EP1456686A1 - Verfahren zum verarbeiten eines datenenthaltenden navigationssignals - Google Patents

Verfahren zum verarbeiten eines datenenthaltenden navigationssignals

Info

Publication number
EP1456686A1
EP1456686A1 EP02805387A EP02805387A EP1456686A1 EP 1456686 A1 EP1456686 A1 EP 1456686A1 EP 02805387 A EP02805387 A EP 02805387A EP 02805387 A EP02805387 A EP 02805387A EP 1456686 A1 EP1456686 A1 EP 1456686A1
Authority
EP
European Patent Office
Prior art keywords
signals
type
signal
processing
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.)
Withdrawn
Application number
EP02805387A
Other languages
English (en)
French (fr)
Inventor
Nicolas Thales Intellectual Property Martin
Blandine Thales Intellectual Property Coatantiec
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.)
Thales SA
Original Assignee
Thales SA
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 Thales SA filed Critical Thales SA
Publication of EP1456686A1 publication Critical patent/EP1456686A1/de
Withdrawn legal-status Critical Current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
    • G01S19/24Acquisition or tracking or demodulation of signals transmitted by the system

Definitions

  • the present invention relates to methods for processing navigation signals when they also include one or more additional modulations making it possible to transmit data which complement the information intrinsically contained in the elementary signal. It applies more particularly to the processing of navigation signals transmitted by satellites.
  • Radio navigation by satellite currently mainly uses the signals emitted by the GPS system, and incidentally those of the GLONASS system. In the future, it will use the signals from the GALILEO system.
  • This radio navigation makes it possible to obtain the position of the receiver by processing the signals transmitted by at least three satellites and by performing phase measurements and code measurements on these signals. Code measurements are not very precise but unambiguous, while phase measurements are much more precise but ambiguous.
  • the signals transmitted by the satellites contain data bits which make it possible to transmit navigation messages. These messages are used in the calculation algorithms to determine the position, speed and time of the receiver.
  • the received phase rotates and it is then necessary to use an integration system, which makes it possible to obtain a reactive control over this phase.
  • the invention proposes a method of processing a navigation signal containing data, in which a first DBPSK type carrier band for demodulating navigation signals, and in which a second BPSK type loop is also used to identify the data tests.
  • the code 101 and carrier 102 oscillators are controlled by the error signals which are described below. They make it possible respectively to obtain a point code and a ⁇ code in a generator 103 and sin signals. and cos. in phase shifters 104 and 105.
  • the punctual signals, ⁇ , cos. and sin. are applied to a correlator 106 which makes it possible, from the received signal, to obtain the signals l p , l ⁇ , Q p and Q ⁇ in a conventional manner using a set of multipliers 107 and blocking samplers 108.
  • these signals are sampled at a given frequency.
  • two demodulators are used, a first demodulator of the DBPSK type for the carrier and a second demodulator of the DBPSK type for the data.
  • the signals sampled at the output of the correlator 106 are multiplied together in a module 109 to obtain crossed products l p . I ⁇ , l Q ⁇ > Qp • I ⁇ and Q p . Q ⁇ .
  • These cross products are integrated into a set of blocking integrator circuits 110, to then obtain the variables A, B, C and D defined by the formulas:
  • the signals l p and Q p are subjected to a so-called "squaring" treatment, which consists in performing a complex product l p x / Q p .
  • These signals are themselves integrated into a second set of blocking integrators 112.
  • the signal ⁇ is then applied to a code corrector 114 which performs a conventional filtering operation. After sampling at the loop frequency, this filtered signal ⁇ forms the error signal applied to the input of the code oscillator 101.
  • the signals l p 'and Q p ' coming from "squaring" are applied to the discriminator carrier type DBPSK 115 which will be described later.
  • the signal ⁇ coming from this discriminator 115 is applied on the one hand to the code discriminator 113, and on the other hand to a carrier corrector 116, which also performs a simple known filtering operation.
  • the signal ⁇ is thus filtered and then sampled at the loop frequency to form the error signal of the carrier oscillator 102.
  • the signals l p 'and Q p ' are first applied to a differentiator 201.
  • the signals at the output of this differentiator are then applied to a BPSK 202 type discriminator which performs the tangent arc operation (x, y) in an interval - ⁇ + ⁇ .
  • This discriminator 202 is then applied to an integrator 203, which operates conventionally with an adder 213 and a generator 223 with a function in Z "1 .
  • a ⁇ n + 1 argument (l n + 1 + iQ n + 1 ). - argument ⁇ + iQ n )
  • the identification of the data bits is done in an identifier 117 from the signals l p and Q p supplied by the correlator 106.
  • This identifier operates on the basis of a BPSK type discriminator. The phase discrimination is therefore then limited between - ⁇ and + ⁇ and the time constant Te / K is chosen small enough to decorrelate the successive bit errors.
  • the signals l p and Q p are applied to a complex multiplier 301, which also receives the signals at the output of a module 302 which will be described later.
  • the signals I and Q coming from this complex conduit are then applied to a discriminator 303 of the BPSK type, which performs the tangent arc operation (x, y) on a signal bounded between - ⁇ / 2 and + ⁇ 12.
  • the signal at the output of this discriminator is multiplied by a constant K in an amplifier 304, then it is applied to an integrator 305 in the structure is identical to that of the integrator 203 of FIG. 2.
  • the signal ⁇ at the output of this integrator is applied to the module 302 which performs the operation e "1 ⁇ to give the signals provided above.
  • the data bits are then obtained by determining, using a comparator circuit 306, the sign of the signal I leaving the complex product generator 301.

