Device for receiving radio-navigation signals with multiple antennas and common synchronization slaving

Patent metadata

Field	Value
Publication number	US-9500749-B2
Application number	US-201313847390-A
Country	US
Kind code	B2
Filing date	Mar 19, 2013
Priority date	Mar 22, 2012
Publication date	Nov 22, 2016
Grant date	Nov 22, 2016

Abstract

The invention relates to a device for receiving satellite radio-navigation signals comprising a plurality of receiving antennas forming an antenna array. The invention consists in using a plurality of antennas disposed around the circumference of a carrier, in demodulating the signals received by each antenna separately and then in combining the various demodulated signals, thereby amounting to effecting a beam forming in an equivalent antenna pattern. The invention then requires only a single synchronization slaving for the set of demodulation pathways.

First claim

The invention claimed is:

1. Device for receiving satellite radio-navigation signals comprising a plurality of receiving antennas forming an antenna array, for each antenna and for each satellite in view of the said device, demodulator for demodulating the signals received comprising a multiplier for phase-wise multiplication with a local carrier, a correlator for time-wise correlation with a local code, an integrator for integration of the correlated signal in phase and in time, a carrier NCO numerical control operator able to deliver a local carrier phase for driving the generation of the local carrier and a code NCO numerical control operator able to deliver a time command for driving the generation of the local code and a measurement of the instant of emission by the satellite of the signal received,
wherein the said device furthermore comprises, for each satellite, a carrier and code tracking loop comprising:
a beamformer able to deliver, on the basis of the output signals Z 1 , Z 2 of the integrator, a unique formed signal Z equal to the sum of the said signals Z 1 , Z 2 weighted by complex weighting coefficients equal to the product of the gain G a of the associated antenna with a corrective gain G BL of the lever arm between the phase centre of the antenna and the centre of symmetry O of the antenna array;
a code discriminator and a phase discriminator which are applied to the said formed signal Z;
a code loop corrector applied at the output of the code discriminator and able to deliver a speed correction as input for the code numerical control operators;
a carrier loop corrector applied at the output of the phase discriminator and able to deliver a speed correction as input for the carrier numerical control operators; and
a calculator for computing the average of the said measurements of the instant of emission by the satellite of the signal received.

2. Device for receiving radio-navigation signals according to claim 1 , wherein the receiving antennas are positioned around the circumference of a carrier of substantially cylindrical shape.

3. Device for receiving radio-navigation signals according to claim 1 , wherein the corrective gain G BL of the lever arm is determined by the following calculation G BL =exp(jΔφ BL ), where Δφ BL =2π·ΔL BS /λ is the phase shift induced by the optical path difference ΔL BS between the phase centre of the antenna and the centre of symmetry O of the antenna array, λ being the wavelength of the carrier of the signal received.

4. Device for receiving radio-navigation signals according to claim 3 , wherein the optical path difference ΔL BS is determined by projecting the lever arm r onto the view axis between the centre of symmetry O of the antenna array and the satellite.

5. Device for receiving radio-navigation signals according to claim 4 , wherein the coordinates of the lever arm r are determined, in a spatial reference frame fixed with respect to the earth, on the basis of a measurement of the attitude of the carrier.

6. Device for receiving radio-navigation signals according to claim 1 , wherein it furthermore comprises, at the input of each code numerical control operator and of each carrier numerical control operator, a speed-wise lever arm corrector for compensating the outputs of the code loop corrector and carrier loop corrector by the temporal derivative of the optical path difference ΔL BS .

Assignees

• Thales Sa

Inventors

• Martin Nicolas
• Chopard Vincent
• Depraz David

Classifications

• G01S19/14 Primary

  specially adapted for specific applications · CPC title

• G01S19/29 Primary

  carrier {including Doppler,} related {(G01S19/246 takes precedence)} · CPC title

• G01S19/36

  relating to the receiver frond end · CPC title