Dual mode satellite signal receiver and method thereof

• US 8,184,048 B2
• Filed: 02/26/2009
• Issued: 05/22/2012
• Est. Priority Date: 02/29/2008
• Status: Active Grant

• Current Assignee: Synergy Innovation Co., Ltd.
• Original Assignee: Synergy Innovation Co., Ltd.
• Inventors: Yoo, Chang-Sik, Jo, Jun-Gi, Park, Seong-Eon
• Primary Examiner(s): Tarcza, Thomas
• Assistant Examiner(s): McGue, Frank J
• Application Number:
  US12/393,107
• Publication Number:
  US 20090219204A1
• Time in Patent Office: 1,181 Days
• Field of Search: 342/357.01, 342/357.73, 342/357.23
• US Class Current: 342/357.73
• CPC Class Codes: G01S 19/33 Multimode operation in different systems which transmit time stamped messages, e.g. GPS/GLONASS
• CPC Class Codes: G01S 19/37 Hardware or software details of the signal processing chain
• CPC Class Codes: H03G 3/3052 in bandpass amplifiers (H.F. or I.F.) or in frequency-changers used in a (super)heterodyne receiver H03G3/32, H03G3/34 take precedence
• CPC Class Codes: H03G 7/001 without controlling loop H03G7/007, H03G7/02, H03G7/06 take precedence

Abstract

A dual mode satellite signal receiver capable of supporting at least two global navigation satellite systems and a satellite signal receiving method are provided. The dual mode satellite signal receiver comprises a frequency synthesizer for generating a local oscillator signal based on a reference frequency; a mixer for mixing the local oscillator signal with a satellite signal and outputting the mixed signal as a signal of an intermediate frequency band; a first filter for filtering the signal output from the mixer to reject an image signal and output only an actual signal; a second filter for filtering the actual signal to output only a predetermined bandwidth according to a positioning mode; and an amplifier for amplifying the second filter output signal to a predetermined level and outputting the amplified signal.

Claims

1. A dual mode satellite signal receiver capable of supporting at least two global navigation satellite systems, the dual mode satellite signal receiver comprising:

a frequency synthesizer operative to generate a local oscillator signal based on a reference frequency wherein the frequency synthesizer is capable of supporting multiple reference frequencies;

a mixer operative to mix the local oscillator signal with a satellite signal and outputting a mixed signal where the mixed signal comprises a signal in an intermediate frequency band;

a first filter operative to filter the mixed signal to reject an image signal and output an actual signal;

a second filter operative to filter the actual signal received from the first filter to output a signal in a predetermined bandwidth based on a mode of the receiver; and

a variable gain amplifier operative to amplify the signal received from the second filter to a predetermined level and output the amplified signal,

wherein the variable gain amplifier comprises and which comprises an exponential current generator operative to generate a first current and a second current such that a ratio of the first current to the second current varies exponentially to a linear-gain-control voltage received from an automatic gain control loop;

an exponential current-to-voltage converter operative to convert the first current and the second current into voltages; and

an amplifier operative to amplify an input signal by a gain based on the voltages from the exponential current-to-voltage converter.

2. The dual mode satellite signal receiver according to claim 1, wherein the frequency synthesizer is a fractional-N phase locked loop capable of supporting multiple reference frequencies.

3. The dual mode satellite signal receiver according to claim 2, wherein the frequency synthesizer comprises:

a voltage controlled oscillator operative to provide the local oscillating signal;

a fractional-N divider operative to divide a frequency of the local oscillator signal by a divisor based on a reference frequency; and

a frequency detector operative to compare the reference frequency with the frequency of the signal received from the fractional-N divider and outputting a control signal,

wherein the frequency of the voltage controlled oscillator is updated based on the control signal from the frequency detector.

4. The dual mode satellite signal receiver according to claim 1, wherein a center frequency of the second filter is controlled by a clock signal provided by the frequency synthesizer.

5. A dual mode satellite signal receiver capable of supporting at least two global navigation satellite systems, the dual mode satellite signal receiver comprising:

a frequency synthesizer operative to generate a local oscillator signal based on a reference frequency;

a mixer operative to mix the local oscillator signal with a satellite signal and outputting a mixed signal where the mixed signal comprises a signal in an intermediate frequency band;

a first filter operative to filter the mixed signal to reject an image signal and output an actual signal;

a second filter operative to filter the actual signal received from the first filter to output a signal in a predetermined bandwidth based on a mode of the receiver; and

a variable gain amplifier operative to amplify the signal received from the second filter to a predetermined level and output the amplified signal, wherein the variable gain amplifier is configured to utilize two internally-generated currents such that the ratio of the currents depend on either only NMOS or only PMOS transistors,

wherein the variable gain amplifier comprises an exponential current generator operative to generate a first current and a second current such that a ratio of the first current to the second current varies exponentially to a linear-gain-control voltage received from an automatic gain control loop;

an exponential current-to-voltage converter operative to convert the first current and the second current into voltages; and

an amplifier operative to amplify an input signal by a gain based on the voltages from the exponential current-to-voltage converter.

