WO1999013352A2 - Systeme de telemetrie - Google Patents
Systeme de telemetrie Download PDFInfo
- Publication number
- WO1999013352A2 WO1999013352A2 PCT/US1998/016530 US9816530W WO9913352A2 WO 1999013352 A2 WO1999013352 A2 WO 1999013352A2 US 9816530 W US9816530 W US 9816530W WO 9913352 A2 WO9913352 A2 WO 9913352A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- transmitters
- receiver
- information
- transmitter
- positioning
- Prior art date
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
- G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
- G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
- G01S5/10—Position of receiver fixed by co-ordinating a plurality of position lines defined by path-difference measurements, e.g. omega or decca systems
Definitions
- the present invention relates to range positioning systems and more particularly to range positioning systems utilizing a plurality of RF transmitters which broadcast their known position to a remote receiver which can utilize the transmitted data to calculate the position of the receiver.
- GPS Global Positioning Systems
- ground based receivers whose position is accurately known may be also utilized to detect any errors that exist in the satellite signals and to broadcast error signals to the receiver for use in correcting the satellite signal errors.
- DGPS Differential Global Positioning Systems
- GPS and DGPS have great utility for determining the position of a receiver that can receive signals from at least four of the satellites at one time (for GPS) or can receive signals from at least four of the satellites and at least one ground error calculating receiver (for DGPS), there are situations where this is not possible.
- the present invention fulfills the need for a simple, low cost positioning system for use in a predetermined location such as remote or confined areas and that will always be able to receive transmissions from at least four transmitters simultaneously. This is achieved by mounting the plurality of receivers around the predetermined location at selected positions and encoding them with their exact location and supplying them with a common clock. The selected positions are chosen so that regardless of the receiver's position within the predetermined area, it will always be able receive signals from at least four of the transmitters.
- the transmitters may be positioned at or near the four corners and, perhaps, placed in high positions so when the farmer with a receiver moves about the farm, he will always have a line of sight to four transmitters and thereby be able to determine his exact location.
- the transmitters may be most anywhere so long as their transmissions are not blocked by large metal structures.
- Figure 1 shows a conceptualized area in which a receiver is surrounded by four transmitters.
- FIG. 1 In Figure 1, four RF transmitters, E, , E 2 , E 3 and E 4 are shown identified by reference numerals 10, 12, 14 and 16 respectively each having a transmitting antenna identified by reference numerals 20, 22, 24 and 26 respectively. While five or more transmitters may be used to assure reception, only four have been shown for simplicity.
- a receiver 30, which may be mounted on or proximate an object, such as a tractor, whose position is desired to be known or controlled, is shown in an area, such as a farm, where the transmitters are mounted.
- the receiver includes a receiving antenna 32 and a position monitor box 34 which will contain the necessary computer programmed to determine position from the received signals.
- a single signal generator 50 Connected to the four transmitters 10, 12, 14 and 16 by lines 40, 42. 44 and 46 respectively is a single signal generator 50 which receives a common time based data signal from a data generator 52 connected to a single common clock 54. While the connections from the signal generator to the transmitters has been shown as hard wired, the signals may be broadcast. Several unobvious advantages accrue by the use of a single clock and signal generator. The only time differences between the various emitters is the transmission delay from the signal generator 50 to the transmitters and, since the positions of the transmitters are fixed with respect to the signal generator, these may be easily calibrated out by moving the receiver 30 to several known locations and calculating the time delays associated with each transmitter. Furthermore, using a single common clock removes any errors that might otherwise occur due to clock performance since such errors are common to all transmitters and the error is thus removed from the solution.
- Each transmitter receives the common time based signal from signal generator 50 and operates to create a spread spectrum signal similar in characteristics to the prior art GPS satellite signals.
- Each transmitter has a unique code to identify it and transmits its signals at a low level so as not to interfere with other RF signals in the area.
- the program for computing the position of receiver 30 can be the same as the prior art GPS programs but may be simplified with minor modifications since there is no need to try to adjust to a common time base or compensate for clock errors nor is there normally any need to try to compensate for atmospheric aberrations.
- the receiver 30 After setting the system up, the receiver 30 will track the transmitted signals and determine a three dimensional solution to its own position relative to the transmitters.
- the system is easily calibrated by feeding back the position information when the receiver 30 is at, say, four known locations relative to the transmitters. For example, by moving the receiver to the four transmitter locations and taking a reading at each, any errors between the calculated position and the actual position will be known and the receiver may be calibrated to correct for them.
