EP1456686A1 - Verfahren zum verarbeiten eines datenenthaltenden navigationssignals - Google Patents
Verfahren zum verarbeiten eines datenenthaltenden navigationssignalsInfo
- 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- Withdrawn
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO 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
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
- G01S19/24—Acquisition 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)
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)
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)
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 |
-
2001
- 2001-12-18 FR FR0116397A patent/FR2833714B1/fr not_active Expired - Fee Related
-
2002
- 2002-12-13 WO PCT/FR2002/004349 patent/WO2003054575A1/fr not_active Application Discontinuation
- 2002-12-13 CA CA002470375A patent/CA2470375A1/fr not_active Abandoned
- 2002-12-13 EP EP02805387A patent/EP1456686A1/de not_active Withdrawn
- 2002-12-13 US US10/494,259 patent/US20040260456A1/en not_active Abandoned
Non-Patent Citations (1)
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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Legal Events
Date | Code | Title | Description |
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PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
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17P | Request for examination filed |
Effective date: 20040421 |
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AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR IE IT LI LU MC NL PT SE SI SK TR |
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STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 20050701 |