Antenna LNA filter for GNSS device

• US 9,748,926 B2
• Filed: 09/19/2013
• Issued: 08/29/2017
• Est. Priority Date: 09/19/2012
• Status: Active Grant

• Current Assignee: Javad GNSS, Inc.
• Original Assignee: Javad GNSS, Inc.
• Inventors: Ashjaee, Javad, Dubrovsky, Dmitry
• Primary Examiner(s): Nguyen, Chuong P
• Application Number:
  US14/031,363
• Publication Number:
  US 20140077865A1
• Time in Patent Office: 1,440 Days
• Field of Search: 34235776, 34235777, 330302, 330306, 330310
• CPC Class Codes: G01S 19/21 Interference related issues ; Issues related to cross-correlation, spoofing or other methods of denial of service
• CPC Class Codes: G01S 19/36 relating to the receiver frond end
• CPC Class Codes: G01S 19/37 Hardware or software details of the signal processing chain
• CPC Class Codes: H03F 2200/451 the amplifier being a radio frequency amplifier
• CPC Class Codes: H03H 11/1239 Modifications to reduce influence of variations of temperature

Abstract

Low-noise amplifier (LNA) filters and processes for filtering global navigation satellite system (GNSS) signals are disclosed. The LNA filters can be used to down-convert a received GNSS signal to a lower frequency, filter the GNSS signal at the lower frequency, and up-convert the GNSS signal to the original frequency of the GNSS signal. The down-converted frequency can be selected based on a temperature of the GNSS signal to compensate for shifts in the frequency response of the filter due to temperature changes.

Claims

1. A low-noise amplifier (LNA) filter comprising:

a temperature sensor for detecting a temperature of the LNA filter;

a first stage coupled to receive a GNSS signal from a first antenna, wherein the first stage is configured to at least partially filter portions of the GNSS signal outside of a first frequency band, and wherein the GNSS signal has a signal frequency equal to an original frequency value within the first frequency band;

a second stage coupled to receive the GNSS signal from the first stage, wherein the second stage is configured to;

down-convert the frequency of the GNSS signal to a first value lower than the original frequency value, wherein the first value is within a second frequency band and the first value is based at least in part on the temperature of the LNA filter detected by the temperature sensor; and

at least partially filter portions of the down-converted GNSS signal outside of the second frequency band, wherein the second frequency band has a frequency range corresponding to a frequency range of the first frequency band after down-converting; and

a third stage coupled to receive the down-converted GNSS signal from the second stage, wherein the third stage is configured to up-convert the frequency of the GNSS signal to the original frequency value.

2. The LNA filter of claim 1 further comprising:

a fourth stage coupled to receive the GNSS signal from a second antenna, wherein the fourth stage is configured to at least partially filter portions of the GNSS signal outside of a third frequency band;

a fifth stage coupled to receive the GNSS signal from the fourth stage, wherein the fifth stage is configured to;

down-convert the frequency of the GNSS signal to a second value lower than the original frequency value; and

at least partially filter portions of the down-converted GNSS signal outside of a frequency band corresponding to the third frequency band; and

a sixth stage coupled to receive the down-converted GNSS signal from the fifth stage, wherein the sixth stage is configured to up-convert the frequency of the GNSS signal to the original frequency value.

3. The LNA filter of claim 2, wherein the first antenna and the second antenna are the same antenna.

4. The LNA filter of claim 2, wherein the fourth stage comprises:

a second ceramic filter coupled to receive the GNSS signal from the second antenna;

a second LNA circuit coupled to receive an output of the second ceramic filter; and

a third ceramic filter coupled to receive an output of the second LNA filter.

5. The LNA filter of claim 2, wherein the fifth stage comprises:

a third mixing circuit coupled to receive the GNSS signal from the first stage and a third clock signal from a third oscillator, wherein the third mixing circuit is configured to down-convert the frequency of the GNSS signal to the value lower than the original frequency value;

a third IFA circuit coupled to receive the down-converted GNSS signal from the third mixing circuit;

a fifth SAW filter coupled to receive an output of the third IFA circuit;

a fourth IFA circuit coupled to receive an output of the fifth SAW filter; and

a sixth SAW filter coupled to receive an output of the fourth IFA circuit.

6. The LNA filter of claim 2, wherein the sixth stage comprises:

a fourth mixing circuit coupled to receive the down-converted GNSS signal from the second stage and a fourth lock signal from a fourth oscillator, wherein the fourth mixing circuit is configured to up-convert the frequency of the GNSS signal to the original frequency value; and

a fourth ceramic filter coupled to receive up-converted GNSS signal from the fourth mixing circuit.

