Receiver for a navigation system, in particular a satellite navigation system

• US 6,069,583 A
• Filed: 12/03/1997
• Issued: 05/30/2000
• Est. Priority Date: 05/09/1996
• Status: Expired due to Term

• Current Assignee: Agence Spatiale Europeenne
• Original Assignee: Agence Spatiale Europeenne
• Inventors: Daly, Peter, Walsh, David, Aardoom, Eric, Silvestrin, Pierluigi
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US08/984,578
• Time in Patent Office: 909 Days
• Field of Search: 342/357.01, 342/357.06, 342/357.12, 342/385, 701/213, 701/215, 455/13.3, 455/277.1
• US Class Current: 342/357.27
• CPC Class Codes: G01S 19/29 carrier including Doppler, related G01S19/246 takes precedence
• CPC Class Codes: G01S 19/32 Multimode operation in a single same satellite system, e.g. GPS L1/L2
• CPC Class Codes: G01S 19/33 Multimode operation in different systems which transmit time stamped messages, e.g. GPS/GLONASS
• CPC Class Codes: G01S 19/36 relating to the receiver frond end
• CPC Class Codes: G01S 19/53 Determining attitude

Abstract

The invention relates to a navigation system receiver comprising at least two antennas, one of which is a "reference" antenna. A multiplexer multiplexes the signals from the antennas, and a first processor situated downstream from the multiplexer delivers at least one navigation parameter on the basis of the signals from the multiplexer. The receiver includes a second processor having an input receiving in continuous manner signals from the reference antenna to deliver at least one reference signal representative of a position parameter of the reference antenna. Processor means process the signals from the multiplexer while taking account of at least one said reference signal.

Claims

1. A satellite navigation system receiver comprising at least two antennas, one of which is a reference antenna, a multiplexer for multiplexing signals from the antennas, a first processor operatively connected to the multiplexer to deliver at least one signal representative of a navigation parameter on the basis of signals from the multiplexer, a second processor having an input that receives signals continuously from the reference antenna to deliver at least one reference signal representative of a parameter concerning the position of the reference antenna, and processor means for processing the signals from the multiplexer while also taking into account said at least one reference signal and for calculating at least one item of navigation data.

2. A receiver according to claim 1, wherein the multiplexer has an input that receives signals from the reference antenna.

3. A receiver according to claim 2, wherein a multiplexer allocates a switching time to said input receiving the signal from the reference antenna which is shorter than the switching time allocated by the multiplexer to its other inputs receiving signals from other antennas.

4. A receiver according to claim 1, wherein:

the first processor includes a first RF/IF converter operatively associated with the multiplexer, and a first analog-to-digital converter;

the second processor includes a second RF/IF converter operatively associated with the reference antenna, and a second analog-to-digital converter; and

the receiver includes a frequency synthesizer common to the first and second processors and producing a local oscillator signal and a clock signal which are applied respectively firstly to at least the first and second RF/IF converters and to at least the first and second analog-to-digital converters.

5. A receiver according to claim 4, wherein the first and second analog-to-digital converters are in cascade with the first and second processors respectively.

6. A receiver according to claim 1, wherein one of said reference signals is a data modulation signal, and wherein said processor means includes means for removing said modulation signal present on said signals from the multiplexer device.

7. A receiver according to claim 1, wherein one of said reference signals is a signal representing the Doppler effect associated with the reference antenna and which is produced by a loop filter associated with the second processor;

and wherein said processor means include means responsive to said signal representing the Doppler effect to control a numerically-controlled oscillator forming a portion of the first processor, said oscillator also being controlled by a signal representing the Doppler effect associated with the antennas whose signals are multiplexed and which is produced by a loop filter associated with the first processor.

8. A receiver according to claim 7, wherein said loop filter of the first processor is a second order filter.

9. A receiver according to claim 8, wherein said loop filter of the first processor has a passband of less than 1 Hz.

10. A receiver according to claim 1, wherein the first processor includes at least one accumulator that is reinitialized both by a code instant signal and by an antenna switching instant signal, and wherein the second processor includes at least one accumulator reinitialized by said code instant signal.

11. A receiver according to claim 1, wherein the second processor includes at least one accumulator which is associated with a circuit for determining signs of consecutive data bits, and wherein the first processor includes at least one accumulator associated with a circuit for correcting partial correlation values as a function of the signs of consecutive data bits in such a manner as to obtain identical sign values.