6. The dual mode satellite signal receiver according to claim 5, wherein the exponential current generator comprises:

a single-to-differential converter operative to receive a single input voltage and outputting two differential voltages;

a first current generator having an NMOS transistor and configured to generate a first current, where a first differential voltage is input to a gate terminal of the NMOS transistor, and a current source is connected to a drain terminal of the NMOS transistor;

a first current mirror operative to mirror and output the first current;

a second current generator having an NMOS transistor and configured to generate a second current, where a second differential voltage is input to a gate terminal of the NMOS transistor, and a current source is connected to a drain terminal of the NMOS transistor; and

a second current mirror operative to mirror and output the second current.

7. The dual mode satellite signal receiver according to claim 5, wherein the exponential current generator comprises:

a single-to-differential converter operative to receive a single input voltage and outputting two differential voltages;

a first current generator having a PMOS transistor and configured to generate a first current, where a first differential voltage is input to a gate terminal of the PMOS transistor, and a current source is connected to a source terminal of the PMOS transistor;

a first current mirror operative to mirror and output the first current;

a second current generator having an PMOS transistor and configured to generate a second current, where a second differential voltage is input to a gate terminal of the PMOS transistor, and a current source is connected to a source terminal of the PMOS transistor; and

a second current mirror operative to mirror and output the second current.

8. The dual mode satellite signal receiver according to claim 5, wherein the frequency synthesizer is a fractional-N phase locked loop capable of supporting multiple reference frequencies.

9. The dual mode satellite signal receiver according to claim 8, wherein the frequency synthesizer comprises:

a voltage controlled oscillator operative to provide the local oscillating signal;

a fractional-N divider operative to divide a frequency of the local oscillator signal by a divisor based on a reference frequency; and

a frequency detector operative to compare the reference frequency with the frequency of the signal received from the fractional-N divider and outputting a control signal,

wherein the frequency of the voltage controlled oscillator is updated based on the control signal from the frequency detector.

10. The dual mode satellite signal receiver according to claim 5, wherein a center frequency of the second filter is controlled by a clock signal provided by the frequency synthesizer.

11. The dual mode satellite signal receiver according to claim 5, wherein the mixer mixes the local oscillator signal with a satellite signal and outputs two signals of an intermediate frequency band having a phase difference of 90 degrees.

12. A satellite signal receiving method for a dual mode satellite signal receiver capable of supporting at least two global navigation satellite systems, the method comprising:

generating a local oscillator signal based on a reference frequency;

mixing the local oscillator signal with a satellite signal and outputting a mixed signal where the mixed signal comprises a signal in an intermediate frequency band;

filtering the output signal in the intermediate frequency band to reject an image signal and output an actual signal;

filtering the actual signal to output a signal in a predetermined bandwidth based on a mode of the receiver; and

amplifying the output signal in the predetermined bandwidth to a predetermined level, wherein the amplifying comprises generating a first current and a second current such that a ratio of the first current to the second current varies exponentially to a linear-gain-control voltage received from an automatic gain control loop;

converting the first current and the second current into respective voltages; and

amplifying the output signal in the predetermined bandwidth by a gain based on the two respective voltages.

13. The satellite signal receiving method according to claim 12, wherein generating a first current and a second current comprises:

converting a single-ended input signal into two differential signals;

generating a first current by inputting a first differential signal into a gate terminal of a first NMOS transistor, where a current source is connected to a drain terminal of the first NMOS transistor; and

generating a second current by inputting a second differential signal into a gate terminal of a second NMOS transistor, where a current source is connected to a drain terminal of the second NMOS transistor.

14. The satellite signal receiving method according to claim 12, wherein generating a first current and a second current includes:

converting a single-ended input signal into two differential signals;

generating a first current by inputting a first differential signal into a gate terminal of a first PMOS transistor, where a current source is connected to a source terminal of the first PMOS transistor; and

generating a second current by inputting a second differential signal into a gate terminal of a second PMOS transistor, where a current source is connected to a source terminal of the second PMOS transistor.

15. The satellite signal receiving method according to claim 12, wherein the generating a local oscillator signal includes:

generating the local oscillator signal of a predetermined frequency;

fractionally dividing a frequency of the local oscillator signal by a divisor based on a reference frequency;

comparing the reference frequency with the divided frequency of the local oscillator signal and generating a corresponding control signal; and

changing the frequency of the local oscillator signal based on the control signal.

16. The satellite signal receiving method according to claim 12, wherein the mixing mixes the local oscillator signal with a satellite signal and outputs two signals of an intermediate frequency band having a phase difference of 90 degrees.