7. The LNA filter of claim 1, wherein the first stage comprises:

a first surface acoustic wave (SAW) filter coupled to receive the GNSS signal from the first antenna;

a first LNA circuit coupled to receive an output of the first SAW filter; and

a second SAW filter coupled to receive an output of the first LNA filter.

8. The LNA filter of claim 1, wherein the second stage comprises:

a first mixing circuit coupled to receive the GNSS signal from the first stage and a first clock signal from a first oscillator, wherein the first mixing circuit is configured to down-convert the frequency of the GNSS signal to the value lower than the original frequency value;

a first intermediate frequency amplifier (IFA) circuit coupled to receive the down-converted GNSS signal from the first mixing circuit;

a third SAW filter coupled to receive an output of the first IFA circuit;

a second IFA circuit coupled to receive an output of the third SAW filter; and

a fourth SAW filter coupled to receive an output of the second IFA circuit.

9. The LNA filter of claim 1, wherein the third stage comprises:

a second mixing circuit coupled to receive the down-converted GNSS signal from the second stage and a second clock signal from a second oscillator, wherein the second mixing circuit is configured to up-convert the frequency of the GNSS signal to the original frequency value; and

a first ceramic filter coupled to receive up-converted GNSS signal from the second mixing circuit.

10. A method for filtering a global navigation satellite system (GNSS) signal, the method comprising:

detecting a temperature of a low-noise amplifier (LNA) filter by a temperature sensor;

receiving, at a first stage of the LNA filter, a GNSS signal from a first antenna having a signal frequency equal to an original frequency value within a first frequency band;

down-converting, by a second stage of the LNA filter, the frequency of the GNSS signal to a value lower than the original frequency value, wherein the value is within a second frequency band and the value is based at least in part on the temperature of the LNA filter detected by the temperature sensor;

at least partially filtering, by the second stage of the LNA filter, the down-converted GNSS signal outside of the second frequency band, wherein the second frequency band has a frequency range corresponding to a frequency range of the first frequency band after down-converting; and

up-converting, by a third stage of the LNA filter, the frequency of the GNSS signal to the original frequency value.

11. The method claim 10 further comprising at least partially filtering portions of the up-converted GNSS signal outside of a third frequency band.

12. The method claim 10 further comprising, after receiving the GNSS signal and before down-converting the GNSS signal, at least partially filtering portions of the GNSS signal outside of the first frequency band.

13. The method claim 10, wherein the GNSS signal comprises information transmitted on an L1, L2, or L5 band.

14. The method claim 10, wherein:

the first stage comprises;

a first surface acoustic wave (SAW) filter coupled to receive the GNSS signal from a first antenna;

a first LNA circuit coupled to receive an output of the first SAW filter; and

a second SAW filter coupled to receive an output of the first LNA filter;

the second stage comprises;

a first mixing circuit coupled to receive the GNSS signal from the first stage and a first clock signal from a first oscillator, wherein the first mixing circuit is configured to down-convert the frequency of the GNSS signal to the value lower than the original frequency value;

a first intermediate frequency amplifier (IFA) circuit coupled to receive the down-converted GNSS signal from the first mixing circuit;

a third SAW filter coupled to receive an output of the first IFA circuit;

a second IFA circuit coupled to receive an output of the third SAW filter; and

a fourth SAW filter coupled to receive an output of the second IFA circuit; and

the third stage comprises;

a second mixing circuit coupled to receive the down-converted GNSS signal from the second stage and a second clock signal from a second oscillator, wherein the second mixing circuit is configured to up-convert the frequency of the GNSS signal to the original frequency value; and

a first ceramic filter coupled to receive up-converted GNSS signal from the second mixing circuit.

15. The method claim 10, wherein:

the first stage comprises;

a second ceramic filter coupled to receive the GNSS signal from a second antenna;

a second LNA circuit coupled to receive an output of the second ceramic filter; and

a third ceramic filter coupled to receive an output of the second LNA filter;

the second stage comprises;

a third mixing circuit coupled to receive the GNSS signal from the first stage and a third clock signal from a third oscillator, wherein the second mixing circuit is configured to down-convert the frequency of the GNSS signal to the value lower than the original frequency value;

a third IFA circuit coupled to receive the down-converted GNSS signal from the third mixing circuit;

a fifth SAW filter coupled to receive an output of the third IFA circuit;

a fourth IFA circuit coupled to receive an output of the fifth SAW filter; and

a sixth SAW filter coupled to receive an output of the fourth IFA circuit; and

the third stage comprises;

a fourth mixing circuit coupled to receive the down-converted GNSS signal from the second stage and a fourth clock signal from a fourth oscillator, wherein the fourth mixing circuit is configured to up-convert the frequency of the GNSS signal to the original frequency value; and

a fourth ceramic filter coupled to receive up-converted GNSS signal from the fourth mixing circuit.