- the calibration also determines the signal delay between the signal generator and the emitters and validates the location data on the signal. Once calibrated, the position information should be accurate to within very close tolerances, e.g. a decimeter. It may be desirable for the position sensor receiver to be not sensitive to the
- near far problem i.e. the overloading from a near transmitter compared to the signal from a remote transmitter. This problem is usually considered in the design of the GPS receivers which interface to pseudolites.
- a discussion of the "near/far” situation may be found , for example, in an paper entitled “Precision Landing Tests With Improved Integrity Beacon Pseudolites” by Stewart Cobb et al, given at the 8th International
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
- Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
Abstract
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU14489/99A AU1448999A (en) | 1997-08-07 | 1998-08-07 | Range positioning system |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US90848597A | 1997-08-07 | 1997-08-07 | |
US08/908,485 | 1997-08-07 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO1999013352A2 true WO1999013352A2 (fr) | 1999-03-18 |
WO1999013352A3 WO1999013352A3 (fr) | 1999-05-06 |
Family
ID=25425883
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1998/016530 WO1999013352A2 (fr) | 1997-08-07 | 1998-08-07 | Systeme de telemetrie |
Country Status (2)
Country | Link |
---|---|
AU (1) | AU1448999A (fr) |
WO (1) | WO1999013352A2 (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008085532A2 (fr) * | 2006-04-28 | 2008-07-17 | Loctronix Corporation | Système et procédé pour le positionnement dans des environnements configurés |
US9455762B2 (en) | 2006-04-28 | 2016-09-27 | Telecommunication Systems, Inc. | System and method for positioning using hybrid spectral compression and cross correlation signal processing |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107632286A (zh) * | 2017-08-07 | 2018-01-26 | 上海斐讯数据通信技术有限公司 | 一种移动终端的定位方法及系统 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1983004451A1 (fr) * | 1982-06-07 | 1983-12-22 | Storno A/S | Systeme de controle de position |
US5056106A (en) * | 1990-08-02 | 1991-10-08 | Wang James J | Golf course ranging and direction-finding system using spread-spectrum radiolocation techniques |
EP0502312A2 (fr) * | 1991-03-06 | 1992-09-09 | Robert Bosch Gmbh | Procédé pour déterminer la position d'un récepteur radio mobile |
WO1995000821A1 (fr) * | 1993-06-25 | 1995-01-05 | Omniplex, Inc. | Determination de la position a l'aide d'emissions de sites cellulaires a synchronisation temporelle |
US5530440A (en) * | 1992-12-15 | 1996-06-25 | Westinghouse Norden Systems, Inc | Airport surface aircraft locator |
US5686924A (en) * | 1995-05-30 | 1997-11-11 | Trimble Navigation Limited | Local-area position navigation system with fixed pseudolite reference transmitters |
-
1998
- 1998-08-07 WO PCT/US1998/016530 patent/WO1999013352A2/fr active Application Filing
- 1998-08-07 AU AU14489/99A patent/AU1448999A/en not_active Abandoned
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1983004451A1 (fr) * | 1982-06-07 | 1983-12-22 | Storno A/S | Systeme de controle de position |
US5056106A (en) * | 1990-08-02 | 1991-10-08 | Wang James J | Golf course ranging and direction-finding system using spread-spectrum radiolocation techniques |
EP0502312A2 (fr) * | 1991-03-06 | 1992-09-09 | Robert Bosch Gmbh | Procédé pour déterminer la position d'un récepteur radio mobile |
US5530440A (en) * | 1992-12-15 | 1996-06-25 | Westinghouse Norden Systems, Inc | Airport surface aircraft locator |
WO1995000821A1 (fr) * | 1993-06-25 | 1995-01-05 | Omniplex, Inc. | Determination de la position a l'aide d'emissions de sites cellulaires a synchronisation temporelle |
US5686924A (en) * | 1995-05-30 | 1997-11-11 | Trimble Navigation Limited | Local-area position navigation system with fixed pseudolite reference transmitters |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008085532A2 (fr) * | 2006-04-28 | 2008-07-17 | Loctronix Corporation | Système et procédé pour le positionnement dans des environnements configurés |
WO2008085532A3 (fr) * | 2006-04-28 | 2008-11-06 | Loctronix Corp | Système et procédé pour le positionnement dans des environnements configurés |
US7511662B2 (en) | 2006-04-28 | 2009-03-31 | Loctronix Corporation | System and method for positioning in configured environments |
CN101479622A (zh) * | 2006-04-28 | 2009-07-08 | 卢克卓尼克斯有限公司 | 用于在配置环境中定位的系统和方法 |