12. A satellite navigation system receiver comprising at least two antennas, one of which is a reference antenna, a multiplexer for multiplexing signals from the antennas;

a first processor operatively associated with said multiplexer to deliver at least one signal representative of a navigation parameter on the basis of signals from the multiplexer, the first processor including a first RF/IF converter operatively associated with the multiplexer and a first analog-to-digital converter;

a second processor having an input that receives signals continuously from the reference antenna to deliver at least one reference signal representative of a parameter concerning the position of the reference antenna, the second processor including a second RF/IF converter operatively associated with the reference antenna and a second analog-to-digital converter;

a frequency synthesizer common to the first and second processors and producing a local oscillator signal and a clock signal which are applied respectively firstly to at least the first and second RF/IF converters and to at least the first and second analog-to-digital converters; and

processor means for processing the signals from the multiplexer and said at least one reference signal and for calculating at least one item of navigation data, wherein for each satellite signal to be processed, the receiver includes a processor block including a reference section forming a portion of the second processor and a slave section forming a portion of the first processor, each said section comprising;

a baseband converter for converting into baseband and also for image frequency rejection;

a numerically-controlled carrier oscillator having an output connected to an input of the baseband converter;

a numerically-controlled code oscillator;

a code generator controlled by said numerically-controlled code oscillator and generating early, punctual, and late codes E, P, and L;

a correlator receiving the signal output in baseband from the baseband converter and the early, punctual, and late codes E, P, and L, as generated by the code generator, and outputting correlation signals; and

an accumulator receiving the correlation signals as inputs and generating early, punctual, and late loop control signals as outputs;

the input of the slave section baseband converter is connected to the output of the first analog-to-digital converter;

the input of the reference section baseband converter is connected to the output of the second analog-to-digital converter; and

the processor means includes a digital processor receiving the loop control signals generated by the accumulator of the reference section and by the accumulator of the slave section, and generating loop signals for the carrier oscillators and for the code oscillators of the reference section and of the slave section.

13. A satellite navigation system receiver comprising at least two antennas, one of which is a reference antenna;

a multiplexer for multiplexing signals from the antennas;

a first processor operatively associated with said multiplexer to deliver at least one signal representative of a navigation parameter on the basis of signals from the multiplexer, the first processor including a first RF/IF converter operatively associated with the multiplexer and a first analog-to-digital converter;

a second processor having an input that receives signals continuously from the reference antenna to deliver at least one reference signal representative of a parameter concerning the position of the reference antenna, the second processor including a second RF/IF converter operatively associated with the reference antenna and a second analog-to-digital converter;

a frequency synthesizer common to the first and second processors and producing a local oscillator signal and a clock signal which are applied respectively firstly to at least the first and second RF/IF converters and to at least the first and second analog-to-digital converters; and

processor means for processing the signals from the multiplexer and said at least one reference signal and for calculating at least one item of navigation data, wherein, for each satellite signal to be processed, the receiver includes a processor block including a reference section forming a portion of the second processor, a slave section forming a portion of the first processor, and a section common to the first and second processors, wherein said common section includes;

a numerically-controlled carrier oscillator having an output;

a numerically-controlled code oscillator; and

a code generator controlled by said numerically-controlled code oscillator and generating early, punctual, and late codes E, P, and L;

wherein said reference section includes;

a baseband converter for conversion into baseband and for image frequency rejection, said baseband converter having an input connected to the output of the second analog-to-digital converter and an input connected to the output of the numerically-controlled carrier oscillator;

a correlator receiving the signal output in baseband from the baseband converter together with the early, punctual, and late codes E, P, and L generated by the code generator and outputting correlation signals; and

an accumulator receiving the correlation signals as inputs and generating as outputs early, punctual, and late loop control signals;

wherein said slave section includes;

a baseband converter performing baseband conversion and image frequency rejection, said baseband converter having an input connected to the output of the first analog-to-digital converter, and an input connected to the output of the numerically-controlled carrier oscillator;

a correlator receiving the signal output in baseband from the baseband converter together with the punctual code P generated by the code generator of the reference section, and outputting a punctual correlation signal; and

an accumulator receiving the punctual correlation signal as its input and outputting a punctual loop control signal;

and wherein the processor means includes a digital processor receiving the loop control signals generated by the accumulators of the reference section and of the slave section, and generating loop signals for the carrier oscillator and for the code oscillator.