EP4168829A1 - Verfahren zur verarbeitung eines von einem satelliten erzeugten funknavigationssignals - Google Patents

Verfahren zur verarbeitung eines von einem satelliten erzeugten funknavigationssignals

Info

Publication number
EP4168829A1
EP4168829A1 EP21740152.0A EP21740152A EP4168829A1 EP 4168829 A1 EP4168829 A1 EP 4168829A1 EP 21740152 A EP21740152 A EP 21740152A EP 4168829 A1 EP4168829 A1 EP 4168829A1
Authority
EP
European Patent Office
Prior art keywords
amplitude
frequency
signal
processing
radio navigation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP21740152.0A
Other languages
English (en)
French (fr)
Inventor
Arnaud Lilbert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Electronics and Defense SAS
Original Assignee
Safran Electronics and Defense SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Safran Electronics and Defense SAS filed Critical Safran Electronics and Defense SAS
Publication of EP4168829A1 publication Critical patent/EP4168829A1/de
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/01Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/13Receivers
    • G01S19/21Interference related issues ; Issues related to cross-correlation, spoofing or other methods of denial of service
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S19/00Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
    • G01S19/38Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
    • G01S19/39Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
    • G01S19/393Trajectory determination or predictive tracking, e.g. Kalman filtering

Definitions

  • TITLE Process for processing a radio navigation signal from a satellite
  • the invention relates to positioning by satellites and relates in particular to a method and a device for processing signals in a satellite positioning system.
  • Global Navigation Satellite System Global Navigation Satellite System
  • GLONASS Global Navigation Satellite System
  • satellite positioning receivers implement a correlation between a measurement signal (from satellites) (hereinafter GNSS signal) and a replica signal and processing s making it possible to reduce interference in the measurement signal before it correlates with the aftershock signal.
  • GNSS signal a measurement signal from satellites
  • GNSS signal a measurement signal from satellites
  • processing s making it possible to reduce interference in the measurement signal before it correlates with the aftershock signal.
  • These treatments are generally called: pre-correlative interference elimination treatments.
  • Gaussian noise power For certain types of pre-correlative interference elimination processing, it is necessary to estimate the Gaussian noise power to separate, on the one hand, the GNSS signals embedded in the noise and, on the other hand, the interference whose power is greater than Gaussian noise. This separation is used in particular in frequency filtering techniques such as frequency excision or amplitude blocking, for which a good estimate of the Gaussian noise power is essential.
  • the invention makes it possible to separate a useful GNSS signal from interference in a simple manner.
  • the invention proposes, according to a first aspect, a method for processing a radionavigation signal originating from a satellite, said method comprising the following steps implemented in a processing unit of a radionavigation receiver :
  • the processing of the frequency radio navigation signal can comprise a frequency excision, the processing consisting in removing the components whose amplitude is greater at the determined threshold;
  • the processing of the frequency radio navigation signal can include amplitude blocking;
  • determining the distribution law consists in obtaining a histogram of the amplitude of the real component;
  • the method further comprises a conversion of the frequency radio navigation signal in which the components whose amplitude is greater than the determined threshold have been removed in the time domain by means of a complex inverse Fourier transform so as to obtain a signal of radio navigation processed.
  • the invention provides, according to a second aspect, a computer program product comprising program code instructions for the execution of steps of a method according to the first aspect of the invention, when this program is executed by a computer.
  • FIG. 1 illustrates a receiver of signals from a satellite according to the invention
  • FIG. 2 a method of processing signals from a satellite according to the invention
  • FIG. 3a and 3b illustrate representations of a frequency signal obtained during the method according to the invention.
  • FIG. 1 illustrates a radionavigation receiver 1 hereinafter GNSS receiver comprising a reception unit 11 configured to acquire a radionavigation signal (hereinafter GNSS signal) originating from a SAT satellite, for example of the GPS or GLONASS type and convert it to a digital GNSS signal.
  • the reception unit 11 comprises in particular an antenna A and an analog-to-digital converter (not shown) to obtain a digital signal S at the output of the reception unit 11.
  • the reception unit 11 comprises other elements which will not be not described in more detail because they are well known to those skilled in the art.
  • the GNSS receiver 1 comprises a processing unit 2 to which the reception unit 11 communicates the digitized GNSS signal S (hereinafter the GNSS signal).
  • the processing unit 2 consists of one or more processors which make it possible to implement various processing operations.
  • the received and digitized GNSS signal comprises a useful signal transmitted by the SAT satellite, a white Gaussian noise and interference to be eliminated.
  • the processing unit 2 comprises a module 20 for dividing the GNSS signal into blocks of samples of predetermined size.
  • the processing unit 2 comprises a time / frequency converter 21 configured to convert the GNSS signal into the frequency domain, the GNSS signal being in the time domain.
  • the converter 21 makes it possible to apply a complex discrete Fourier transform (DFT, for Discrete Fourier Transform).
  • DFT complex discrete Fourier transform
  • the receiver 1 comprises an interference suppression module 22 configured to implement a certain number of processing operations on the frequency signal coming from the converter 21. These steps will be detailed below.
  • This module 22 supplies a frequency signal in which interference has been eliminated to a frequency / time converter 23 which is configured to convert this signal in the time domain.
  • converter 23 makes it possible to apply a complex discrete Fourier transform inverse to that applied by converter 21.
  • This time signal is then supplied to a correlation unit 24 which allows processing to be applied to the time signal to provide the navigation signal as known to those skilled in the art.
  • the processing unit 2 also includes a memory 25 which makes it possible to store signals during the various processing operations.
  • FIG. 2 illustrates the steps of a method for processing GNSS signals originating from a satellite implemented by the processing unit 2.
  • a signal from a satellite is received and digitized by receiver 1 (step 100) to obtain the GNSS signal denoted S.
  • the digitized GNSS signal S comprising a useful signal transmitted by the satellite
  • SAT a Gaussian white noise and interference to be eliminated is first windowed (step 101) and cut into blocks of several samples on which a complex DFT (step 102) is applied to obtain a frequency signal.
  • Windowing has the effect of limiting the spectral diffusion resulting from the complex DFT and linked to the temporal truncation.
  • An example of windowing is of the Blackman-Harris type.
  • the frequency signal comprises N samples of indices 1 to N, N being a multiple of 2, for example 256 ⁇ N ⁇ 1024.
  • the frequency signal comprises a real part (component in phase I) and an imaginary part (component in quadrature Q).
  • the determination of this distribution function consists in calculating the amplitude I, 2 of each samples li of the real part and classifying them by level to obtain a histogram of the number of samples having a certain amplitude value.
  • the step of the histogram is constant and is for example equal to 1.
  • the amplitude of the real part for which the distribution function vanishes is determined (step 104). This determined amplitude corresponds to a threshold so that the samples for which the amplitude of the real part is greater than this threshold are noise levels.
  • Figure 3a illustrates the amplitude of the real part as a function of frequency, the corresponding distribution function being illustrated in Figure 3b.
  • the spectrogram represents a GPS C / A signal embedded in Gaussian noise in the presence of CW interference centered on the L1 frequency.
  • the frequency signal is processed so as to filter or remove its components whose amplitude of the real part is greater than the determined threshold (step 105).
  • the signal thus processed is then converted into a temporal signal via the application of a complex inverse transform (complex DFT 1 ) to this signal (step 106).
  • complex DFT 1 complex inverse transform
  • a signal S ’ is then obtained. It is this signal which then makes it possible to obtain the navigation signal S ".
  • the processing on the frequency signal in step 105 can consist of frequency excision on this signal.
  • Such treatment consists in canceling the frequency components for which the amplitude of the real part is greater than the threshold determined in step 104.
  • the cancellation of the frequency components is implemented on the real and imaginary parts.
  • the processing on the frequency signal in step 105 can consist of amplitude blocking.
  • amplitude blocking involves fixing the amplitude in the frequency range of the interference while maintaining its phase.
  • the value of the fixed amplitude can be chosen to: maximize the signal to noise ratio; take into account the percentage of frequency components to be processed; keep the spectral representation of the signal (advantageous variant) to limit the contribution of distortion in the rest of the processing.