EA013169B1 (ru) * | 2006-04-28 | 2010-02-26 | Локтроникс Корпорейшн | Система и способ для определения местоположения в конфигурированных средах |
US7916074B2 (en) | 2006-04-28 | 2011-03-29 | Loctronix Corporation | System and method for positioning in configured environments |
KR101106387B1 (ko) * | 2006-04-28 | 2012-01-17 | 록트로닉스 코포레이션 | 설정되는 환경에서의 위치확인을 위한 시스템 및 방법 |
US9455762B2 (en) | 2006-04-28 | 2016-09-27 | Telecommunication Systems, Inc. | System and method for positioning using hybrid spectral compression and cross correlation signal processing |
Also Published As
Publication number | Publication date |
---|---|
AU1448999A (en) | 1999-03-29 |
WO1999013352A3 (fr) | 1999-05-06 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4894655A (en) | Landing assistance system using navigation satellites | |
US5225842A (en) | Vehicle tracking system employing global positioning system (gps) satellites | |
EP2221641B1 (fr) | Procédé et appareil pour déterminer une localisation à l'aide d'une estimation grossière de position | |
US5952961A (en) | Low observable radar augmented GPS navigation system | |
US7978133B1 (en) | GPS gyro calibration | |
EP1366376B1 (fr) | Procédé et appareil permettant de fournir une estimation de position améliorée en fonction d'une estimation de position initiale grossière | |
US5420594A (en) | Multi-mode position location method | |
US6839021B2 (en) | Method and apparatus for determining time in a satellite positioning system | |
US5945943A (en) | System for using differential GPS receivers with autopilot systems for category III precision approaches | |
US20060208946A1 (en) | System and method for global positioning system repeater | |
EP2000820A2 (fr) | Procédé et appareil pour déterminer une estimation d'erreur dans un système hybride de détermination de position | |
US6559793B1 (en) | Differential global positioning system using coarse GPS data for a fast time to a precise first fix | |
WO2009041846A1 (fr) | Mesure d'altitude indépendante dans un système de positionnement par satellite | |
Stombaugh | Satellite‐based Positioning Systems for Precision Agriculture | |
US6600444B2 (en) | System and method for computing navigation information in the presence of interference | |
US6844847B2 (en) | Method and device for instantaneous determination of orientation, based on satellite positioning signals | |
EP0682332A1 (fr) | Système de guidage précis de véhicules mobiles pour l'approche de points équipés d'un tel système | |
US8532885B1 (en) | Automatic GNSS signal allocation between remote and base receivers | |
EP3667369A1 (fr) | Système de positionnement pour véhicule terrestre et procédé de calcul de haute précision de position gnss d'un véhicule terrestre | |
JP3549893B2 (ja) | マルチパスを除去するための複数のgpsの受信装置 | |
EP2367023B1 (fr) | Flugzeuglandesystem mit relativer GNSS | |
WO1999013352A2 (fr) | Systeme de telemetrie | |
US6218984B1 (en) | Geo-referencing radio position determination systems using co-located antennas | |
EP1924029A1 (fr) | Procédé de contrôle de la formation de faisceau à une station de base, et une station de base | |
EP0524771A2 (fr) | Procédé radiogoniométrique |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
AK | Designated states |
Kind code of ref document: A2 Designated state(s): AL AM AT AU AZ BA BB BG BR BY CA CH CN CU CZ DE DK EE ES FI GB GE GH GM HR HU ID IL IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MD MG MK MN MW MX NO NZ PL PT RO RU SD SE SG SI SK SL TJ TM TR TT UA UG UZ VN YU ZW |
|
AL | Designated countries for regional patents |
Kind code of ref document: A2 Designated state(s): GH GM KE LS MW SD SZ UG ZW AM AZ BY KG KZ MD RU TJ TM AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE BF BJ CF CG CI CM GA GN GW ML MR NE SN TD TG |
|
AK | Designated states |
Kind code of ref document: A3 Designated state(s): AL AM AT AU AZ BA BB BG BR BY CA CH CN CU CZ DE DK EE ES FI GB GE GH GM HR HU ID IL IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MD MG MK MN MW MX NO NZ PL PT RO RU SD SE SG SI SK SL TJ TM TR TT UA UG UZ VN YU ZW |
|
AL | Designated countries for regional patents |
Kind code of ref document: A3 Designated state(s): GH GM KE LS MW SD SZ UG ZW AM AZ BY KG KZ MD RU TJ TM AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE BF BJ CF CG CI CM GA GN GW ML MR NE SN TD TG |
|
DFPE | Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101) | ||
121 | Ep: the epo has been informed by wipo that ep was designated in this application | ||
REG | Reference to national code |
Ref country code: DE Ref legal event code: 8642 |
|
122 | Ep: pct application non-entry in european phase |