagon AB)
• Inventors: Balodis, Miroslaw
• Primary Examiner(s): Chin, Stephen
• Assistant Examiner(s): JIANG, LENNY R
• Application Number:
  US09/255,972
• Time in Patent Office: 1,127 Days
• Field of Search: 375/130, 375/136, 375/141, 375/147, 375/148, 375/220, 375/229, 375/260, 375/316, 375/340, 375/354, 375/356, 375/362, 329/327, 329/348, 329/363, 455/12.1, 455/13.2, 701/207, 342/357.06, 342/357.13
• US Class Current: 375/316
• CPC Class Codes: G01S 19/235 Calibration of receiver components
• CPC Class Codes: G01S 19/36 relating to the receiver frond end
• CPC Class Codes: G01S 19/43 using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry

Abstract

A GLONASS receiver and a corresponding method for its calibration for more precise carrier phase measurements. The receiver includes a conventional receiver channel (36), having a bandpass filter (40) for establishing the sampling bandwidth prior to digitizing a plurality of received satellite signals, each having a different frequency. The receiver also includes a calibration channel (50) in which multiple satellite signals are bandbass filtered (in filter 58) at a single intermediate frequency, to avoid errors resulting from group delay variation introduced by passing multiple satellite signals through a common bandpass filter. The calibration channel (50) downconverts (56) to the intermediate frequency, bandpass filters (58), and then upconverts (60) again. Each satellite signal in turn is processed in this manner by selecting appropriate difference frequencies for downconversion and upconversion. The calibration channel (50) produces a set of reference carrier phase measurements that can be applied to correct errors in carrier phase measurements generated by the conventional receiver channels (36).

Claims

1. A global orbiting satellite system (GLONASS) receiver, comprising:

an antenna subsystem for receiving signals from a plurality of orbiting satellites;

a conventional receiver channel coupled to the antenna subsystem, the receiver channel being designed to receive, filter and digitally select the frequencies of signals from the plurality of orbiting satellites, wherein the satellites are distinguished by the use of different carrier frequencies and the receiver channel includes a bandpass filter; and

a calibration channel, including a single narrow bandpass filter centered at a selected intermediate frequency, and means for processing signals from each of the satellites in turn through the single filter, to provide for each channel a reference carrier phase measurement that is independent of effects arising from group delay variation introduced by the bandpass filter in the receiver channel.

2. A global orbiting satellite system (GLONASS) receiver as defined in claim 1, wherein the means for processing signals from each of the satellites in turn through the filter includes:

a first frequency mixer, for downconverting signals received from the antenna subsystem to the selected intermediate frequency;

a second frequency mixer, for upconverting signals output by the narrow bandpass filter, by the same frequency that the signals were downconverted in the first frequency mixer;

a local signal generator providing to the first and second frequency mixers a signal at a frequency that is the difference between the carrier frequency of signals received from a selected satellite and the intermediate frequency; and

means for applying satellite selection signals to the local signal generator, to effect selection of different satellite signals in turn for processing through the narrow bandpass filter.

3. A global orbiting satellite system (GLONASS) receiver as defined in claim 2, and further comprising:

means for storing the reference carrier phase measurements corresponding to each of multiple receiver channels; and

means for computing the difference between a carrier phase measurement from each conventional receiver channel and the reference carrier phase measurement corresponding to the same channel, to obtain a calibrated carrier phase measurement for each channel.

4. A global orbiting satellite system (GLONASS) receiver as defined in claim 3, wherein the means for storing the reference carrier phase measurements includes:

a plurality of phase measurement storage cells; and

a demultiplexer having an input derived from the calibration channel, multiple outputs coupled to the phase measurement storage cells, and a control signal input receiving satellite selection signals to effect switching of the demultiplexer to successive phase measurement storage cells.

5. A global orbiting satellite system (GLONASS) receiver as defined in claim 4, wherein:

the calibration channel and the conventional receiver channel each include an analog-to-digital converter; and

the carrier phase measurements and reference carrier phase measurements are converted to digital form for demultiplexing and storing.

6. A global orbiting satellite system (GLONASS) receiver as defined in claim 2, wherein the calibration channel further includes:

first and second wide passband filters to remove unwanted frequency images that are a necessary by-product of frequency mixing.

7. A method for calibration of a global orbiting satellite system (GLONASS) receiver, comprising the steps of:

receiving signals from a plurality of orbiting satellites, each distinguished by use of a different carrier frequency band;

bandpass filtering the plurality of orbiting satellite signals using a bandpass filter in each of a plurality of conventional receiver channels;

digitizing the filtered signal spectrum;

obtaining from the digitized filtered satellite channel signals a set of carrier phase measurements that is subject to errors resulting from the use of different passband filters in the receiver channels;

processing the received signals in a calibration channel that has a single bandpass filter centered at a selected intermediate frequency; and

generating in the calibration channel a set of carrier phase reference measurements that can be used to correct the carrier phase measurements from the conventional receiver channels.

8. A method as defined in claim 7, wherein the step of processing the received signals in the calibration channel includes:

downconverting the received signals by a difference frequency selected to position the frequency band of signals from a selected satellite over the intermediate frequency;

bandpass filtering the downconverted signals;

upconverting the signals after bandpass filtering, by the same selected difference frequency used in the downconverting step; and

periodically selecting a different satellite by changing the selected difference frequency used in the downconverting and upconverting steps;

and wherein the step of generating a set of carrier phase reference measurements includes tracking and measuring the carrier phase for each of the selected satellites, and storing the carrier phase measurements resulting from the foregoing processing steps.

9. A method as defined in claim 8, wherein the step of generating a set of carrier phase reference measurements further comprises:

receiving reference carrier phase measurements from the calibration channel; and

distributing the reference carrier phase measurements to separate storage units corresponding to the separate satellites.

10. A method as defined in claim 9, and further comprising:

computing corrected carrier phase measurements by computing the difference between the carrier phase measurements obtained from the conventional receiver channels and the corresponding reference carrier phase measurements stored in the storage units.