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Noise Elimination (AREA)
EP21740152.0A 2020-06-22 2021-06-22 Verfahren zur verarbeitung eines von einem satelliten erzeugten funknavigationssignals Pending EP4168829A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2006070A FR3111712B1 (fr) 2020-06-22 2020-06-22 Procédé de traitement d’un signal de radionavigation issu d’un satellite
PCT/FR2021/051129 WO2021260315A1 (fr) 2020-06-22 2021-06-22 Procédé de traitement d'un signal de radionavigation issu d'un satellite

Publications (1)

Publication Number Publication Date
EP4168829A1 true EP4168829A1 (de) 2023-04-26

Family

ID=73138887

Family Applications (1)

Application Number Title Priority Date Filing Date
EP21740152.0A Pending EP4168829A1 (de) 2020-06-22 2021-06-22 Verfahren zur verarbeitung eines von einem satelliten erzeugten funknavigationssignals

Country Status (5)

Country Link
US (1) US20230258816A1 (de)
EP (1) EP4168829A1 (de)
CN (1) CN115735139A (de)
FR (1) FR3111712B1 (de)
WO (1) WO2021260315A1 (de)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101063300B1 (ko) * 2011-01-31 2011-09-07 국방과학연구소 위성 항법 신호의 간섭 제거 시스템, 장치 및 방법

Also Published As

Publication number Publication date
US20230258816A1 (en) 2023-08-17
CN115735139A (zh) 2023-03-03
WO2021260315A1 (fr) 2021-12-30
FR3111712A1 (fr) 2021-12-24
FR3111712B1 (fr) 2023-03-10

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