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Digital Transmission Methods That Use Modulated Carrier Waves (AREA)
EP02805387A 2001-12-18 2002-12-13 Verfahren zum verarbeiten eines datenenthaltenden navigationssignals Withdrawn EP1456686A1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0116397A FR2833714B1 (fr) 2001-12-18 2001-12-18 Procede de traitement d'un signal de navigation contenant des donnees
FR0116397 2001-12-18
PCT/FR2002/004349 WO2003054575A1 (fr) 2001-12-18 2002-12-13 Procede de traitement d'un signal de navigation contenant des donnees

Publications (1)

Publication Number Publication Date
EP1456686A1 true EP1456686A1 (de) 2004-09-15

Family

ID=8870645

Family Applications (1)

Application Number Title Priority Date Filing Date
EP02805387A Withdrawn EP1456686A1 (de) 2001-12-18 2002-12-13 Verfahren zum verarbeiten eines datenenthaltenden navigationssignals

Country Status (5)

Country Link
US (1) US20040260456A1 (de)
EP (1) EP1456686A1 (de)
CA (1) CA2470375A1 (de)
FR (1) FR2833714B1 (de)
WO (1) WO2003054575A1 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2834144B1 (fr) * 2001-12-20 2004-02-27 Thales Sa Convertisseur et convertisseur inverse (moyenne, ecart), correcteur de boucle, recepteur et procede de reception bi-frequence associe les utilisant
FR2913773B1 (fr) * 2007-03-16 2014-08-01 Thales Sa Dispositif de reception de signaux satellitaires comprenant une boucle de phase avec compensation des retards

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61270678A (ja) * 1985-05-24 1986-11-29 Hitachi Ltd Gps受信機
US4972431A (en) * 1989-09-25 1990-11-20 Magnavox Government And Industrial Electronics Company P-code-aided global positioning system receiver
US5117232A (en) * 1990-06-04 1992-05-26 Raytheon Company Global system positioning receiver
US5541606A (en) * 1995-02-02 1996-07-30 Trimble Navigation Limited W-code enhanced cross correlation satellite positioning system receiver
FI98412C (fi) * 1995-03-13 1997-06-10 Vaisala Oy Kooditon GPS-paikannusmenetelmä sekä laitteisto kooditonta paikannusta varten
US5610984A (en) * 1995-11-22 1997-03-11 Trimble Navigation Limited Optimal L2 tracking in a SPS receiver under encryption without knowledge of encryption timing characteristics
FR2742612B1 (fr) * 1995-12-15 1998-02-06 Sextant Avionique Procede et circuit de reception de signaux de positionnement par satellites avec elimination des erreurs de multitrajets
US5825887A (en) * 1995-12-28 1998-10-20 Trimble Navigation Limited Transmitting and receiving apparatus for full code correlation operation under encryption for satellite positioning system
US5923287A (en) * 1997-04-01 1999-07-13 Trimble Navigation Limited Combined GPS/GLONASS satellite positioning system receiver
US5983160A (en) * 1997-04-21 1999-11-09 Raytheon Company Increase jamming immunity by optimizing processing gain for GPS/INS systems
FR2769442B1 (fr) * 1997-10-02 1999-12-31 Dassault Electronique Recepteur de radionavigation perfectionne, en particulier du type gps
US6236355B1 (en) * 1999-01-23 2001-05-22 Trimble Navigation Ltd Fast recovery of lock point information for GPS RTK receiver
FR2789172B1 (fr) * 1999-02-02 2001-04-13 Sextant Avionique Appareil a gyrometres et accelerometres pour la determination des attitudes d'un aerodyne
US6608589B1 (en) * 1999-04-21 2003-08-19 The Johns Hopkins University Autonomous satellite navigation system
US6658048B1 (en) * 2000-04-07 2003-12-02 Nokia Mobile Phones, Ltd. Global positioning system code phase detector with multipath compensation and method for reducing multipath components associated with a received signal

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO03054575A1 *

Also Published As

Publication number Publication date
FR2833714A1 (fr) 2003-06-20
WO2003054575A1 (fr) 2003-07-03
US20040260456A1 (en) 2004-12-23
FR2833714B1 (fr) 2004-04-02
CA2470375A1 (fr) 2003-07-03

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